- Source: List of aircraft engines
This is an alphabetical list of aircraft engines by manufacturer.
0–9
= 2si
=2si 215
2si 230
2si 430
2si 460
2si 500
2si 540
2si 690
= 3W
=Source: RMV
3W 106iB2
3W-110
3W-112
3W-170
3W-210
3W-220
A
= Abadal (Francisco Serramalera Abadal)
=Abadal Y-12 350/400 hp 120 mm × 140 mm (4.7 in × 5.5 in)
= ABC
=Source: Lumsden.
ABC 8 hp
ABC 30 hp V-4
ABC 45 hp V-6
ABC 60 hp V-8
ABC 85 hp V-6
ABC 100 hp V-8
ABC 115 hp
ABC 170 hp V-12
ABC 225 hp V-16
ABC Dragonfly
ABC Gadfly
ABC Gnat
ABC Hornet
ABC Mosquito
ABC Scorpion
ABC Wasp
ABC type 10 APU
ABC type 11 APU
= ABECO
=Source: RMV
ABECO GEM
= Aberg
=Source: RMV
Type Sklenar
= ABLE
=Source: RMV, Able Experimental Aircraft Engine Co. (Able Experimental Aircraft Engine Co., Altimizer, Hoverhawk (US))
ABLE 2275
ABLE 2500
ABLE VW x 2 Geared Drive
= Accurate Automation Corp
=Accurate Automation AT-1500
Accurate Automation AT-1700
= Ace
=(Ace American Engr Corp, Horace Keane Aeroplane Co, North Beach, Long Island NY.)
Ace 1919 40 hp
= ACE
=(American Cirrus Engine Inc)
Source: RMV
ACE Cirrus
ACE LA-1 19?? (ATC 31) = 140 hp 7RA. Evolved into Jacobs LA-1.
ACE Mk III 1929 (ATC 30, 44) = 90 hp 310ci 4LAI; (44) for 110 hp supercharged model.
ACE Mk III Hi-Drive
ACE Ensign
= ACT
=(Aircraft Cylinder and Turbine Co)
Source: RMV
ACT Super 600
= Adams
=Source: RMV
Adams (UK) 4 Cylinder in-line of 140 HP
Adams (UK) 8 V
= Adams-Dorman
=Source: RMV
Adams-Dorman 60/80 HP
= Adams-Farwell
=The Adams Company, Dubuque, Iowa / F.O. Farwell, engines for gyrocopters
Adams-Farwell 36 hp 5-cyl rotary engine 4.25 in × 3.25 in (108 mm × 83 mm)
Adams-Farwell 50 HP
Adams-Farwell 55 hp 5-cyl rotary 5.25 in × 5 in (133 mm × 127 mm)
Adams-Farwell 63 hp 5-cyl rotary 5.625 in × 5 in (142.9 mm × 127.0 mm)
Adams-Farwell 72 hp 5-cyl rotary 6 in × 6 in (150 mm × 150 mm)
Adams-Farwell 280 hp 6cyl double rotary 6 in × 6 in (150 mm × 150 mm)
Adams-Farwell 6-cyl double rotary 5 in × 5 in (130 mm × 130 mm)
Adams-Farwell 10-cyl double rotary 5 in × 5 in (130 mm × 130 mm)
Adams-Farwell 14-cyl double rotary 5 in × 5 in (130 mm × 130 mm)
Adams-Farwell 18-cyl double rotary 5 in × 5 in (130 mm × 130 mm)
Adams-Farwell KM 11
= ADC
=ADC (from "Aircraft Disposal Company") bought 35,000 war-surplus engines in 1920. Initially produced engines from Renault 70 hp spares.
ADC Airdisco
ADC Cirrus
ADC Nimbus, development of Siddeley Puma
ADC Airsix, air-cooled version of Nimbus. Not put into use
ADC BR2
ADC Viper
ADC Airdisco-Renault
= Adept-Airmotive
=Source: RMV
Adept 280 N
Adept 300 R
Adept 320 T
= Ader
=Source: RMV
Ader Eole engine (Vapour)
Ader Avion engine (Vapour)
Ader 2V
Ader 4V
= Adler
=Source: RMV
Adler 50 hp 4-cyl in-line 100 mm × 125 mm (3.9 in × 4.9 in)
Adler 100 hp 6-cyl in-line 115 mm × 135 mm (4.5 in × 5.3 in)
Adler 222 hp V-8 116 mm × 160 mm (4.6 in × 6.3 in)
= Adorjan & Dedics
=Source: RMV
Adorjan & Dedics 2V
= Advance Engines
=Source: RMV
Advance 4V, 20/25 HP
= Advanced Engine Design
=Source: RMV
Advanced Engine Design Spitfire 1 Cylinder
Advanced Engine Design Spitfire 2 Cylinder
Advanced Engine Design Spitfire 3 Cylinder
Advanced Engine Design Spitfire 4 Cylinder
Advanced Engine Design K2-1000
Advanced Engine Design 110 HP (BMW Conversion)
Advanced Engine Design 220 LC
Advanced Engine Design 440 LC
Advanced Engine Design 660 LC
Advanced Engine Design 880 LC
Advanced Engine Design 530 (Kawasaki Conversion)
= AEADC
=(Aircraft Engine & Accessory Development Corporation)
Source: RMV
AEADC Gryphon M
AEADC Gryphon N
AEADC O-510 (Gryphon M)
AEADC O-810 (Gryphon N)
= AEC
=Source: RMV
AEC Keane
= Aeolus Flugmotor
=Source: RMV
= Aerien CC
=Source: RMV
Aerien 20/25 HP
Aerien 30 HP
= Aermacchi
=Source: RMV
Aermacchi MB-2
= Aero & Marine
=Aero & Marine 50 HP
= Aero Adventure
=Source: RMV
Aero Adventure GFL-2000
= AeroConversions
=AeroConversions AeroVee 2180
= Aero Development
=Source: RMV
(See SPEER)
= Aero Engines Ltd.
=(formerly William Douglas (Bristol) Ltd.)
Aero Engines Dryad
Aero Engines Pixie
Aero Engines Sprite
Aero Engines inverted V-4
Aero Engines inverted V-6
Douglas 750cc
= Aero Motion
=Source: RMV
Aero Motion 0-100
Aero Motion 0-101
= Aero Motors
=Source: RMV
Aero Motors Aerobat 150 HP
= Aero Pixie
=Source: RMV
Aero Pixie 153 cc, 2T
= Aero Prag
=Source: RMV
Aeroprag KT-422
Aeroprag AP-45
Aeroprag TP-422
= Aero Products
=(Aero Products Aeronautical Products Corp, Naugatuck CT.)
Source: RMV
Aero Products Scorpion 100 HP
= Aero Sled
=Source: RMV
Aero Sled Twin Flat, 20 HP
= Aero Sport International
=Source: RMV
Aero Sport International Wade Aero (WANKEL) 2 Types
= AeroTwin Motors Corporation
=AeroTwin AT972T
= Aerojet
=Aerojet produced rocket engines for missiles. It merged with Pratt & Whitney Rocketdyne.
= Aeromarine Company
=Source: RMV
Aeromarine Company D5-1 (Pulse-Jet)
= Aeromarine
== Aeromax
=Source: RMV
Aeromax 100 I-F-B
Aeromax 100 L-D
= Aeromotion
=See: AMI
= Aeromotor
=(Detroit Aeromotor. Const. Co)
Source: RMV
Aeromotor 30 hp 4-cyl in-line
Aeromotor 75 hp 6-cyl in-line
= Aeronamic
=Source: RMV
Aeronamic ATS
= Aeronautical Engineering Co.
=Source: RMV
Aeronautical Engineering 9-cyl radial 200 HP
= Aeronca
=Aeronca E-107 (O-107)
Aeronca E-113 (O-113)
= Aeroplane Motors Company
=(Aeroplane Motors)
Source: RMV
Aeroplane 59 hp V-8 3.98 in × 4.72 in (101 mm × 120 mm)
= Aeroprotech
=Source: RMV
Aeroprotech VW 2.3
= Aerosila
=Source: RMV
Aerosila TA-4 FE
Aerosila 6 A/U
Aerosila 8 N/K
Aerosila 12
Aerosila 12-60
Aerosila 14 (-032,-130,-35)
Aerosila 18-100 (-200)
GTTP-300
= Aerosport
=Aerosport-Rockwell LB600
= Aerostar
=Source: RMV
Aerostar M14P
Aerostar M14V-26
= Aerotech engines
=Source: RMV
Aerotech 2 Cylinder 2T
= Aerotech-PL
=Source: RMV
Aerotech-PL EA81, Subaru conversion
Aerotech-PL VW conversion
Aerotech-PL BMW conversion
Aerotech-PL Suzuki conversion
Aerotech-PL Guzzi conversion
= Aerotechnik
=Source: RMV
Aerotechnik Tatra-100
Aerotechnik Tatra-102
Aerotechnik Hirth (Lic)
Aerotechnik Mikron (Lic)
Aerotechnik Tatra-714 (VW)
= Aerotek
=Source: RMV
Aerotek Mazda RX-7 (conversion)
= AES
=(See Rev-Air)
= Affordable Turbine Power
=Source: RMV
Affordable Turbine Power Model 6.5
= AFR
=Source: RMV
AFR BMW Conversion
AFR R 100 70/80 hp
AFR R 1100D 90/100 hp
AFR R 1100S 98 hp
AFR R 1150RT 95 hp
AFR R 1200GS 100 hp
= Agilis
=(Agilis Engines)
Sources: RMV
Agilis TF-800
Agilis TF-1000
Agilis TF-1200
Agilis TF-1400
Agilis TF-1500
Agilis TJ-60 (MT-60)
Agilis TJ-75
Agilis TJ-80
Agilis TJ-400
= Agusta
=Agusta GA.40
Agusta GA.70
Agusta GA.140
Agusta A.270
Turbomeca-Agusta TA.230
= Ahrbecker Son and Hankers
=Source: RMV
Ahrbecker Son and Hankers 10 HP
Ahrbecker Son and Hankers 20 HP
Ahrbecker Son and Hankers 1 Cylinder – vapor
= AIC
=(Aviation Ind. China. See Catic and Carec)
= Aichi
=Source:Gunston 1989 except where noted.
Aichi AC-1
Aichi Atsuta (Atsuta 31) – Licence-builtDaimler-Benz DB 601A for IJN
Aichi AE1A (Atsuta 21)
Aichi AE1P (Atsuta 32)
Aichi Ha-70 (Coupled Atsuta 30s)
= AICTA
=(AICTA Design Work, Prague, Czech Republic)
AICTA LMD 416-00R
= Aile Volante
=Aile Volante C.C.2
Aile Volante C.C.4
= Air Repair Incorporated
=Source: RMV
(Jacobs Licence)
Air Repair Incorporated L-4
Air Repair Incorporated L-5
Air Repair Incorporated L-6
(Jacobs-Page Licence)
Air Repair Incorporated R755
= Air Ryder
=Source: RMV
Air Ryder Subaru EA-81 (Conversion)
= Air Technical Arsenal
=Source: RMV
Air Technical Arsenal TSU-11
Air Technical Arsenal TR-30
= Air-Craft Engine Corp
=Source: RMV
Air-Craft Engine Corp LA-1
= Aircat
=(Detroit Aircraft Eng. Corp.)
Source: RMV
Aircat Radial 5 cylinders
= Aircooled Motors
=See: Franklin
= Aircraft Engine Co
=(Aircraft Engine Co Inc, Oakland, CA)
Aircraft 1911 80 hp
= Aircraft & Ind. Motor Corp
=(See Schubert)
= AiResearch
=See: Garrett, Allied Signal and Honeywell
= Airex
=Airex Rx2
Airex Rx10
= Airmotive-Perito
=See: Adept-Airmotive
= Airship Aircraft Engine Company
=Airship A-Tech 100 Diesel
= Airtrike
=(AirTrike GmbH i.L., Berlin, Germany)
Airtrike 850ti
= AISA
=Source: RMV
Ramjet on rotor
= Aixro
=Source: RMV
Aixro XF-40
Aixro XH-40
Aixro XP-40
Aixro XR-30
Aixro XR-40
Aixro XR-50
= Ajax
=Source: RMV
Ajax 7-cyl rotary
Ajax 6-cyl radial (2 rows of 3 cyls.), 80 HP
= Akkerman
=Akkerman Model 235 30 HP, special fuel
= Akron
=Funk E200
Funk E4L
= Albatross
=(Albatross Co Detroit)
Albatross 50 hp 6-cyl radial 4.5 in × 5 in (110 mm × 130 mm)
Albatross 100 hp 6-cyl radial 5.5 in × 5 in (140 mm × 130 mm)
= Aldasoro
=Aldasoro aero engine
= Alexander
=Alexander 4-cyl
Alexanderradial 5-cyl
= Alfa Romeo
=Societa per Azioni Alfa Romeo
= Alfaro
=Alfaro baby engine
Alfaro 155 hp 4-cyl barrel engine
= Allen
=Allen O-675
= Alliance
=(Aubrey W. Hess/Alliance Aircraft Corporation)
Hess Warrior
= Allied
=Allied Monsoon Licensed manufacturer of French Règnier 4L
= AlliedSignal
=AlliedSignal TPE-331
Garrett TPF351
AlliedSignal LTS101
AlliedSignal ALF502/LF507
= Allis-Chalmers
=Source: Gunston
Allis-Chalmers J36
= Allison
== Almen
=Almen A-4
= Alvaston
=Alvaston 20 hp 2-cyl opposed 114 mm × 114 mm (4.5 in × 4.5 in)
Alvaston 30 hp 2-cyl opposed 132 mm × 127 mm (5.2 in × 5.0 in)
Alvaston 50 hp 4-cyl opposed 144 mm × 128 mm (5.7 in × 5.0 in)
= Alvis
=Alvis Alcides
Alvis Alcides Major
Alvis Leonides
Alvis Leonides Major
Alvis Maeonides Major
Alvis Pelides
Alvis Pelides Major
= American Cirrus Engine
=See: ACE
= American Engineering Corporation
=Source: RMV
ACE Keane
= American Helicopter
=American Helicopter PJ49 Pulsejet
American Helicopter XPJ49-AH-3
= American Motor & Aviation Co
=American 1911 rotary
American S-5 radial
= AMCEL
=(AMCEL Propulsion Company)
AMCEL controllable solid fuel rocket
= AMI
=(AeroMotion Inc.)
AeroMotion Twin
AeroMotion O-100 Twin
AeroMotion O-101 Twin
= AMT Netherlands
=(Aviation Microjet Technology)
AMT Olympus
AMT Titan
AMT Lynx
= AMT USA
=(AMT USA, LLC, Cincinnati)
AMT-450
= A.M.U.A.L
=(Établissement A.M.U.A.L)
A.M.U.A.L M.J.5 65° V-8 350 hp 150 mm × 200 mm (5.9 in × 7.9 in)
A.M.U.A.L M.J.6 90° V-8 400 hp 150 mm × 200 mm (5.9 in × 7.9 in)
A.M.U.A.L M.J.7 90° V-8 600 hp 180 mm × 210 mm (7.1 in × 8.3 in)
= Angle
=Angle 100 hp Radial
= Ansaldo
=Ansaldo San Giorgio 4E-145 6I 300 hp
Ansaldo San Giorgio 4E-150 6I 300 hp
Ansaldo San Giorgio 4E-284 V-12 450 hp
Ansaldo San Giorgio 4E-290 V-12 550 hp
= Antoinette
=Source:Gunston
Antoinette 32 hp V-8 80 mm × 80 mm (3.1 in × 3.1 in)
Antoinette 46 hp?
Antoinette 64 hp V-16 80 mm × 80 mm (3.1 in × 3.1 in)
Antoinette 67hp V-8 110 mm × 105 mm (4.3 in × 4.1 in)
Antoinette 165 hp V-16
Antoinette 134 hp V-8 110 mm × 105 mm (4.3 in × 4.1 in)
Antoinette 55 hp V-8
Antoinette V-32
= Anzani
=For British Anzani products see: British Anzani
Source:
Air-cooled Anzani engines
Water-cooled Anzani engines
Anzani 30-32 hp V-4 100 mm × 120 mm (3.9 in × 4.7 in)
Anzani 56-70 hp V-4 135 mm × 150 mm (5.3 in × 5.9 in)
Anzani 600-700 hp 20-cyl radial 140 mm × 150 mm (5.5 in × 5.9 in) In-line radial 10 banks of 2 cylinders
Anzani W-6
Anzani 6A3 (6-cyl radial 60 hp)
= ARDEM
=(Avions Roger Druine Engines M)
Ardem 4 CO2
= Ares
=(Ares ltd., Finland)
Ares diesel Cirrus
= Argus Motoren
=Source:Gunston except where noted
= Argylls
=Argyll aircraft engine
= Armstrong Siddeley
=Armstrong Siddeley was formed by purchase of Siddeley-Deasy in 1919.
= Armstrong Whitworth
=Armstrong Whitworth 1918 30° V-12
= Arrow SNC
=Arrow 250
Arrow 270 AC
Arrow 500
Arrow 1000
= Arsenal
=Source:Gunston
Arsenal 213
Arsenal 12H
Arsenal 12H-Tandem
Arsenal 12K
Arsenal 24H
Arsenal 24H-Tandem
= Asahina
=Asahina 9-cyl 100 hp rotary
= Ashmusen
=(Ashmusen Manufacturing Company)
Ashmusen 1908 60 hp 8HOA
Ashmusen 1908 105 hp 12HOA
= Aspin
=(F.M. Aspin & Company)
Aspin Flat-Four
= Aster
=Aster 51 hp 4-cylinder-line
= Astrodyne
=(Astrodyne Inc.)
Astrodyne 16NS-1000
Astrodyne XM-34 (ZELL booster)
= ATAR
=(Atelier Technique Aéronautique de Rickenbach – pre SNECMA take-over)
ATAR 101
ATAR 103
ATAR 104 (Vulcain)
ATAR 201
ATAR 202
ATAR 203
= Atwood
=(Atwood Aeronautic Company, Williamsport, PA / Harry N. Atwood)
Atwood 120-180 hp V-12 (3.5 in × 4.5 in (89 mm × 114 mm) bore x stroke
Atwood M-1 (1916)
Atwood M-2 (1916)
Atwood Twin Six
= Aubier & Dunne
=Data from:Italian Civil & Military Aircraft 1930–1945
Aubier & Dunne 2-cyl 17 hp
Aubier & Dunne 3-cyl
Aubier-Dunne V.2D
= Austin
=Austin V-12
Austin rotary engine
= Austro-Daimler
=Source:Gunston
Austro-Daimler 35-40 hp 4-cyl. (35-40 hp 100 mm × 120 mm (3.94 in × 4.72 in))
Austro-Daimler 65-70 hp 4-cyl. (65-70 hp 120 mm × 140 mm (4.72 in × 5.51 in))
Austro-Daimler 90hp 6-cyl. (90 hp 120 mm × 140 mm (4.72 in × 5.51 in))
Austro-Daimler 120hp 6-cyl. (120 hp 130 mm × 175 mm (5.12 in × 6.89 in))
Austro-Daimler 160hp 6-cyl.
Austro-Daimler 185hp 6-cyl.
Austro-Daimler 200hp 6-cyl. (200 hp 135 mm × 175 mm (5.31 in × 6.89 in))
Austro-Daimler 210hp 6-cyl.
Austro-Daimler 225hp 6-cyl.
Austro-Daimler 300 hp V-12
Austro-Daimler 360 hp 6-cyl (360 hp 130 mm × 175 mm (5.12 in × 6.89 in))
Austro-Daimler 400 hp V-12 (400 hp 130 mm × 175 mm (5.12 in × 6.89 in))
Austro-Daimler D-35 (400 hp 130 mm × 175 mm (5.12 in × 6.89 in))
= Austro Engine
=Austro Engine E4 (AE 300)
Austro Engine AE50R
Austro Engine AE75R
Austro Engine AE80R
Austro Engine AE500
Austro Engine GIAE110R
= Auto Diesels
=Auto Diesels STAD A250
Auto Diesels STAD A260
Auto Diesels LPI Mk.12A/L
Auto Diesels LPI Mk.12A/T
Auto Diesels LPI Mk.12A/D
Auto Diesels GT15
Auto Diesels 7660.001.020
= Ava
=(L'Agence General des Moteurs Ava)
Ava 4A
= Avco Lycoming
=See: Lycoming
= Avia Motors
== Aviadvigatel
=Aviadvigatel PD-14
Aviadvigatel PS-90
= Aviatik
=Argus engines sold in France under the brand name 'Aviatik' by Automobil und Aviatik AG
Aviatik 70hp 4-cyl in-line 124 mm × 130 mm (4.9 in × 5.1 in)
Aviatik 100hp 4-cyl in-line 140 mm × 140 mm (5.5 in × 5.5 in)
Aviatik 150hp 4-cyl in-line 155 mm × 165 mm (6.1 in × 6.5 in)
= A.V. Roe
=A.V. Roe 20 hp 2-cyl.
= Avro
=Avro Alpha
= Avro Canada
=Avro Chinook
Avro Iroquois
Avro Orenda
Avro P.35 Waconda
= Axelson
=Axelson A-7-R 115 hp
Axelson-Floco B 150 hp
= Axial Vector Engine Corporation
=Dyna-Cam
= Aztatl
=Aztatl 3-cyl radial
Aztatl 6-cyl 80 hp radial
Aztatl 10-cyl radial
B
= Bailey
=Bailey C-7-R "Bull's Eye" 1927 = 140 hp 7RA.
= Bailey Aviation
=Bailey B200
Bailey Hornet
Bailey V5 engine
= Baradat–Esteve
=(Claudio Baradat Guillé & Carlos Esteve)
Baradat toroidal engine
= Basse und Selve
=Basse und Selve BuS. 120 hp (125 mm × 160 mm (4.9 in × 6.3 in) 120-130 hp)
Basse und Selve BuS.III 150 hp
Basse und Selve BuS.IV (160 mm × 200 mm (6.3 in × 7.9 in) / 155 mm × 200 mm (6.1 in × 7.9 in) 260 hp / 270 hp)
Basse und Selve BuS.IVa 300 hp
= Bates
=Data from:
Bates 29 hp V-4
= Bayerische
=(Bayerische Motoren Gesellschaft)
Bayerische 7-cyl 50 hp rotary
= Beardmore
=Source: Lumsden
Beardmore 90 hp (120 mm × 140 mm (4.7 in × 5.5 in))
Beardmore 120 hp
Beardmore 160 hp
Beardmore Simoon
Beardmore Cyclone
Beardmore Tornado
Beardmore 12-cyl opposed diesel
Beardmore Typhoon
Galloway Adriatic
Galloway Atlantic
= Béarn
=Construction Mécanique du Béarn/Société de Construction et d'Exploitation de Matériels et de Moteurs
Béarn 6
Béarn 12A
Béarn 12B
= Beatty
=Beatty 40 hp 4-cyl.(4.375 in × 4 in (111.1 mm × 101.6 mm))
Beatty 50 hp 4-cyl.(4.375 in × 4.5 in (111.1 mm × 114.3 mm))
Beatty 60 hp 4-cyl. (geared 0.66:1 4.375 in × 5 in (111.1 mm × 127.0 mm))
Beatty 80 hp 8-cyl. V-8 (4.375 in × 4 in (111.1 mm × 101.6 mm))
= Beck
=Beck 1910 toroidal engine
Beck 35 hp 4cyl toroidal engine 80 mm × 130 mm (3.1 in × 5.1 in)
Beck 50 hp 4cyl toroidal engine 110 mm × 130 mm (4.3 in × 5.1 in)
Beck 75 hp 4cyl toroidal engine 120 mm × 130 mm (4.7 in × 5.1 in)
= Beecher
=(B.L. Beecher Company, New Haven, Connecticut)
Beecher 8HOA
= Bell Aerosystems Company
== Bentley
=Bentley BR1
Bentley BR2
= Benz
=Source:Gunston
= Berliner
=Berliner 6 hp rotary helicopter engine
= Bertin
=Bertin 50 hp X-4
Bertin 100 hp X-8
= Besler
=See: Doble-Besler
= Beaussier
=(Moteurs Beaussier)
Beaussier 4-cyl
= Bessonov
=(A. A. Bessonov)
Bessonov MM-1
= Better Half
=Better Half VW
= Beardmore Halford Pullinger (B.H.P.)
=Adriatic
Atlantic
230 hp – built by Galloway and Siddeley-Deasy developed into Siddeley Puma
= Binetti
=Binetti B-300
= Blackburn
=Includes engines of Cirrus Engine Division of Blackburn
Source: Lumsden
Blackburn Cirrus – originally ADC Cirrus,
Blackburn Cirrus Midget
Blackburn Cirrus Minor
Blackburn Cirrus Major
Blackburn Cirrus Bombardier
Blackburn Cirrus Grenadier
Blackburn Cirrus Musketeer
Blackburn Nimbus
Blackburn Artouste – licence built Turbomeca Artouste
Blackburn Turbomeca Palouste – Turbomeca Palouste
Blackburn Turbomeca Palas – Turbomeca Palas
Blackburn Turbomeca Turmo – Turbomeca Turmo
Blackburn A.129
= Blackburne
=Blackburne Tomtit
Blackburne Thrush
= Bliss
=(E.W. Bliss Company)
Bliss Jupiter
Bliss Neptune
Bliss Titan
= Bloch
=Bloch 4B-1
Bloch 6B-1
= BMW
=Source: Gunston except where noted
= Boeing
=Source:Pelletier except where noted
Boeing T50
Boeing T60
Boeing 500
Boeing 502
Boeing 514
Boeing 520
Boeing 540 gas turbine engine (turboprop)
Boeing 550
Boeing 551 gas turbine engine (turboprop)
Boeing 553 gas turbine engine (turboprop)
= Boitel
=Boitel soleil
= Boland
=Boland V-8
= Bonner
=(Aero Bonner Ltd.)
Bonner Super Sapphire
= Borzecki
=(Jozef Borzecki)
Borzecki 2RB
Borzecki JB 2X250
= Botali
=Botali Diesel – eight-cylinder air-cooled 118 hp
= Bramo
=Source:Gunston except where noted
Bramo Sh.14A
Bramo 301
Bramo 314
Bramo 322
Bramo 323 Fafnir
Bramo 325
Bramo 328
Bramo 329 Twin Fafnir
Bramo 109-002
Bramo 109-003
= Brandner
=Brandner E-300
= Breda
=Breda 320 hp V-8
= Breguet-Bugatti
=Breguet-Bugatti U.16
Breguet-Bugatti U.24
Breguet-Bugatti U.24bis
Breguet-Bugatti Quadrimotor Type A
Breguet-Bugatti Quadrimotor Type B
Breguet-Bugatti H-32B
= Breitfeld & Danek
=Breitfeld & Danek Perun I 6-cylinder 170 hp
Breitfeld & Danek Perun II 6-cylinder 276 hp
Breitfeld & Danek BD-500 500 hp
Breitfeld & Daněk Hiero IV
Breitfeld & Daněk Hiero L
Breitfeld & Daněk Hiero N
= Breese
=Breese 40 hp 3-cyl radial
= Breuer
=(Breuer Werke G.m.b.H.)
Breuer 9-091
Breuer 9-094
= Brewer
=(Captain R.W.A. Brewer)
Brewer Type M Gryphon O-8
Brewer 250 hp O-12
Brewer 500 hp X-16
= Briggs & Stratton
=Briggs & Stratton Vanguard Big Block V-Twin
= Bristol Engine Company (Bristol)
=Division of Bristol Aeroplane Company formed when Cosmos Engineering was taken over in 1920. Became Bristol Aero Engines in 1956. Merged with Armstrong Siddeley in 1958 to form Bristol Siddeley.
Sources: Piston engines, Lumsden, gas turbine and rocket engines, Gunston.
Ramjets
= Bristol Siddeley
=Bristol Siddeley was formed by Bristol taking over Armstrong Siddeley, rebranding several of the engines. It took over de Havilland engines and, in turn, became a division of Rolls-Royce Limited.
= British Anzani
=For French Anzani engines see: Anzani
British Anzani 35 hp 2-cyl.
British Anzani 45 hp 6-cyl.
British Anzani 60 hp 6-cyl.
British Anzani 100hp 10-cyl.
= British Salmson
=British Salmson AD.3
British Salmson AC.7
British Salmson AC.9
British Salmson AD.9
British Salmson AD.9R srs III
British Salmson AD.9NG
= British Rotary
=British Rotary 100 hp 10-cyl. rotary
= Brooke
=(Brooke, Chicago)
Brooke 85 hp 10-cyl. rotary
Brooke 24 hp 6-cyl. rotary
Brooke Multi-X
= Brott
=(A. Brott, Denver, Colorado)
Brott 35 hp V-4 air-cooled
Brott 45 hp V-4 water-cooled
Brott 60 hp V-8 air-cooled
= Brouhot
=Brouhot 60 hp V-8
= Brownback
=(Brownback Motor Laboratories Inc.)
Brownback C-400 (Tiger 100)
= Bucherer
=Bucherer 2-cyl rotary
= Buchet
=Buchet 6 in-line
Buchet 8-12 hp 3-cyl inline
Buchet 24 hp 6-cyl radial 80 mm × 80 mm (3.15 in × 3.15 in)
= Bücker
=Bücker M 700
= Budworth
=(David Budworth Limited)
Budworth Puffin
Budworth Brill
Budworth Buzzard
= Bugatti
=Bugatti 8
Bugatti U-16
Bugatti Type 14
Bugatti Type 34 U-16
Bugatti Type 50B
Bugatti Type 60
= Burgess-White
=(W. Starling Burgess, Rollin H. White / Burgess Company of Marblehead, MA and White Company of Cleveland, OH)
Burgess-White X-16
= Burlat
=(Société des Moteurs Rotatifs Burlat)
Burlat 8cyl. 35 hp rotary – 26 kW (35 hp) at 1800 rpm, 95 mm × 120 mm (3.74 in × 4.72 in). 85 kg (187 lb). 6 500F
Burlat 8cyl. 60 hp rotary – 45 kW (60 hp) at 1800 rpm, 120 mm × 120 mm (4.72 in × 4.72 in), 120 kg (264 lb), 11000F
Burla 8cyl. 75 hp rotary – 56 kW (75 hp) at 1800 rpm, 120 mm × 170 mm (4.72 in × 6.69 in), 140 kg (308 lb), 11000F
Burlat 16cyl. 120 hp rotary – 89 kW (120 hp)p at 1750 rpm, 120 mm × 120 mm (4.72 in × 4.72 in), 225 kg (495 lb), 22000 F
= Burnelli
=Burnelli AR-3
= Burt
=(Peter Burt)
Burt 180 hp V-12
C
= CAC
=CAC R-975 Cicada
CAC R-1340
CAC R-1830
CAC Merlin
= CAE
=See:Teledyne CAE
= Caffort
=(Anciens Etablissements Caffort Frères)
Caffort 12Aa
= Cal-Aero
=(Cal-aero Institute, California)
Cal-Aero Project
= Call
=(Henry L. Call)
Call E-1 2OW
Call E-2 4OW
= CAM
=(Canadian Airmotive Inc.)
CAM TURBO 90
= Canton-Unné
=Canton-Unné X-9
= Cameron
=(Cameron Aero Engine Division / Everett S. Cameron)
Cameron C4-I-E1
Cameron C6
Cameron C12
= Campini
=Source:Gunston
Secondo Campini thermojet
= CANSA
=(Fabbrica Italiana Automobili Torino – Costruzioni Aeronautiche Novaresi S.A.)
CANSA C.80
= Carden Aero Engines
=Source:Ord-Hume.
Carden-Ford 31hp 4-cyl.
Carden-Ford S.P.1
= CAREC
=(China National Aero-Engine Corporation)
CAREC WP-11
= Casanova
=(Ramon Casanova)
Casanova pulse-jet
= Cato
=Cato 35 hp 2-cyl 2OA
Cato 60 hp 4-cyl 4IL
Cato C-2 75 hp 2OA
= Caunter
=Caunter B
Caunter C
Caunter D
= Centrum
=Centrum 150 hp 6-cyl radial
= Ceskoslovenska Zbrojovka
=Data from:
Ceskoslovenska Zbrojovka ZOD 260-B 2-stroke radial diesel engine – 260 hp
= CFM International
=CFM International CFM56
CFM International LEAP
CFM International RISE
= Chaise
=(Societe Anonyme Omnium Metallurgique et Industriel / Etablissements Chaise et Cie)
Chaise 12 hp V-2
Chaise 30 hp V-4
Chaise 4A 101 hp
Chaise 4B 120 hp (14° inverted V-4)
Chaise 4Ba
Chaise AV.2
= Chamoy
=(M. Fernand Chamoy)
Chamoy 5-cyl radial
= Chamberlin
=Chamberlin L-236
Chamberlin L-267
= Changzhou
=(Changzhou Lan Xiang Machinery Works)
Changzhou WZ-6
= Charomskiy
=Source:Gunston
Charomskiy AN.1
Charomskiy ACh-30
Charomskiy ACh-31
Charomskiy ACh-32
Charomskiy ACh-39
Charomskiy M-40
= Chelomey
=Chelomey D-3 Pulse-jet
Chelomey D-5 Pulse-jet
Chelomey D-6 Pulse-jet
Chelomey D-7 Pulse-jet
= Chenu
=Chenu 50-65 hp 4-cyl DD 110 mm × 190 mm (4.3 in × 7.5 in)
Chenu 75 hp 6-cyl in-line 110 mm × 190 mm (4.3 in × 7.5 in)
Chenu 90 hp 4-cyl GD 120 mm × 130 mm (4.7 in × 5.1 in)
Chenu 80-90 hp 6-cyl DD
Chenu 80-90 hp 6-cyl GD
Chenu 200-250 hp 6-cyl DD 150 mm × 120 mm (5.9 in × 4.7 in) (for dirigibles)
= Chengdu
=Chengdu WS-18
= Chevrolair
=(The Arthur Chevrolet Aviation Motors Corporation)
Chevrolair 1923 Water-cooled in-line 4 upright
Chevrolair D-4
Chevrolair D-6
Chevrolair 1923 Air-cooled in-line 4 upright and inverted
= Chevrolet
=Chevrolet Turbo-Air 6 engine
Chinese aero-engines
= Chotia
=Chotia 460
= Christoffersen
=(Christoffersen Aircraft Company)
Christoffersen 120 hp 6-cyl in-line
Christoffersen 120 hp V-12
= Chrysler
=Chrysler IV-2220
Chrysler T36D
= Church
=(Jim Church)
Church J-3 Marathon
Church V-248 V-8
= Cicaré
=Cicaré 4C2T
= Cirrus
=Cirrus I
Cirrus II
Cirrus III
Cirrus Hermes
Cirrus Major
Cirrus Minor
= Cisco Motors
=Cisco Snap 100
= Citroën
=Citroen 2cyl Citroën 2CV – 18 hp
Citroen 4cyl Citroën GS 1.2 – 65 hp at 5,700 rpm
= Clapp's Cars
=Clapp's Cars Spyder Standard
= Clément-Bayard
=Data from:
Clément-Bayard 30 hp 2-cyl HOW 130.2 mm × 111.1 mm (5.125 in × 4.375 in)
Clément-Bayard 29 hp 4-cyl in-line 100 mm × 120 mm (3.94 in × 4.72 in)
Clément-Bayard 40 hp 4-cyl in-line 100 mm × 120 mm (3.94 in × 4.72 in)
Clément-Bayard 100 hp 4-cyl in-line 135 mm × 160 mm (5.3 in × 6.3 in)
Clément-Bayard 118.5 hp 4-cyl in-line 190 mm × 230 mm (7.48 in × 9.06 in)
Clément-Bayard 117.5 hp 6-cyl in-line 155 mm × 185 mm (6.1 in × 7.28 in)
Clément-Bayard 250 hp 6-cyl in-line 155 mm × 200 mm (6.1 in × 7.87 in) (for dirigibles)
Clément-Bayard 50 hp 7-cyl Radial 100 mm × 115 mm (3.94 in × 4.53 in)
Clément-Bayard 300 hp 8-cyl in-line 165 mm × 225 mm (6.5 in × 8.86 in) (for airships)
Clément-Bayard V-16 (for airships)
= Cleone
=Cleone 1930 25 hp 2-cyl hor opp 2 stroke
= Clerget
=(Société Clerget-Blin et Cie / Pierre Clerget)
Source:Lumsden except where noted
= Cleveland
=(Walter C. Willard / Cleveland Aero Engines)
Cleveland 150 hp 6-cyl axial engine 6x130 mm × 150 mm (5 in × 6 in)
= Cleveland
=(Cleveland Engineering Laboratories Company)
Cleveland Weger 400 hp 6-cyl 2-stroke radial 4.25 in × 5 in (108 mm × 127 mm)
= C.L.M.
=(Compagnie Lilloise de Moteurs S.A)
Lille 6As 6-cyl opposed piston 2-stroke diesel (Junkers Jumo 205 licence built)
Lille 6Brs (600 hp)
= CMB
=(Construction Mécanique du Béarn)
See: Béarn
= CNA
=CNA C.II
CNA C.VI I.R.C.43
CNA C.7
CNA D.4
CNA D.VIII
= Coatalen
=Source:Brew
Coatalen 12Vrs-2 diesel
= Colombo
=Colombo C.160
Colombo D.110
Colombo E.150
Colombo S.53
Colombo S.63
= Combi
=Combi 150 hp 6-cyl
= Comet
=(Comet Engine Corp, Madison WI.)
Comet 130hp
Comet 5
Comet 7-D 1928 (ATC 9) = 150 hp 612ci 7RA.
Comet 7-E 1929 (ATC 47) = 165 hp 612ci 7RA.
Comet 7-RA 1928 (ATC 9) = 130 hp 7RA.
= Compagnie Lilloise de Moteurs
=See:C.L.M.
= Conrad
=(Deutsche Motorenbau G.m.b.H. / Robert Conrad)
Conrad C.III – (licence built by N.A.G. as the C.III N.A.G.)
= Continental
== Cors-Air
=(Cors-Air srl, Barco di Bibbiano, Italy)
Cors-Air M19 Black Magic
Cors-Air M21Y
Cors-Air M25Y Black Devil
= Corvair
=(conversions and derivatives of the Chevrolet Turbo-Air 6 engine)
AeroMax Aviation AeroMax 100
Clapp's Cars Spyder Standard
Magsam/Wynne (Del Magsam / William Wynne)
= Cosmos Engineering
=Cosmos Jupiter
Cosmos Lucifer
Cosmos Mercury
Cosmos Hercules 1,000 hp – 18x 6.25 in × 7.5 in (159 mm × 191 mm)
= Coventry Victor
=Coventry Victor Neptune
= Crankless Engines Company
=(Anthony Michell)
Michell XB-4070
= C.R.M.A.
=(Société de construction et de Reparationde Materiel Aéronautique)
C.R.M.A. Type 102
= Curtiss
== Curtiss-Kirkham
=Curtiss-Kirkham K-12
= Curtiss-Wright
=Curtiss-Wright LR25
Curtiss-Wright RJ41 Ramjet
Curtiss-Wright RJ47 Ramjet
Curtiss-Wright RJ51 Ramjet
Curtiss-Wright RJ55 Ramjet
Curtiss-Wright RC2-60 Wankel engine
Curtiss-Wright R-600 Challenger
Curtiss-Wright TJ-32 (Olympus from Bristol, modified by CW)
Curtiss-Wright TJ-38 Zephyr (Americanised Olympus 551)
= Cuyuna
=See:2si
D
= D-Motor
=D-Motor LF26
D-Motor LF39
= D'Hennian
=D'Hennian 10-12 hp rotary
D'Hennian 50 hp 7-cyl rotary
= Daiichi Kosho Company
=Daiichi Kosho DK 472
= Daimler-Benz
=Source:Gunston except where noted
= Damblanc-Mutti
=Damblanc-Mutti 165 hp
Damblanc-Mutti 11-cyl. rotary 220 hp
= Danek
=(Ceskomorarsk-Kolben-Danek & Co.)
Danek Praga 500 hp V-12
= Daniel
=(Daniel Engine Company)
Daniel 7-cyl rotary
= Dansette-Gillet
=Dansette-Gillet Type A 45 hp 4-cyl in-line 105 mm × 160 mm (4.1 in × 6.3 in)
Dansette-Gillet Type C 32 hp 4-cyl in-line 98 mm × 125 mm (3.9 in × 4.9 in)
Dansette-Gillet Type D 70 hp 4-cyl in-line 130 mm × 160 mm (5.1 in × 6.3 in)
Dansette-Gillet 100 hp 6-cyl in-line 130 mm × 160 mm (5.1 in × 6.3 in)
Dansette-Gillet 120 hp V-8 114 mm × 160 mm (4.5 in × 6.3 in)
Dansette-Gillet 200 hp 6-cyl in-line 180 mm × 200 mm (7.1 in × 7.9 in)
= Darracq
=Data from:
Darracq 25 hp O-2 130 mm × 120 mm (5.1 in × 4.7 in)
Darracq 50 hp O-4 130 mm × 120 mm (5.1 in × 4.7 in)
Darracq 43 hp 4-cyl in-line 120 mm × 140 mm (4.7 in × 5.5 in)
Darracq 84 hp 4-cyl in-line 170 mm × 140 mm (6.7 in × 5.5 in)
Darracq 12Da 420 hp V-12
= Dassault
=Dassault MD.30 Viper
Dassault R.7 Farandole
= Day
=(Charles Day)
Day 25 hp 5-cyl
= Dayton
=(Dayton Airplane Engine Co.)
Dayton Bear
= de Dietrich
=de Dietrich 4-cyl in-line
= De Dion-Bouton
=De Dion-Bouton 80 hp V-8 100 mm × 120 mm (3.9 in × 4.7 in)
De Dion-Bouton 100 hp V-8 90 mm × 150 mm (3.5 in × 5.9 in)
De Dion-Bouton 130 hp 12B V-12
De Dion-Bouton 150 hp V-8 125 mm × 150 mm (4.9 in × 5.9 in)
De Dion-Bouton 800 hp X-16 170 mm × 190 mm (6.7 in × 7.5 in)
= de Havilland
=Sources: Piston engines, Lumsden, gas turbine and rocket engines, Gunston.
Piston engines
de Havilland Iris
de Havilland Ghost (V8)
de Havilland Gipsy
de Havilland Gipsy Twelve – known as "Gipsy King" in military service
de Havilland Gipsy Major – also known as Gipsy IIIA
de Havilland Gipsy Minor
de Havilland Gipsy Queen
de Havilland Gipsy Six
Gas turbines
Halford H.1
de Havilland Ghost
de Havilland Gnome
de Havilland Goblin
de Havilland Gyron
de Havilland Gyron Junior
Rockets
de Havilland Spectre
de Havilland Double Spectre – two Spectre engines mounted together
de Havilland Sprite – for rocket-assisted take off
de Havilland Super Sprite – development of Sprite
= de Laval
=de Laval T42
= Deicke
=(Arthur Deicke)
Deicke ADM-7
= Delafontaine
=Delafontaine Diesel – seven-cylinder air-cooled
= Delage
=Delage 12C.E.D.irs
Delage Gvis
= DeltaHawk
=DeltaHawk DH160
DeltaHawk DH180A4
= Demont
=(Messrs Demont, Puteaux, France)
Demont 300 hp 6-cyl double acting rotary 175 mm × 80 mm (6.9 in × 3.1 in)
= Deschamps
=Data from:
(D.J.Deschampsdesigner – Lambert Engine & machine Co., Illinois manufacturer)
Deschamps v-12 inverted 2-stroke diesel
= Detroit Aero
=Detroit Aero 25-30 hp 2OA
= DGEN
=(Price_Induction, Anglet, France)
DGEN 380
DGEN 390
= Diamond Engines
=Diamond Engines GIAE 50R
Diamond Engines GIAE 75R
Diamond Engines GIAE-110R
= Diemech Turbine Solutions
=(DeLand, Florida, United States)
Diemech TJ 100
Diemech TP 100
= Diesel Air
=Diesel Air Dair 100
= DKW
=(A.G.-Werk DKW, Zschopau S.a.)
DKW FL 600W
= Doble-Besler
=Doble-Besler V-2 steam engine
= Dobrotvorskiy
=Dobrotvorskiy MB-100
Dobrotvorskiy MB-102
= Dobrynin
=Source:Gunston
Dobrynin VD-4K
Dobrynin VD-7
= Dongan
=(also known as Harbin Engine Factory)
Dongan HS-7
Dongan HS-8
Dongan WJ-5
Dongan WZ-5
Dongan WZ-6
= Dodge
=Dodge 125 hp 6-cyl rotary Victory 5 in × 6 in (130 mm × 150 mm)
= Dorman
=(W. H. Dorman and Co., Ltd)
Dorman 60-80 hp V-8 4 in × 4.75 in (102 mm × 121 mm)
= Douglas
=Mostly developed from Douglas motorcycle engines
Douglas 350cc
Douglas 500cc
Douglas Dot
Douglas 736cc (some sources 737cc)
Douglas 750cc
Douglas Digit 22 hp at 3,000rpm
Douglas Dryad
Douglas/Aero Engines Sprite/
Aero Engines 1500cc
= Douseler
=Douseler 40 hp 4-cyl in-line
= Dreher
=(Dreher Engineering Company)
Dreher TJD-76 Baby Mamba
= Duesenberg
=Duesenberg Special A
Duesenberg Special A3
Duesenberg H 850 hp V-16 6 in × 7.5 in (150 mm × 190 mm)
Duesenberg 100 hp 4-cyl. direct drive in-line 4.75 in × 7 in (121 mm × 178 mm)
Duesenberg 125 hp 4-cyl. geared in-line 4.75 in × 7 in (121 mm × 178 mm)
Duesenberg 300 hp V-12 4.875 in × 7 in (123.8 mm × 177.8 mm)
Duesenberg A-44 70 hp 4-cyl 4.375 in × 6 in (111.1 mm × 152.4 mm)
= Dufaux
=Dufaux 5-cyl tandem double-acting in-line engine
= Dushkin
=Dushkin D-1-A-1100
Dushkin RD-A-150
Dushkin RD-A-300
Dushkin S-155
Dushkin RD-2M
= Dutheil et Chalmers
=Data from: (some sources erroneously as Duthiel-Chambers)
Dutheil et Chalmers 20 hp O-2 125 mm × 120 mm (4.9 in × 4.7 in)
Dutheil et Chalmers 25 hp O-2 128 mm × 130 mm (5.0 in × 5.1 in)
Dutheil et Chalmers 37.25 hp O-2 110 mm × 300 mm (4.3 in × 11.8 in)
Dutheil et Chalmers 40 hp O-4 125 mm × 120 mm (4.9 in × 4.7 in)
Dutheil et Chalmers 50 hp O-4
Dutheil et Chalmers 60 hp O-6 125 mm × 120 mm (4.9 in × 4.7 in)
Dutheil et Chalmers 72.5 hp O-6 128 mm × 130 mm (5.0 in × 5.1 in)
Dutheil et Chalmers 76 hp O-4
Dutheil et Chalmers 38 hp OP-2
Dutheil et Chalmers 56.5 hp O-3 110 mm × 300 mm (4.3 in × 11.8 in)
Dutheil et Chalmers 75 hp O-4 110 mm × 300 mm (4.3 in × 11.8 in)
Dutheil et Chalmers 97 hp O-4 125 mm × 300 mm (4.9 in × 11.8 in)
Dutheil et Chalmers 100 hp O-4 160 mm × 140 mm (6.3 in × 5.5 in)
Dutheil et Chalmers 72.5 hp O-6 128 mm × 130 mm (5.0 in × 5.1 in)
= Dux
=Dux Hypocycle
= Dyna-Cam
=Dyna-Cam
E
= Easton
=Data from:
Easton 50 hp V-8
Easton 75 hp V-8
= ECi
=ECi O-320
ECi Titan X320
ECi Titan X340
ECi Titan X370
= Ecofly
=(Ecofly GmbH, Böhl-Iggelheim, Germany)
Ecofly M160
= Edelweiss
=Edelweiss 75 hp 6-cyl fixed piston radial 115 mm × 120 mm (4.5 in × 4.7 in)
Edelweiss 125 hp 6-cyl fixed piston radial 115 mm × 120 mm (4.5 in × 4.7 in)
= Eggenfellner Aircraft
=Eggenfellner E6
= E.J.C.
=E.J.C. 60 hp 6-cyl rotary 100 mm × 100 mm (3.9 in × 3.9 in)
E.J.C. 10-cyl rotary 100 mm × 100 mm (3.9 in × 3.9 in)
= Elbridge
=(Elbridge Engine Company)
Elbridge A 2IW 6-10 hp 3.75 in × 3.5 in (95 mm × 89 mm)
Elbridge C 3IW 18-30 hp 4.625 in × 4.5 in (117.5 mm × 114.3 mm)
Elbridge 4-cyl 4IW 4.625 in × 4.5 in (117.5 mm × 114.3 mm)
Elbridge Featherweight 3-cyl 3IW 30-40 hp 4.625 in × 4.5 in (117.5 mm × 114.3 mm)
Elbridge Featherweight 4-cyl 4IW 40-60 hp 4.625 in × 4.5 in (117.5 mm × 114.3 mm)
Elbridge Featherweight 6-cyl 6IW 60-90 hp 4.625 in × 4.5 in (117.5 mm × 114.3 mm)
Elbridge Aero Special 4IW 50-60 hp 4.625 in × 4.5 in (117.5 mm × 114.3 mm)
= Electravia
=Electravia GMPE 102
Electravia GMPE 104
Electravia GMPE 205
= Electric Aircraft Corporation
=Electric Aircraft Corporation Electra 1
= Elektromechanische Werke
=Elektromechanische Werke Taifun rakatenmotor
Elektromechanische Werke Wasserfall rakatenmotor
= Elizalde
=Source:Gunston
Elizalde A
Elizalde A6?
Elizalde Dragon
Elizalde D V
Elizalde D VII
Elizalde D IX B.
Elizalde D IX M.R.
Elizalde D IX C.R.
Elizalde Super Dragon
Elizalde S.D.M
Elizalde S.D.M.R.
Elizalde S.D.C
Elizalde S.D.C.R.
Elizalde Sirio
Elizalde Tigre IV
Elizalde Tigre VI
Elizalde Tigre VIII
Elizalde Tigre XII
= Ellehammer
=Elllehammer 3-cyl radial
Elllehammer 5-cyl radial
Elllehammer rotary engine
= Emerson
=Emerson 100 hp 6-cyl
= EMG
=(EMG Engineering Company / Eugene M. Gluhareff)
Gluhareff G8-2-20
Gluhareff G8-2-80
Gluhareff G8-2-130
Gluhareff G8-2-250
= Emrax
=Emrax 2
Emrax 207
Emrax 228
Emrax 268
= Endicott
=Endicott 60 hp 3-cyl 2-stroke
= Engine Alliance
=Engine Alliance GP7000
= Engineered Propulsion Systems
=(Engineered Propulsion Systems)
Engineered Propulsion Systems Graflight V-8
= Engineering Division
=Engineering Division W-1 750 hp W-18 5.5 in × 6.5 in (140 mm × 170 mm)
Engineering Division W-1A-18
Engineering Division W-2779
Engineering Division W-2 1000 hp W-18 6.5 in × 7.5 in (170 mm × 190 mm)
Engineering Division 350 hp 9-cyl radial 5.875 in × 6 in (149.2 mm × 152.4 mm)
= ENMA
=(Empresea Nacional de motores de Aviacion S.A.)
ENMA Alcion
ENMA Beta
ENMA Flecha
ENMA Sirio
ENMA Tigre
ENMA A-1 Alcion
ENMA F-IV Flecha
ENMA Flecha F.1
ENMA Sirio S2
ENMA Sirio S3
ENMA S-VII Sirio
ENMA 4.(2L)-00-93
ENMA 7.E-CR.15-275
ENMA 7.E-C20-500
ENMA 7.E-CR20-600
ENMA 7.E-CR.15-275
ENMA 9.E-C.29-775
= E.N.V.
=E.N.V. Type A
E.N.V. Type C
E.N.V. Type D
E.N.V. Type F/FA
E.N.V. Type H
E.N.V. Type T
E.N.V. 40 hp V-8
E.N.V. 62 hp V-8
E.N.V. 75 hp V-8
E.N.V. 100 hp V-8
E.N.V. 1914 100 hp V-8
E.N.V. 1909 25/30 hp O-4
E.N.V. 1910 30 hp O-4
= ERCO
=ERCO IL-116
= Esselbé
=Esselbé 65 hp 7-cyl rotary 110 mm × 120 mm (4.33 in × 4.72 in)
= Etoile
=Etoile 400 hp
= EuroJet
=Eurojet EJ200
= Europrop
=Europrop TP400
F
= F&S
=F&S K 8 B
= Fahlin
=Fahlin Plymouth conversion
= Fairchild
=For Ranger and Fairchild Ranger engines see: Ranger
Source:Gunston except where noted
Fairchild Caminez 4-cylinder
Fairchild Caminez 8 cylinder
Fairchild J44
Fairchild J63
Fairchild J83
Fairchild T46
= Fairdiesel
=Fairdiesel barrel engine
= Fairey
=None of Fairey Aviation Company's own engine designs made it to production.
Felix – imported Curtiss D-12 engines
P.12 Prince – V-12
P.16 Prince – H-16
P.24 Monarch also known as Prince 4
= Falconer
=(Ryan Falconer Racing Engines)
Falconer L-6
Falconer V-12
= Farcot
=Farcot 8-10 hp V-2
Farcot Fan-6
Farcot 100-110 hp V-8
Farcot 30 hp 8cyl radial
Farcot 65 hp 8cyl radial 105 mm × 120 mm (4.13 in × 4.72 in)
Farcot 100 hp 8cyl radial
= Farina
=(S.A. Stabilimenti Farina)
Farina Algol
Farina Aligoth
Farina T.58
= Farman
=Source:Liron
Note: Farman engine designations differ from other French manufacturers in using the attributes as the basis of the designation, thus; Farman 7E (7-cyl radial E – Etoile / Star / Radial) or Farman 12We (W-12 fifth type – the e is not a variant or sub-variant it is the type designator). As usual there are exceptions such as the 12Gvi, 12B, 12C and 18T.
= Fasey
=Fasey 200 hp V-12 127 mm × 127 mm (5.0 in × 5.0 in)
= Fatava
=Source:
Fatava 45 hp 4IL 110 mm × 120 mm (4.3 in × 4.7 in)
Fatava 90 hp V-8 110 mm × 120 mm (4.3 in × 4.7 in)
Fatava 180 hp X-16 110 mm × 120 mm (4.3 in × 4.7 in)
= Faure and Crayssac
=Faure and Crayssac 80 hp rotary
Faure and Crayssac 350 hp 6-cyl. 2st barrel engine 100 mm × 180 mm (3.9 in × 7.1 in)
= Fedden
=Designed post war by Roy Fedden formerly of Cosmos Engineering and Bristol. Roy Fedden Ltd went into liquidation in 1947
Fedden Cotswold – design only
Fedden 6A1D-325 (185 hp 6HO)
Fedden G6A1D-325 (geared) 6AID-325?
= Fiat
=Data from:Italian Civil & Military Aircraft 1930–1945
= Firewall Forward Aero Engines
=Firewall Forward CAM 100
Firewall Forward CAM 125
= FKFS
=FKFS Gruppen-Flugmotor A
FKFS Gruppen-Flugmotor B?
FKFS Gruppen-Flugmotor C
FKFS Gruppen-Flugmotor D
FKFS Gruppen-Flugmotor 37.6 L 48-cyl
= Flader
=Source:Geen and Cross
Flader J55 Type 124 Lieutenant
Flader T33 Type 125? Brigadier
= Fletcher
=Fletcher 5 hp
Fletcher 9 hp
Fletcher Empress 50 hp rotary
= FNM
=FNM R-760
FNM R-975
= Ford
=Ford O-145
4 Cylinder X engine
8 Cylinder X engine
Ford PJ31 Pulsejet, see Republic-Ford JB-2
Ford V-1650 Liberty V-12
= Fox
=(Dean Manufacturing Company, Newport, Kentucky)
Fox 45 hp 3-cyl in-line 2-stroke 4 in × 4 in (100 mm × 100 mm)
Fox 36 hp 4-cyl in-line 2-stroke 3.5 in × 3.5 in (89 mm × 89 mm)
Fox 60 hp 4-cyl in-line 2-stroke 4 in × 4 in (100 mm × 100 mm)
Fox 90 hp 6-cyl in-line 2-stroke 4 in × 4 in (100 mm × 100 mm)
Fox 200 hp 8-cyl in-line 2-stroke 6 in × 6 in (150 mm × 150 mm)
Fox De-luxe 50 hp 4-cyl in-line 2-stroke 4.75 in × 4.25 in (121 mm × 108 mm)
= Franklin
=Source:Gunston.
= Fredrickson
=(World's Motor Company, Bloomington, Illinois)
Fredrickson Model 5a
Fredrickson Model 10a
= Frontier
=(Frontier Iron Works, Buffalo, New York)
Frontier 35 hp 4-cyl in-line 4.125 in × 4.75 in (104.8 mm × 120.7 mm)
Frontier 55 hp V-8 4.125 in × 4.75 in (104.8 mm × 120.7 mm)
= Fuji
=Fuji JO-1 (Nippon JO-1)
Fuji J3-1 (Nippon J3-1)
= Fuscaldo
=Fuscaldo 90 hp
= Funk
=(Akron Aircraft Company / Funk Aircraft Company)
Funk Model E
G
= Gaggenau
=Gaggenau 4-cyl in-line
= Gajęcki
=Gajęcki XL-Gad
= Galloway
=(Galloway Engineering Company ltd.)
Galloway Adriatic 6IL 145 mm × 190 mm (5.7 in × 7.5 in)
Galloway Atlantic 145 mm × 190 mm (5.7 in × 7.5 in)(master rod)
= Garrett
=Source:Gunston except where noted
Now under Honeywell management/design/production
= Garuff
=Garuff A – aircraft diesel engine
= GE Honda Aero Engines
=GE Honda HF120
= Geiger Engineering
=Geiger HDP 10
Geiger HDP 12
Geiger HDP 13.5
Geiger HDP 16
Geiger HDP 25
Geiger HDP 32
Geiger HDP 50
= GEN Corporation
=GEN 125
= General Aircraft Limited
=General Aircraft Monarch V-4
General Aircraft Monarch V-6
= General Electric
== General Electric/Rolls-Royce
=General Electric/Rolls-Royce F136
= General Motors Research
=General Motors Research X-250
= General Ordnance
=(General Ordnance Company, Derby, Conn.)
General Ordnance 200 hp V-8 4.75 in × 6.5 in (121 mm × 165 mm)
= Giannini
=(Pulsejets)
Giannini PJ33
Giannini PJ35
Giannini PJ37
Giannini PJ39
= Glushenkov
=Source:Gunston.
Glushenkov TVD-10
Glushenkov TVD-20
Glushenkov GTD-3
= Gnome et Rhône
=Gnome et Rhône except where noted
Im French engine designations —even— sub-series numbers (for example Gnome-Rhône 14N-68) rotated anti-clockwise (LH rotation) and were generally fitted on the starboard side, —odd numbers— (for example Gnome-Rhône 14N-69) rotated clockwise (RH rotation) and were fitted on the port side.
Gnome
Gnome 1906 25 hp rotary – prototype Gnome rotary engine
Gnome 34 hp 5-cyl rotary 100 mm × 100 mm (3.9 in × 3.9 in)
Gnome 123 hp 14-cyl rotary 110 mm × 120 mm (4.33 in × 4.73 in)
Gnome 1907 50 hp
Gnome 7 Gamma 70 hp 130 mm × 120 mm (5.1 in × 4.7 in)
Gnome 14 Gamma-Gamma
Gnome 9 Delta 100 hp 124 mm × 150 mm (4.9 in × 5.9 in)
Gnome 18 Delta-Delta 200 hp
Gnome 7 Lambda 80 hp 124 mm × 140 mm (4.9 in × 5.5 in)
Gnome 14 Lambda-Lambda 160 hp
Gnome 7 Sigma 60 hp 120 mm × 120 mm (4.7 in × 4.7 in)
Gnome 14 Sigma-Sigma 120 hp
Gnome 7 Omega 50 hp 110 mm × 120 mm (4.3 in × 4.7 in)
Gnome 14 Omega-Omega 100 hp
Gnome Monosoupape 7 Type A 80 hp 110 mm × 150 mm (4.3 in × 5.9 in)
Gnome Monosoupape 9 Type B-2 100 hp 110 mm × 150 mm (4.3 in × 5.9 in)
Gnome Monosoupape 11 Type C 190 hp 115 mm × 170 mm (4.5 in × 6.7 in)
Gnome Monosoupape 9 Type N 165/170 hp 115 mm × 170 mm (4.5 in × 6.7 in)
Gnome Monosoupape 18 Type Double-N 300 hp
Gnome 600 hp 20-cyl radial 140 mm × 170 mm (5.5 in × 6.7 in)
Gnome et Rhône
Gnome-Rhône 5B – licence built Bristol Titan
Gnome-Rhône 5K Titan – licence built Bristol Titan
Gnome-Rhône 7K Titan Major – 7-cylinder development of 5K
Gnome-Rhône 9A Jupiter – licence built Bristol Jupiter
Gnome-Rhône 9K Mistral
Gnome-Rhône 14K Mistral Major
Gnome-Rhône 14M Mars
Gnome-Rhône 14N
Gnome-Rhône 14P
Gnome-Rhône 14R
Gnome-Rhône 18L
Gnome-Rhône 18R
Gnome-Rhône 28T
= Gobe
=Gobe 2-stroke engine
= Gobrón-Brillié
=(Gustave Gobrón and Eugène Brillié)
Gobrón-Brillié 54 hp X-8 90 mm × 160 mm (3.5 in × 6.3 in) (fitted to 1910 Voisin de-Caters)
Gobrón-Brillié 102 hp X-8 120 mm × 200 mm (4.7 in × 7.9 in)
= Goebel
=(Georg Goebel of Darmstadt) / (ver Gandenbergesche Maschinen Fabrik)
Goebel 2-cyl. 20/25 hp HOA
Goebel Type II 100/110 hp 7-cyl. rotary 138 mm × 150 mm (5.4 in × 5.9 in)
Goebel Type III 200/230 hp 9-cyl. rotary 138 mm × 290 mm (5.4 in × 11.4 in)
Goebel Type V 50/60 hp 7-cyl. rotary 105 mm × 105 mm (4.1 in × 4.1 in)
Goebel Type VI 30/40 hp 7-cyl. rotary 94 mm × 95 mm (3.7 in × 3.7 in)
Goebel 170 hp 9-cyl rotary
Goebel 170 hp 11-cyl rotary
Goebel 180 hp 11-cyl rotary
= Grade
=Grade 16 hp V-4 2-stroke
= Great Plains Aircraft Supply
=Great Plains Type 1 Front Drive
= Green
=Green 32hp 4-cyl in-line 4.13 in × 4.73 in (105 mm × 120 mm)
Green 60hp 4-cyl in-line 5.52 in × 5.75 in (140 mm × 146 mm)
Green 82 hp V-8 4.57 in × 5.52 in (116 mm × 140 mm)
Green C.4
Green D.4
Green E.6
Green 150 hp 6-cyl in-line 5.59 in × 7.01 in (142 mm × 178 mm)
Green 260-275 hp V-12 1914
Green 300 hp V-12 5.59 in × 7.01 in (142 mm × 178 mm)
Green 450 hp W-18 5.59 in × 7.01 in (142 mm × 178 mm) 1914
= Grégoire-Gyp
=(Pierre Joseph Grégoire / Automobiles Grégoire)
Grégoire-Gyp 26 hp 4-cyl in-line (3-cyl?)92 mm × 140 mm (3.62 in × 5.52 in)
Grégoire-Gyp 40 hp 4-cyl inverted in-line
Grégoire-Gyp 51 hp 4-cyl in-line 130 mm × 140 mm (5.12 in × 5.52 in)
Grégoire-Gyp 70 hp
= Grey Eagle
=Grey Eagle 40 hp 4-cyl in-line – 4.25 in × 4.5 in (108 mm × 114 mm)
Grey Eagle 60 hp 6-cyl in-line – 4.25 in × 4.5 in (108 mm × 114 mm)
Grey Eagle 50 hp 4-cyl in-line – 4 in × 4.5 in (100 mm × 110 mm)
= Grizodubov
=(S.V. Grizodubov)
Grizodubov 1910 40 hp 4-cyl.
= Grob
=Grob 2500
Grob 2500E
= Guiberson
=(Guiberson Diesel Engine Company)
Source:Gunston except where noted
Guiberson A-918
Guiberson A-980 – 210 hp (160 kW)
Guiberson A-1020 – 340 hp (250 kW)
Guiberson T-1020 – 210 hp (160 kW) (tank engine?)
Guiberson T-1400 – 250 hp (190 kW) (tank engine)
= Guizhou
=(Guizhou Liyang Aircraft Engine Company)
Guizhou WP-13
Guizhou WS-13 ("Taishan")
= Gyro
=Data from:
Gyro 50 hp 7-cyl rotary Old Gyro 4.3125 in × 4.75 in (109.54 mm × 120.65 mm)
Gyro Model J 5-cyl 50 hp Duplex
Gyro Model K 7-cyl 50 hp Duplex
Gyro Model L 9-cyl 50 hp Duplex
H
= Haacke
=(Haacke Flugmotoren)Source: RMV
Haacke HFM 2 – 2cyl. 25/28 hp 112 mm × 140 mm (4.4 in × 5.5 in)
Haacke HFM 2a – 2cyl. 35 hp 120 mm × 140 mm (4.7 in × 5.5 in)
Haacke HFM 3 – 3cyl. fan 40 hp
Haacke 55/60 hp 5-cyl. radial
Haacke 60/70 hp radial
Haacke 90 hp 7-cyl. radial
Haacke 120 hp 10-cyl. radial
= HAL
=See:Hindustan Aeronautics Limited
= Hall-Scott
=Hall-Scott 60 hp
Hall-Scott A-1
Hall-Scott A-2
Hall-Scott A-3
Hall-Scott A-4
Hall-Scott A-5
Hall-Scott A-5a
Hall-Scott A-7
Hall-Scott A-7a
Hall-Scott A-8
Hall-Scott L-4
Hall-Scott L-6
= Hallett
=(Hallett Aero Motors Corp, Inglewood CA.)
Hallett H-526 7-cyl radial 130 hp
= Hamilton
=Hamilton DOHC V-8
= Hamilton Sundstrand
=Sundstrand T100
= Hansa-Lloyd
=(Hansa-LLoyd Werke AG)
Hansa-LLoyd V-16
= Hansen-Snow
=(W.G. Hansen & L.L. Snow, Pasadena, CA)
Hansen-Snow 35 hp 4-cyl in-line 4 in × 4.5 in (100 mm × 110 mm)
= Hardy-Padmore
=Hardy-Padmore 100 hp 5-cyl rqdial 4 in × 4 in (100 mm × 100 mm)
= Harkness
=(Donald (Don) Harkness, built by Harkness & Hillier Ltd)
Harkness Hornet
= Harriman
=(Harriman Motors Company, South Glastonbury, Conn.)
Harriman 30 hp 4-cyl in-line
Harriman 60 hp 4-cyl in-line 5 in × 5 in (130 mm × 130 mm)
Harriman 100 hp 4-cyl in-line 5 in × 5 in (130 mm × 130 mm)
= Harris-Gassner
=Harris-Gassner 50/60 hp V-8
= Harroun
=Harroun 24 hp 2-cyl HOA 4 in × 4 in (100 mm × 100 mm)
= Hart
=Hart 150 hp 9-cyl rotary 5 in × 6 in (130 mm × 150 mm)
Hart 156 hp 9-cyl radial (?) 6 in × 5 in (150 mm × 130 mm)
= Hartland
=Hartland 125 hp
= H.C.G.
=(Les Établissements lipton)
H.C.G. 2-cyl HOA
= Heath
=(Heath Aircraft Corp)
Heath 4-B
Heath 4-C
Heath B-4
Heath B-12
Heath C-2
Heath C-3
Heath C-6
= Heath
=(Heath Aerial Vehicle Company, Chicago Illinois)
Heath 25/30 hp 4-cyl in-line
= Heath-Henderson
=Heath-Henderson B-4
= Heinkel-Hirth
=Source:
= Helium
=From Flight
Helium 45 hp 3-cyl radial
Helium 60 hp 3-cyl radial
Helium 75 hp 5-cyl radial
Helium 100 hp 5-cyl radial
Helium 45 hp 3-cyl rotary 2-stroke
Helium 60 hp 3-cyl rotary 2-stroke
Helium 100 hp 5-cyl rotary 2-stroke
Helium 120 hp 6-cyl rotary 2-stroke
Helium 200 hp 10-cyl rotary 2-stroke
Helium 120 hp 6-cyl rotary 2-stroke
Helium 200 hp 10-cyl rotary 2-stroke
= Hendee
=Hendee Indian 60/65 hp V-8 4 in × 4.5 in (100 mm × 110 mm)
Hendee Indian 50 hp 7-cyl rotary 4.375 in × 4.875 in (111.1 mm × 123.8 mm)
Hendee Indian 60 hp 9-cyl rotary
= Henderson
=Henderson 6 hp 4-cyl in-line 2.375 in × 2.1875 in (60.33 mm × 55.56 mm)
= Herman
=Herman 45 hp
Herman 70 hp
= Hermes Engine Company
=Hermes Cirrus
= Hess
=(Aubrey W. Hess / Alliance Aircraft Corporation)
Hess Warrior
= Hewland
=Hewland AE75
= Hexatron Engineering
=Hexadyne P60
Hexadyne O-49
= Hiero
=(Otto Hieronimus – designer – several manufacturers)
= Hill Helicopters
=Hill Helicopters GT50
= Hiller
=Hiller 1910
Hiller 30 hp
Hiller 60 hp
Hiller 90 hp
= Hiller Aircraft
=Hiller 8RJ2B – ramjet for the Hiller YH-32 Hornet
= Hilz
=Hilz 45/50 hp 4-cyl in-line 120 mm × 130 mm (4.7 in × 5.1 in)
Hilz 50/55 hp 4-cyl in-line 120 mm × 130 mm (4.7 in × 5.1 in)
Hilz 65 hp 4-cyl in-line 124 mm × 140 mm (4.9 in × 5.5 in)
= Hindustan Aeronautics Limited
=HAL HPE-2
HAL PTAE-7
HAL HJE-2500
HAL HTFE-25
HAL HTSE-1200
HAL HPE-90
HAL P.E.90H
HAL HJE-2500
GTRE GTX-35VS Kaveri
PTAE-7
GTSU-110
= Hiro
=Hiro Type 14
Hiro Type 61
Hiro Type 90
Hiro Type 91
Hiro Type 94
= Hirth
=Hirth Motoren GmbH was merged with Heinkel to make "Heinkel-Hirth" in 1941.
= Hispano-Suiza
== Hitachi
=Source:Gunston.
Hitachi Ha12 (Army Type 95 150 hp Air Cooled Radial)
Hitachi Ha13 (Army Type 95 350 hp Air Cooled Radial)
Hitachi Ha13a (Army Type 98 450 hp Air Cooled Radial)
Hitachi Ha42
Hitachi Ha47
Hitachi Ha-51 (unified designation)
Hitachi GK2
Hitachi GK4
Hitachi GK2 Amakaze
Hitachi Kamikaze
Hitachi Hatsukaze
Hitachi Jimpu
Hitachi Tempu
Army Type 95 150 hp Air Cooled Radial (Ha12 – Hatsudoki system)
Army Type 95 350 hp Air Cooled Radial (Ha13 – Hatsudoki system)
Army Type 98 450 hp Air Cooled Radial (Ha13a – Hatsudoki system)
Army Type 4 110hp Air Cooled Inline (Ha47 – Hatsudoki system / GK4 – Navy system)
= HKS
=HKS 700E
HKS 700T
= Hodge
=Hodge 320 hp 18-cyl radial 4 in × 4 in (100 mm × 100 mm)
= Hofer
=(Al Hofer)
Hofer 10-12 hp 4cyl in-line 3.125 in × 3.75 in (79.4 mm × 95.3 mm)
= Holbrook
=(Holbrook Aero Supply)
Holbrook 35 hp
Holbrook 50 hp
= Honda
=Honda HFX-01
Honda HFX20
Honda HF118
GE Honda HF120
= Honeywell
=Honeywell ALF502
Honeywell HTF7000
Honeywell LF507
Honeywell LTS101
Honeywell TPE-331
Honeywell TFE731
Honeywell FX5
= Hopkins & de Kilduchevsky
=Hopkins & de Kilduchevsky 30-40 hp
Hopkins & de Kilduchevsky 60-80 hp
= Howard
=Howard 120 hp 6-cyl in-line 150 mm × 105 mm (5.9 in × 4.1 in)
= Hudson
=(John W Hudson)
Hudson 100 hp 10-cyl radial 4.3125 mm × 4.75 mm (0.16978 in × 0.18701 in)
= Hummel
=(James Morris (Morry) Hummel of Bryan, Ohio)
Hummel 28 hp 1/2 VW
Hummel 32 hp 1/2 VW
Hummel 45 hp 1/2 VW
Hummel 50 hp VW
Hummel 60 hp VW
Hummel 70 hp VW
Hummel 85 hp VW
= HuoSai
=(HuoSai – Piston engine)
HuoSai HS-5
HuoSai HS-6
HuoSai HS-7
HuoSai HS-8
= Hurricane
=Hurricane C-450 (8-cyl 2-stroke radial)
I
= IAE
=IAE V2500
IAE V2500SF SuperFan
= I.Ae.
=I.Ae. 16 El Gaucho
I.Ae. 19R El Indio
IA IAO-1600-RX/1
= IAME
=(Ital-American Motor Engineering)
KFM 104
KFM 105
KFM 107
KFM 112M
= IAR
=IAR K7-I 20
IAR K9-I C40
IAR K14
IAR 4-G1
IAR 6-G1
IAR LD 450
IAR DB605
= ICP
=ICP M09
= IHI
== IL
=(Instytut Lotnictwa – Aviation Institute)
IL SO-1
IL SO-3
IL K-15
= ILO
=ILO F 12/400
= Imaer
=Imaer 1000
Imaer 2000
= Imperial
=(Imperial Airplane Society)
Imperial 35-70 hp (various 6cyl rotary engines)
Imperial 100 hp (12cyl rotary)
= In-Tech
=(In-Tech International Inc.)
In-Tech Merlyn
= Indian
=See: Hendee
= Innodyn
=(Innodyn L.L.C.)
Innodyn TAE165
Innodyn TAE185
Innodyn TAE205
Innodyn TAE255
Innodyn 165 TE
Innodyn 185 TE
Innodyn 205 TE
Innodyn 255 TE
= International
=Data from:
International 21.5 hp 4-cyl rotary 3.74 in × 2.52 in (95 mm × 64 mm)
International 66 hp 6-cyl rotary 5 in × 3.98 in (127 mm × 101 mm)
= Ion
=(Gabriel Ion)
Ion airship steam engine
= Irwin
=(Irwin Aircraft Co)
Irwin 79 Meteormotor (a.k.a. X)
= Isaacson
=(Isaacson Engine (Motor Supply Co.) / R.J. Isaacson)
Isaacson 45 hp 7-cyl. radial
Isaacson 50 hp
Isaacson 60 hp
Isaacson 6-cyl. radial
Isaacson 50 hp 7-cyl. radial
Isaacson 65 hp 7-cyl. radial
Isaacson 100 hp 14-cyl. radial
Isaacson 100 hp 9-cyl. rotary
Isaacson 200 hp 18-cyl. rotary
= Ishikawajima
=See: IHI
= Isotov
=Source:Gunston
Isotov GTD-350
Isotov TV-2-117
Isotov TV-3-117
Isotov TVD-850
= Isotta Fraschini
== Ivchenko
=Source:Gunston.
= IWL
=See:Pirna
J
= Jabiru
=Jabiru 1600
Jabiru 2200
Jabiru 3300
Jabiru 5100
= Jack & Heinz
=Jack & Heinz O-126
= Jacobs
=Source:Gunston except where noted
Jacobs 35 hp
Jacobs B-1
Jacobs L-3
Jacobs L-4
Jacobs L-5
Jacobs L-6
Jacobs LA-1
Jacobs LA-2
Jacobs O-200
Jacobs O-240A
Jacobs O-240L
Jacobs O-360A (air-cooled)
Jacobs O-360L (liquid-cooled)
Jacobs R-755
Jacobs R-830
Jacobs R-915
= Jaenson
=Jaenson 300 hp V-8 140 mm × 180 mm (5.51 in × 7.09 in)
= Jalbert-Loire
=Jalbert-Loire 4-cyl. 160 hp
Jalbert-Loire 6-cyl. 235 hp
Jalbert-Loire 16-H – 16-cyl. 600 hp
= Jameson
=(Jameson Aero Engines Ltd.)
Jameson FF-1 – 1940s horizontally opposed, four cylinder (106 hp)
= Janowski
=(Jaroslaw Janowski)
Janowski Saturn 500
= J.A.P.
=Data from:
J.A.P. 1909 9 hp 2-cyl.
J.A.P. 1909 20 hp 4-cyl.
J.A.P. 38 hp V-8 (air-cooled) 3.35 in × 3.74 in (85 mm × 95 mm)
J.A.P. 45 hp V-8 (water-cooled) 3.54 in × 4.33 in (90 mm × 110 mm)
J.A.P. 1910 40 hp V-8
J.A.P. 8-cyl.
Aeronca-J.A.P. J-99
= Japanese rockets and Pulse-jets
=Type4 I-Go Model-20 (Rocket)
Tokuro-1 Type 2 (Rocket)
= Javelin
=Javelin Ford 230hp conversion
= Jawa
=Jawa 1000
Jawa M-150
= Jendrassik
=Jendrassik Cs-1
= J.E.T
=(James Engineering Turbines Ltd)
J.E.T Cobra
= JetBeetle
=JetBeetle Tarantula H90
JetBeetle Locust H150R
JetBeetle Mantis H250
= Jetcat
=Jetcat P160
Jetcat P200
Jetcat P300
Jetcat P400
= Johnson
=Johnson Aero 75 hp V-6 5 in × 4 in (130 mm × 100 mm)
Johnson Aero 100 hp V-8 5 in × 4 in (130 mm × 100 mm)
Johnson Aero 150 hp V-12 5 in × 4 in (130 mm × 100 mm)
= JLT Motors
=(Boos, Seine-Maritime, France)
JLT Motors Ecoyota 82
JLT Motors Ecoyota 100
= JPX
=JPX 4TX75
JPX D160
JPX PUL 212
JPX PUL 425
JPX D-320
= Junkers
=Source:Kay
K
= Kalep
=(Fyodor Grigoryevich Kalep)
Kalep 1911 4-cyl 2-stroke
Kalep-60
Kalep-80
Kalep-100
= Kawasaki
=Source:Gunston except where noted
Kawasaki Ha9 – licence-built BMW VI for IJAAF
Kawasaki Ha40 – licence-built Daimler-Benz DB 601A for IJAAF
Kawasaki Ha-60
Kawasaki Ha140
Kawasaki Ha201 – twin Ha40s with common gearbox
Kawasaki KAE-240
Kawasaki 440 engine.
Kawasaki KJ12
Kawasaki KT5311A
= Kelly
=Kelly 200 hp 2-stroke 4-cyl inline 6.5 in × 6.3 in (170 mm × 160 mm)
= Kemp
=(a.k.a. Grey Eagle)
Kemp D-4
Kemp E-6
Kemp G-2
Kemp H-6 (55 hp 6IL) 4.25 in × 4.5 in (108 mm × 114 mm)
Kemp I-4 (35 hp 4IL) 4.25 in × 4.5 in (108 mm × 114 mm)
Kemp J-8 (80 hp V-8) 4.25 in × 4.75 in (108 mm × 121 mm)
Kemp K-2
Kemp M-2
Kemp O-101
Kemp-Henderson 27 hp
= Ken Royce
=LeBlond Aircraft Engine Corporation was sold to Rearwin Airplanes in 1937 and renamed Ken-Royce.
Ken-Royce 5E – LeBlond 70-5E
Ken-Royce 5G – LeBlond 90-5G
Ken-Royce 7F- developed from LeBlond 7DF
Ken-Royce 7G
= Kessler
=Kessler 200 hp 4.75 in × 5 in (121 mm × 127 mm)
Kessler 6C-400 5.5 in × 6 in (140 mm × 150 mm)
= KFM
=(KFM (Komet Flight Motor) Aircraft Motors Division of Italian American Motor Engineering)
KFM 107
KFM 112M
= Khatchaturov
=Khatchaturov R-35
= KHD
=Humboldt-Deutz 6 cyl. in-line diesel
Klöckner-Humboldt-Deutz diesel 8 cyl. rotary DZ 700?
Klöckner-Humboldt-Deutz DZ 700
Klöckner-Humboldt-Deutz DZ 710 16-cylinder horizontally opposed diesel
Klöckner-Humboldt-Deutz DZ 720 32-cylinder H-block version of the 710
KHD T112 (APU)
KHD T117
KHD T216
KHD T312
KHD T317
Klöckner-Humboldt-Deutz T53-L-13A
= Kiekhaefer
=Kiekhaefer O-45
Kiekhaefer V-105
= Kimball
=Kimball Beetle K
Kimball Gnat M
= King
=(Chas. B. King)
King 550 hp V-12 5.5 in × 7 in (140 mm × 180 mm)
= King-Bugatti
=King-Bugatti U-16
= Kinner
=Source:Gunston except where noted
Kinner 60 hp
Kinner B-5
Kinner B-54
Kinner C-5
Kinner C-7
Kinner SC-7
Kinner K-5
Kinner O-550
Kinner O-552
Kinner R-5
Kinner R-53
Kinner R-55
Kinner R-56
Kinner R-370
Kinner R-440
Kinner R-540
Kinner R-720
Kinner R-1045-2
= Kirkham
=Kirkham 50 hp 4IL (C-4?) 4.3125 in × 5.125 in (109.54 mm × 130.18 mm)
Kirkham 75-85 hp
Kirkham 110 hp
Kirkham 180 hp 9-cyl. radial
Kirkham B-4 4.125 in × 4.75 in (104.8 mm × 120.7 mm)
Kirkham B-6 4.125 in × 4.75 in (104.8 mm × 120.7 mm)
Kirkham B-12
Kirkham BG-6 (geared) 4.3125 in × 5.125 in (109.54 mm × 130.18 mm)
Kirkham C-4
Kirkham K-12
= Kishi
=Kishi 70 hp V-8 96 mm × 120 mm (3.8 in × 4.7 in)
= Klimov
=Source:Gunston
= Knox
=(Knox Motors Company, Springfield Mass.)
Knox 300 hp V-12 4.75 in × 7 in (121 mm × 178 mm)
Knox H-106
Knox R-266
= Koerting
=Koerting 65 hp V-8 116 mm × 126 mm (4.6 in × 5.0 in)
Koerting 185 hp V-8 110 mm × 140 mm (4.3 in × 5.5 in)
Koerting 250 hp V-12 120 mm × 140 mm (4.7 in × 5.5 in)
= Kosoku
=(Kosokudo Kikan KK)
Kosoku KO-4
= Kolesov
=Kolesov RD-36-51
Kolesov VD-7
= Köller
=(Dr. Kröber und Sohn GmbH, Treuenbrietzen)
Köller M3
= König
=(Compact Radial Engines)
König SC 430
König SD 570
= Konrad
=(Oberbayische Forschungsanhalt Dr. Konrad)
Konrad 109-613
Konrad Enzian IV rakatenmotor
Konrad Enzian V rakatenmotor
Konrad Rheintochter R 3 rakatenmotor
= Körting
=Körting Kg IV V-8
Körting 8 SL
= Kossov
=Kossov MG-31F
= Kostovich
=(O.S. Kostovich)
Kostovich 2-cyl airship engine
Kostovich 80 hp 8-cyl airship engine
= Krautter
=(Dipl. Ing. Willi Krautter)
Krautter-Leichtflugmotor
= Kroeber
=(Doktor Kroeber & Sohn G.m.b.H.)
Kroeber M4
= Kruk
=Kruk rotary 130 mm × 130 mm (5.1 in × 5.1 in)
= Kuznetsov
=Source:Gunston except where noted
Kuznetsov Type 022
Kuznetsov NK-2
Kuznetsov NK-4
Kuznetsov NK-6
Kuznetsov NK-8
Kuznetsov NK-12
Kuznetsov NK-22
Kuznetsov NK-25
Kuznetsov NK-32
Kuznetsov NK-86
Kuznetsov NK-87
Kuznetsov NK-88
Kuznetsov NK-89
Kuznetsov NK-144
Kuznetsov TV-2
Kuznetsov 2TV-2F
L
= L'Aisle Volante
=L'Aisle Volante C.C.4
= Labor
=Labor 70 hp 4-cyl in-line 100 mm × 210 mm (3.9 in × 8.3 in)
= Lambert Engine Division
=(Monocoupe Corporation – Lambert Engine Division)
Lambert M-5
Lambert R-266
Lambert R-270
= Lamplough
=Lamplough 6-cyl 2-stroke rotary 116 mm × 126 mm (4.6 in × 5.0 in)
Lamplough 6-cyl 2-stroke axial
= Lancia
=(Lancia & Company. / Vincenzo Lancia)
Lancia Tipo 4
Lancia Tipo 5
= Lange
=Lange EA 42
= Laviator
=Laviator 35 hp 3-cyl rotary 2-stroke 110 mm × 100 mm (4.3 in × 3.9 in)
Laviator 50 hp 6-cyl rotary 2-stroke 100 mm × 130 mm (3.9 in × 5.1 in)
Laviator 65 hp 6-cyl rotary 2-stroke 100 mm × 130 mm (3.9 in × 5.1 in)
Laviator 75 hp 9-cyl rotary 2-stroke 100 mm × 130 mm (3.9 in × 5.1 in)
Laviator 100 hp 12-cyl rotary 2-stroke 100 mm × 130 mm (3.9 in × 5.1 in)
Laviator 80 hp 6-cyl 2-stroke water-cooled radial 100 mm × 130 mm (3.9 in × 5.1 in)
Laviator 120 hp 4IL 145 mm × 174 mm (5.7 in × 6.9 in)
Laviator 110 hp 6IL 130 mm × 160 mm (5.1 in × 6.3 in)
Laviator 250 hp 6IL 180 mm × 200 mm (7.1 in × 7.9 in)
Laviator 80 hp V-8 100 mm × 130 mm (3.9 in × 5.1 in)
Laviator 120 hp V-8 114 mm × 160 mm (4.5 in × 6.3 in)
Laviator 200 hp V-8 145 mm × 175 mm (5.7 in × 6.9 in)
= Lawrance
=Lawrance A-3
Lawrance B 60 hp 3-cyl.
Lawrance C-2
Lawrance J-1
Lawrance J-2
Lawrance L-2 65 hp 4.25 in × 5.25 in (108 mm × 133 mm)
Lawrance L-3
Lawrance L-4 a.k.a. 'Wright Gale'
Lawrance L-5
Lawrance L-64
Lawrance N
Lawrance N-2 40HP 2OA 4.25 in × 4.25 in (108 mm × 108 mm)
Lawrance R
Lawrance R-1
Lawrance-Moulton A (France)
Lawrance-Moulton B (200 hp V-8 USA) 4.75 in × 6.5 in (121 mm × 165 mm)
Lawrance 140 hp 9-cyl radial 4.25 in × 5.25 in (108 mm × 133 mm)
Lawrance 200 hp 9-cyl radial 4.5 in × 5.5 in (110 mm × 140 mm)
= Lawrence Radiation Laboratory
=Tory IIA (Project Pluto)
Tory IIC (Project Pluto)
= Le Gaucear
=Le Gaucear 150 hp 10-cyl rotary
= Le Maitre et Gerard
=Le Maitre et Gerard 700 hp V-8 180 mm × 210 mm (7.1 in × 8.3 in)
= Le Rhône
== LeBlond
=LeBlond was sold to Rearwin and engines continued under Ken-Royce name.
LeBlond B-4
LeBlond B-8
LeBlond 40-3
LeBlond 60-5D
LeBlond 70-5DE
LeBlond 75-5
LeBlond 80-5
LeBlond 85-5DF
LeBlond 70-5E
LeBlond 80-5F (in military use known as R-265)
LeBlond 85-5DF
LeBlond 90-5F
LeBlond 90-5G
LeBlond 90-7
LeBlond 110-7
LeBlond 120-7
LeBlond 7D
LeBlond 7DF
= Lee
=Lee 80 hp
= Lefèrve
=(F. Lefèrve)
Lefèrve 2-cyl. 33 hp
= Lenape
=Lenape AR-3
Lenape LM-3 Papoose 3-cyl.
Lenape LM-5 Brave 5-cyl.
Lenape LM-7 Chief 7-cyl.
Lenape LM-125 Brave (suspect should be LM-5-125)
Lenape LM-365 Papoose (suspect should be LM-3-65)
Lenape LM-375 Papoose (suspect should be LM-3-75)
= Lessner
=Lessner 1908 4-cyl airship engine
= Levavasseur
=Léon Levavasseur see Antoinette
= Levi
=Levi 7-cyl barrel engine
= Leyland Motors
=J. G. Parry-Thomas, the chief engineer at Leyland Motors.
A single X-8 engine was built in August 1918 but failed during testing and with the end of WWI development was abandoned.
= LFW
=LFW 0
LFW I
LFW II
LFW III
LFW-12 X-1
= LHTEC
=LHTEC T800
= Liberty
=Source:Gunston except where noted
Liberty L-4
Liberty L-6
Liberty L-8
Liberty L-12
Liberty L-12 double-crankshaft
Liberty X-24
= Ligez
=Ligez 3-cyl rotary 115 mm × 130 mm (4.5 in × 5.1 in)
= Light
=Light Kitten 20
Light Kitten 30
Light Tiger 100
Light Tiger 125
Light Tiger Junior 50
= Lilloise
=See:C.L.M.
= Limbach
=Limbach L1700
Limbach L2000
Limbach L2400
Limbach L275E
Limbach L550E
= Lincoln
=Rocket 29 hp
= Lindequist
=(Konsortiert Överingeniör Sven Lindequist's Uppfinninggar – Consortium Senior Engineer Sven Lindqvist Inventions)
Lindewqiuist 1,000 hp Stratospheric engine
= Les Long Long Harlequin
=Long Harlequin 933
= Lockheed
=Lockheed XJ37/L-1000
= LOM
=(Letecke Opravny Malesice, Praha)
LOM M132
LOM M137
LOM M337
= Loravia
=(Yutz, France)
Loravia LOR 75
= Lorraine-Dietrich
=(Société Lorraine des Anciens Établissements de Dietrich)
Source:Jane's All the World's Aircraft 1938
except where noted
= Lotarev
=(Vladimir Lotarev) (see also Ivchenko-Progress)
Lotarev D-36
Lotarev D-136
Lotarev D-236-T
Lotarev DV-2
Lotarev RD-36 (lift turbofan)
= Loughead
=Loughead XL-1
= LPC
=LPC Fang 1-KS-40
LPC Sword 3.81-KS-4090
LPC Meteor 33-KS-2800
LPC Mercury 0.765-KS-53,600
LPC Viper I-C 5.6-KS-5,400
LPC Viper II-C 3.77-KS-8,040
LPC Lance I-C 6.65-KS-38,800
= LSA-Engines
=(LSA-Engines GmbH, Berlin, Germany)
LSA-Engines LSA850
= Lucas
=Lucas CT 3201
= Lutetia
=(Marcel Echard / Moteurs Lutetia)
Lutetia 4.C.02 V-4, 2-stroke, 1267 cc, 40-45 hp at 2800rpm
Lutetia 6-cyl radial 70 hp a 2600 rpm
= Lycoming
== Lyulka
=Source:Gunston.
Lyulka TR-1
Lyulka AL-5
Lyulka AL-7
Lyulka AL-21
Lyulka AL-31
Lyulka AL-34
Lyulka TS-31M
= LZ Design
=Front electric sustainer
M
= M&D Flugzeugbau
=M&D Flugzeugbau TJ-42
= MAB
=4-cylinder air-cooled "fan" engine
4-cylinder vertical water-cooled in-line engine
= MacClatchie
=MacClatchie X-2 Panther
= Macchi
=Macchi MB.2 – 2.cyl 20 hp at 3,000 rpm
= Macomber Avis
=Macomber Rotary Engine Company with Avis Engine Company
Macomber Avis 7-cylinder axial engine
= M.A.N.
=Maschinenfabrik Augsburg-Nürnberg (MAN)
Licence-built Argus As III
MAN Mana V (350 hp V-10) V-10 airship engine?
MAN Mana III (185 hp 6-cyl in-line)
260 hp 6-cylinder in-line – "quite similar to 160-hp Mercedes design"
= MAN Turbo
=MAN Turbo 6012
MAN Turbo 6022
Rolls-Royce/MAN Turbo RB153
Rolls-Royce/MAN Turbo RB193
= Manfred Weiss
=See: Weiss
= Manly
=Charles M. Manly redesigned an engine built by Stephen Balzer.
Manly–Balzer engine
= Mantovani
=Mantovani Citroën 2CV car engine conversion
= Marchetti
=(Marchetti Motor Patents)
Marchetti A
= Mark
=(Stahlwerk Mark Flugzeugbau)
Mark F.II (35 hp)
Mark M.3 (40 hp)
Mark M.5 (70 hp)
Mark 55 hp
Mark 120 hp
= Marcmotor
=(Macerata, Italy)
Marcmotor ROS100
Marcmotor ROS125
Marcmotor ROS200
= Marlin-Rockwell
=Marlin-Rockwell 72 hp
= Marquardt Corporation
=Marquardt PJ40 pulsejet
Marquardt PJ46 pulsejet
Marquardt RJ30 C-20 ramjet
Marquardt RJ31 C-30 Ramjet
Marquardt RJ34 ramjet
Marquardt RJ39 ramjet
Marquardt RJ43
Marquardt RJ57 ramjet
Marquardt RJ59 ramjet
Marquardt MA-19
Marquardt MA-20
Marquardt MA-24
Marquardt MA-74
Marquardt MA-196
Marquardt C-20 (2x C-20s fitted to P-51 and 2x Marquardt C20-85D fitted to P-80A 44-85042)
Marquardt C-30 (2x Marquardt C30-10B fitted to P-80A 44-85214)
Marquardt C-48
Marquardt R-1E
Marquardt R-40A
= Martin
=Martin 133? typo?
Martin 333
Martin 500
Martin 8200 (190 hp V-8) 4.625 in × 7 in (117.5 mm × 177.8 mm)
Martin L-330
= Maru
=Maru Ka10
= Masson
=Masson 50 hp 6-cyl in-line
= Mathis
== Mawen
=(Mawen S.A.)
Mawen 150 hp rotary
Mawen 350 hp rotary
Mawen 700 hp two row rotary
= Max Ams
=(Max Ams machine Company)
Max Ams 75 hp V-8 3.9375 in × 5.125 in (100.01 mm × 130.18 mm)
= Maxim
=Maxim 87 hp 4-cyl in-line 5 in × 5.625 in (127.0 mm × 142.9 mm)
= Maximotor Makers
=Maximotor 50 hp
Maximotor 60-70 hp
Maximotor 70-80 hp
Maximotor 80-100 hp
Maximotor 100 hp
Maximotor 120 hp
Maximotor 150 hp
Maximotor A-4 (50 hp 4ILW) 4.5 in × 5 in (110 mm × 130 mm)
Maximotor A-6 (75 hp 6ILW) 4.5 in × 5 in (110 mm × 130 mm)
Maximotor A-8 (110 hp V-8)5 in × 5.5 in (130 mm × 140 mm)
Maximotor B-6 (115 6ILW) 5 in × 6 in (130 mm × 150 mm)
Maximotor 70 hp 4-in-line 5.25 in × 5.5 in (133 mm × 140 mm)
= Maybach
== Mayo
=(Mayo Radiator Co)
Mayo 1915 (6LW)
= McCulloch
=McCulloch MAC-101
McCulloch 104-100
McCulloch O-90
McCulloch O-100
McCulloch O-150
McCulloch 4318A O-100-1
McCulloch 4318B O-100-2
McCulloch 4318C O
McCulloch 4318E YO-100-4
McCulloch TSIR-5190
McCulloch 6150 O-150-1
McCulloch 6318 O-150-2
= McDonnell
=McDonnell PJ42 pulsejet
= McDowell
=(Geo. McDowell. Brooklyn NY.)
McDowell Twin-Piston V-4 2-stroke
= Mead
=(Mead Engine Co.)
Mead 50 hp 4-cyl in-line 4.75 in × 4.5 in (121 mm × 114 mm)
= Mekker
=Mekker Sport
= Menasco
=Sources:Gunston and Jane's.
Menasco Pirate/Super Pirate
Menasco Buccaneer/Super Buccaneer
Menasco M-50
Menasco Unitwin 2-544
Menasco-Salmson B-2
Menasco L-365 – Military designation for Pirate
Menasco XIV-2040
Menasco XH-4070
Menasco RJ37
= Mengin
=(Établissements Pierre Mengin)
Mengin B
Mengin C (later 2A.01), Poinsard design
Mengin G.M.H. (Genete, Mengin, and Hochet)
Mengin 2A.01 Poinsard design
Hochet-Mengin
= Mercedes
=See: Daimler-Benz
= Merkulov
=(Ivan A. Merkulov)
Merkulov DM-4 ramjet
= Métallurgique
=Data from:
Métallurgique 32 hp 4-cyl in-line 100 mm × 150 mm (3.94 in × 5.91 in)
Métallurgique 40 hp 4-cyl in-line 85 mm × 130 mm (3.35 in × 5.12 in)
Métallurgique 48 hp 4-cyl in-line 125 mm × 150 mm (4.92 in × 5.91 in)
Métallurgique 60 hp 4-cyl in-line 100 mm × 150 mm (3.94 in × 5.91 in)
Métallurgique 90 hp 4-cyl in-line 125 mm × 150 mm (4.92 in × 5.91 in)
= Meteormotor
=Meteormotor 20-25 hp
= Meteor
=(Meteor S.p.A. Constuzioni Aeronautiche)
Meteor G 80cc
Meteor Alfa 1
Meteor Alfa 1AQ
Meteor Alfa 2
Meteor Alfa 2AQ
Meteor Alfa 2V
Meteor Alfa 3
Meteor Alfa 3AQ
Meteor Alfa 4
Meteor Alfa 4V
Meteor Alfa 5
= Metropolitan-Vickers
=Metrovick F.1
Metrovick F.2 Freda
Metrovick F.2/2
Metrovick F.2/3
Metrovick F.2/4 Beryl
Metrovick F.3
Metrovick F.5
Metrovick F.9 Sapphire
= Metz
=(Metz Company, Waltham, Mass.)
Metz 125 hp rotary 6.75 in × 6.75 in (171 mm × 171 mm)
= Michel
=Michel IV-AT3
Michel 4A-14
Michel RAT-3 100 hp
Michel A.M. 14 MARK II
Michel A.M.7 6L 200 hp
Michel A.M.14 Type I 4L 100 hp
Michel A.M.14 Type II
Michel A.M.14 Type III
Michel A.M.16 6L 40 hp
= Michigan
=Michigan 2-cyl 2-stroke rotary 5 in × 5 in (130 mm × 130 mm)
Michigan Rover
= Microturbo
== Mid-west
=(Mid-West Engines Limited / Diamond engines / Austro Engine)
MidWest AE50
MidWest AE100
MidWest AE110
Austro Engine AE50R
Austro Engine AE75R
= Miese
=Data from:
Miese 50-60 hp 8-cyl
Miese 100 hp 8-cyl radial 130 mm × 130 mm (5.1 in × 5.1 in)
= Mikulin
=Mikulin AM-3M
Mikulin AM-13
Mikulin AM-34
Mikulin AM-35
Mikulin AM-37
Mikulin AM-38
Mikulin AM-39
Mikulin AM-42
Mikulin M-85
Mikulin RD-3M
Mikulin M-17
Mikulin M-209
Mikulin AM-TKRD-01
= Mikulin-Stechkin
=(A.A. Mikulin & B.S. Stechkin)
AMBS-1
= Milwaukee Tank
=Milwaukee Tank V-470
Milwaukee Tank V-502
= Miller
=Miller 22 hp radial
= Miller
=(Harry A. Miller Manufacturing Company)
Miller 125 hp 4-cyl in-line 4 in × 7 in (100 mm × 180 mm)
Miller V-12 5 in × 6 in (130 mm × 150 mm)
= Minié
=Data from:
(Établissements Minié, Colombes, Seine, France)
Minié 4.B0 Horus
Minié 4.D
Minié 4.E0 Horus
Minié 4.E2 Horus
= Mistral Engines
=Mistral G-190
Mistral G-200
Mistral G-230-TS
Mistral G-300
Mistral G-360-TS
Mistral K-200
Mistral K-300
= Mitsubishi
=Mitsubishi Ha-42
Mitsubishi Ha-43
Mitsubishi Kasei
Mitsubishi Kinsei
Mitsubishi Shinten
Mitsubishi TS1/MG5
Mitsubishi Zuisei
= Modena Avio Engines
=(Rubiera, Italy)
MAE 323
= Monaco
=(Monaco Motor and Engineering Co. Ltd.)
Monaco 75 hp
Monaco 100 hp
= Monnett
=Data from:'
Monnett AeroVee
Monnett 1600cc E-Vee
Monnett 1600cc SuperVee
Monnett 1700cc E-Vee
Monnett 1700cc SuperVee
Monnett 1835cc E-Vee
Monnett 2007cc E-Vee
= Morehouse
=Morehouse 15 hp
Morehouse 29 hp
Morehouse M-42
Morehouse M-80
= Mors
=Data from:
Mors 30 hp V-4 100 mm × 130 mm (3.9 in × 5.1 in)
= Mosler
=(Mosler, Inc. of Hendersonville, North Carolina)
Mosler MM CB-35
Mosler MM CB-40
Mosler Red 82X
= Motor Sich
=Motor Sich MS-500V
= Motorav Industria
=Motorav 2.3 V
Motorav 2.6 R
Motorav 2.6 V
Motorav 2.8 R
Motorav 3.1 R
= Motorlet
=Motorlet M-701
Motorlet M-601
Motorlet M-602
Motorlet M-20
Motorlet AI-25/Titan/Sirius – see Ivchenko AI-25
= Mozhaiskiy
=Mozhaisky gas fired machine
= MTH
=MTH R 422-CG
= MTR
=MTR MTR390
= MTU Aero Engines
=MTU DB 720F/PTL6
MTU DB 721/PTL10
MTU DB 730F/PTL6
MTU DB 730H/ZTL6
MTU 6012
MTU 6022
= Mudry
=(Moteurs Mudry-Buchoux)
Mudry MB-4-80
Mudry MB-4-90
= Mulag
=Mulag 90/113 hp 6-cyl in-line 110 mm × 170 mm (4.3 in × 6.7 in)
= Murray-Willat
=Murray Ajax
Murray Atlas
Murray-Willat 35 hp 6-cyl 2-stroke rotary 75 mm × 90 mm (3.0 in × 3.5 in)
Murray-Willat 90 hp 6-cyl 2-stroke rotary 100 mm × 130 mm (3.9 in × 5.1 in)
= MWfly
=(MWfly srl, Passirana di Rho, Italy)
MWfly B22
MWfly B25
N
= N.A.G.
=Source:Angle.
NAG 40 hp 4-cyl in-line
NAG C.III
NAG F.1
NAG F.2
NAG F.3
NAG F.4
NAG Model 301
NAG 6-cyl 135 hp
= Nagel
=Nagel 444
= Nagliati
=Nagliati V.N.V 160 hp Y-12 120 mm × 130 mm (4.7 in × 5.1 in)
Nagliati 250 hp 8-cyl twin4 120 mm × 100 mm (4.7 in × 3.9 in)
= Nakajima
=Nakajima Ha5
Nakajima Ha219
Nakajima Hikari
Nakajima Homare
Nakajima Kotobuki
Nakajima Mamoru
Nakajima Sakae
= NAMI
=NAMI A.M.B.20
= Napier
=Sources: Piston engines, Lumsden, gas turbine and rocket engines, Gunston.
= Narkiewicz
=(Wiktor N. Narkiewicz – production at C.Z.P.S.K. (National)
Narkiewicz WN-1
Narkiewicz WN-2
Narkiewicz WN-3
Narkiewicz WN-4
Narkiewicz WN-6
Narkiewicz WN-6R
Narkiewicz WN-7
Narkiewicz WN-7R
Narkiewicz NP-1
Narkiewicz 2-cyl.
= Naskiewicz
=(Stanislaw Naskiewicz)
Naskiewicz gas turbine
= National Aerospace Laboratory of Japan
=MITI/NAL FJR710
= National
=National 35
= N.E.C.
=(New Engine Co.)
N.E.C. 1910 2-cyl 2-stroke
N.E.C. 1910 60 hp 6-cyl 2-stroke
N.E.C. 40 hp 4-cyl 2-stroke
N.E.C. 50 hp V-4 2-stroke 94 mm × 114 mm (3.7 in × 4.5 in)
N.E.C. 90 hp 6-cyl 2-stroke 94 mm × 114 mm (3.7 in × 4.5 in)
N.E.C. 100 hp 6-cyl 2-stroke(1912)
N.E.C. 69.6 hp 4-cyl 2-stroke 114 mm × 101 mm (4.5 in × 4.0 in)
= Nelson
=Nelson 60 hp 4-stroke
Nelson 120 hp 4-stroke
Nelson 150 hp 4-stroke
Nelson H-44
Nelson H-49
Nelson H-56
Nelson H-59
Nelson H-63
Nelson O-65
= Nielsen & Winther
=Nielsen & Winther M.A.J.
= Nieuport
=Nieuport 28 hp 2-cyl opposed 130 mm × 150 mm (5.1 in × 5.9 in)
Nieuport 32/35 hp 2-cyl opposed 135 mm × 150 mm (5.3 in × 5.9 in)
= Nihonnainenki
=Nihonnainenki Semi
= Nippon
=(Nippon Jet Engine Company)
Nippon J0-1
Nippon J0-3
Nippon J1-1
Nippon J3-1
= Noel Penney Turbines
=NPT301
= Nord
=Nord ST.600 Sirius I
Nord ST.600 Sirius II
Nord ST.600 Sirius III
Nord Véga
= Normalair Garrett
=NGL WAM 274
NGL WAM 342
= Northrop
=Source:Gunston.
Northrop Model 4318F
Northrop O-100
Northrop Turbodyne XT-37
= Norton
=(Kenneth Norton / Norton-Newby Motorcycle Co.)
Norton 2-cyl opposed 4 in × 4.5 in (100 mm × 110 mm)
Norton NR642
= Novus
=Novus 70 hp 6-cyl rotary 120 mm × 130 mm (4.7 in × 5.1 in)
Novus 70 hp 6-cyl double rotary 120 mm × 130 mm (4.7 in × 5.1 in)
= NPO Saturn
=AL-31
AL-32
AL-34
AL-55
= NPT
=NPT100
NPT109
NPT151
NPT301
NPT301 LTD
= NST-Machinenbau
=(Niedergoersdorf, Germany)
NST BS 650
= Nuffield
=Nuffield 100 hp 4HO
O
= Oberursel
=Oberursel U.0
Oberursel U.I
Oberursel U.II
Oberursel U.III
Oberursel Ur.II
Oberursel Ur.III
Oberursel 200 hp 18-cyl rotary 124 mm × 150 mm (4.9 in × 5.9 in)
Oberursel 240 hp V-8
= Oerlikon
=Oerlikon 50/60 hp 4-cyl opposed 100 mm × 200 mm (3.9 in × 7.9 in)
= Oldfield
=Oldfield 15A 124 mm × 150 mm (4.9 in × 5.9 in)
= Omsk
=Omsk TVO-100
= Opel
=Opel Argus As III
= Orenda Engines
=Orenda Engines, formed by Avro Canada taking over publicly funded jet engine development by Turbo Research. Later became Orenda Aerospace under Magellan.
Avro Canada Chinook
Avro Canada Orenda
Orenda Iroquois
Orenda OE600
licence-built General Electric J79
licence-built General Electric J85
= Orion
=Orion LL-30
= Orlo
=(Orlo Motor Company)
Orlo B-4 4IL 50 hp 4.5 in × 6 in (110 mm × 150 mm)
Orlo B-6 6IL 75 hp 4.5 in × 6 in (110 mm × 150 mm)
Orlo B-8 V-8 100 hp 4.5 in × 6 in (110 mm × 150 mm)
= Orlogsværftet
=Orlogsværftet O.V. 160
= OKL
=(Ośrodek Konstrukcji Lotniczych WSK Okęcie)
OKL LIS-2
OKL LIS-2A
OKL LIS-5
OKL LIT-3
OKL TO-1
OKL NP-1
OKL WN-3 (Wiktor Narkiewicz)
OKL WN-6 (Wiktor Narkiewicz)
OKL WN-7 (Wiktor Narkiewicz)
= Otis-Pifre
=Otis-Pifre 6-cyl in-line
Otis-Pifer 500 hp V-12 130 mm × 160 mm (5.1 in × 6.3 in)
= Otto A.G.O.
=Otto A.G.O. 50 hp
Otto A.G.O. 70 hp
Otto A.G.O. 80/100 hp
Otto A.G.O. 100/130 hp
Otto 200 hp 8 in-line
P
= Packard
=Source:Gunston.
= Palmer
=(Palmer Motor Company)
Palmer 80 hp
= Palons & Beuse
=Palons & Beuse 2-cyl opposed
= Panhard & Levassor
=Source:
(Société Panhard & Levassor)
= Parker
=(Aero Parker Motor Sales Company)
Parker 1912 3 cyl
Parker 1912 6 cyl
= Parma Technik
=(Luhačovice, Zlín Region, Moravia, Czech Republic)
Parma Mikron III UL
= Parodi
=(Roland Parodi)
Parodi HP 60Z
= PBS
=(První Brnenská Strojírna Velká Bíteš, a.s.)
PBS TJ-20
PBS TJ-40
PBS TJ-100
PBS Velka Bites ÒÅ 50Â
= Pegasus Aviation
=Pegasus PAL 95
= Per Il Volo
=Per Il Volo Top 80
= Peterlot
=Peterlot 80 hp 7-cyl radial
= Peugeot
=Peugeot 8Aa, or L112, V-8 100 mm × 180 mm (3.9 in × 7.1 in)
Peugeot Type 16AJ 440 hp double V-8 120 mm × 160 mm (4.7 in × 6.3 in)
Peugeot L41 600 hp V-12 160 mm × 170 mm (6.3 in × 6.7 in)
Peugeot Type 16X X-16 130 mm × 170 mm (5.1 in × 6.7 in)
Peugeot 12L13
= Pheasant Aircraft Company
=Pheasant Flight 4-cyl
= Phillips
=(Phillips Aviation Company)
Phillips 333 (Martin 333)
Phillips 500
= Piaggio
=Data from:Italian Civil & Military Aircraft 1930–1945 and Jane's 1938
Piaggio P.II (Armstrong Siddeley Lynx)
Piaggio Stella P.VII
Piaggio Stella P.IX
Piaggio P.X
Piaggio P.XI
Piaggio P.XII
Piaggio P.XV
Piaggio P.XVI
Piaggio P.XIX
Piaggio P.XXII
Piaggio-Jupiter
Piaggio Lycoming
= Pierce
=(Samuel S Pierce Airplane Company)
Pierce B 35 hp 3RA 4 in × 6 in (100 mm × 150 mm)
= Pieper
=(Pieper Motorenbau GmbH)
Pieper Stamo MS 1500
Pieper Stamo 1000
= Pipistrel
=Pipistrel E-811
= Pipe
=Data from:
Pipe 50 hp V-8 3.94 in × 3.94 in (100 mm × 100 mm)
Pipe 110 hp V-8
= Pirna
=Pirna 014
= Platzer
=Platzer MA 12 P/Nissan
= Pobjoy
=Pobjoy P
Pobjoy R
Pobjoy Cataract
Pobjoy Cascade
Pobjoy Niagara
= Poinsard
=Poinsard 25hp 2-cyl
= Porsche
=Porsche 678
Porsche 702
Porsche PFM N00
Porsche PFM N01
Porsche PFM N03
Porsche PFM T03
Porsche PFM 3200
Porsche 109-005
Porsche YO-95-6
= Potez
== Pouit
=Pouit S-4
= PowerJet
=PowerJet SaM146
= Power Jets
=Power Jets WU
Power Jets W.1
Power Jets W.2
Power Jets/Rover B/23 – Rolls-Royce Welland
= Poyer
=(Poyer Aircraft Engine Company)
Poyer 3-40
Poyer 3-50
= Praga
=Source:Jane's All the World's Aircraft 1938
Praga B
Praga B2
Praga D
Praga DH
Praga DR
Praga ER
Praga ES
Praga ESV
Praga ESVKe
Praga ESVR
Praga FRK
Praga M-197 helicopter engine
Praga Doris B
Praga Doris M-208B
Praga E-I
Praga BD 500
= Pratt & Whitney
== Pratt & Whitney/Allison
=PW-Allison 578DX
= Pratt & Whitney Canada
=Pratt & Whitney Canada PT6
Pratt & Whitney Canada PT6T
Pratt & Whitney Canada ST6
Pratt & Whitney Canada JT15D
Pratt & Whitney Canada PW100
Pratt & Whitney Canada PW200
Pratt & Whitney Canada PW300
Pratt & Whitney Canada PW500
Pratt & Whitney Canada PW600
Pratt & Whitney Canada PW800
Pratt & Whitney Canada T74
Pratt & Whitney Canada T101
Pratt & Whitney Canada T400
= Pratt & Whitney Rzeszów
=Pratt & Whitney Rzeszów PZL-10
= Preceptor
=Preceptor 1/2 VW
Preceptor 1600cc
Preceptor Gold 1835
Preceptor Gold 2074
Preceptor 2180cc
= Price Induction
=DGEN
= Primi-Berthand
=Primi-Berthand 4-cyl in-line 2-stroke 100 mm × 180 mm (3.9 in × 7.1 in)
= Pulch
=(Otto Pulch)
Pulch 003
Pulch 3-cyl. radial
= Pulsar
=Pulsar Aeromaxx 100
= PZI
=(Państwowe Zakłady Inżynieryjne – National Engineering Works)
P.Z. Inż. Junior 120 hp
P.Z. Inż. Major
P.Z. Inż. Minor
= PZL
=(PZL Państwowe Zakłady Lotnicze)
PZL Rzeszów
(PZL Rzeszów)
PZL Rzeszów SO-1
PZL Rzeszów SO-3
PZL-Wytwórnia Silników
PZL GR.760
PZL GR.1620-A
PZL GR.1620-B
PZL-3 – Ivchenko AI-26
PZL-10
PZL GTD-350 – Klimov GTD-350
PZL-Kalisz ASz-61R
PZL ASz-62 – Shvetsov ASh-62
PZL-F 2A – Franklin 2 series
PZL-F 4A – licence built Franklin Engine Company
PZL-F 6A – licence built Franklin Engine Company
PZL-F 6V – licence built Franklin Engine Company
PZL-65KM
PZL K-15
Q
= Quick Air Motors Co
=(Quick Air Motors, Wichita KS.)
Quick Super Rhone – conversion of 80 hp Le Rhône 9C rotary engine to radial.
Quick 180 hp
R
= Radne Motor AB
=Radne Raket 120
= Ranger
=Ranger Engines were a division of Fairchild Aircraft
Ranger 6-370
Ranger 6-375
Ranger 6-390
Ranger 6-410
Ranger L-440 (company designation 6-440)
Ranger V-770
Ranger V-880
Ranger XV-920
Ranger XH-1850 (not actually an H – a double 150° V – two separate crankshafts linked by a gearbox)
= Rapp
=Rapp Motorenwerke became BMW in 1917
Rapp 100 hp
Rapp 125/145 hp
Rapp Rp III
Rapp 200 hp
= Rasmussen
=(Hans L Rasmussen)
Rasmussen 65 hp
= Rateau
=Rateau GTS.65
Rateau A.65 gas turbine
Rateau SRA-01 Savoie
Rateau SRA-101 10-stage axial compressor
Rateau SRA-301 16-stage axial compressor
= Rausenberger
=Rausenberger A-8 45 hp V-8 3.5 in × 3.75 in (89 mm × 95 mm)
Rausenberger B-8 75 hp V-8 4.125 in × 4.75 in (104.8 mm × 120.7 mm)
Rausenberger C-12 150 hp V-12 4.125 in × 6 in (104.8 mm × 152.4 mm)
Rausenberger D-23 250 hp V-12 5 in × 6.5 in (130 mm × 170 mm)
Rausenberger E-6 150 hp 6IL 5 in × 6 in (130 mm × 150 mm)
Rausenberger 500 hp
= Raven Redrives
=Raven 1000 UL
Raven 1300 SVS Turbo
Raven 1600 SV
= RBVZ
=RBVZ-6 (M-1)
MRB-6
= Reaction Motors
== Rearwin
=Rearwin 1909 30-45 hp
Rearwin 1909 40-60 hp
Rearwin 1910 50-75 hp
Rearwin 1911 80-90 hp
= Rebus
=Rebus 50 hp 4-cyl
= Rectimo
=(Rectimo Aviation SA) / (Rectimo-Savoie Aviation)
Rectimo 4 AR 1200
Rectimo 4 AR 1600
= RED
=RED Aircraft GmbH
RED A03 – V12 four-stroke diesel engine
= Redrup
=Redrup 1910 50 hp 10-cyl contra-rotating rotary
Redrup 1914 150 hp 7-cyl radial
Redrup 5-cyl barrel engine
Redrup Fury (barrel engine built by Aero Syndicate Ltd.)
= Reggiane
=Reggiane Re 101 R.C.50 I (sometimes designated Re L 101 R.C.50 I)
Reggiane Re 102 R.C.50 I (inverted W-18)
Reggiane Re 103 R.C.40 I (inverted W-18)
Reggiane Re 103 R.C.50 I (inverted W-18)
Reggiane Re 103 R.C.57 I (inverted W-18)
Reggiane Re 103 R.C.48 (inverted W-18)
Reggiane Re 104 R.C.38 (V-12 derived from the Isotta Fraschini Asso L.121 R.C.40)
Reggiane Re 105 R.C.100 I (inverted W-18)
Reggiane H-24
= Régnier
== Renard
=(Société anonyme des avions et moteurs Renard / Alfred Renard, Belgium)
Renard Type 7 7RA
Renard Type 100 5RA
Renard Type 120 5RA
Renard Type 200 9RA
Renard Type 400 18RA (twin-row type 200)
= Renard
=Renard y Krebs
= Renault
=(Source: and)
= R.E.P.
=R.E.P. 20/24 hp 5-cyl. 85 mm × 95 mm (3.35 in × 3.74 in)
R.E.P. 30/34 hp 7-cyl. 85 mm × 95 mm (3.35 in × 3.74 in)
R.E.P. 95 hp 7-cyl. 110 mm × 160 mm (4.33 in × 6.3 in)
R.E.P. 40/48 hp 10-cyl. 85 mm × 95 mm (3.35 in × 3.74 in)
R.E.P. 60 hp 14-cyl. 85 mm × 95 mm (3.35 in × 3.74 in)
R.E.P. 60 hp 5-cyl fan 110 mm × 160 mm (4.3 in × 6.3 in)
R.E.P. 50 hp 5-cyl fan 100 mm × 140 mm (3.9 in × 5.5 in)
R.E.P. 75 hp 6-cyl
R.E.P. 60 hp 7-cyl
R.E.P. 85 hp 7-cyl radial 110 mm × 160 mm (4.3 in × 6.3 in)
= Revmaster
=Revmaster R-800 2cyl 27 hp (Citroën 2CV)
Revmaster R-1600D VW
Revmaster R-1600S
Revmaster R-1831D
Revmaster R-1831S
Revmaster R-2100D
Revmaster R-2100D Turbo 70 hp at 3,200 rpm
Revmaster R-2100S 65 hp at 3,200 rpm
Revmaster R-2300
Revmaster R-3000D 110 hp at 3,200 rpm
= Rex
=(Flugmachine Rex GesellschaftG.m.b.H.)
Rex rotary engine
= RFB
=RFB SG 85
RFB SG 95
= Rheem
=Rheem S-10 axial
= Rheinische
=Rheinische 35 hp 3-cyl fan 105 mm × 130 mm (4.1 in × 5.1 in)
Rheinische 50/60 hp 5-cyl radial 120 mm × 140 mm (4.7 in × 5.5 in)
Rheinische 70 hp 4-cyl in-line 120 mm × 140 mm (4.7 in × 5.5 in)
Rheinische 100 hp 6-cyl in-line 120 mm × 140 mm (4.7 in × 5.5 in)
= Rheinmetall-Borsig
=Rheinmetall 109-502
Rheinmetall 109-505
Rheinmetall 109-515 rocket (solid fuel)
Rheinmetall Rheintochter R 1 first stage
Rheinmetall Rheintochter R 1 second stage
Rheinmetall Rheintochter R 3 first stage
= Rhenania
=(Rhenania Motorenwerke)
Rhenania 11-cyl. rotary engine
= Ricardo
=Ricardo-Burt S55/4
Ricardo-Halford-Armstrong R.H.A.
= Richard & Hering
=(Rex-Simplex Automobilwerke)
Richard & Hering engines
= Richardson
=(Archibald and Mervyn, Sydney Australia)
Richardson rotary
= Righter Manufacturing
=Righter O-15
Righter O-45
= Roberts
=(Roberts Motor Company / E.W. Roberts, Sandusky. Ohio)
Roberts 50 hp 4-cyl in-line 4.5 in × 5 in (110 mm × 130 mm)
Roberts 75 hp 6-cyl in-line 4.5 in × 5 in (110 mm × 130 mm)
Roberts 4-X.
Roberts 6-X 100 hp 5 in × 5 in (130 mm × 130 mm)
Roberts 6-XX 200 hp 6.5 in × 6 in (170 mm × 150 mm)
Roberts 6-Z
Roberts E-12 350 hp 6 in × 6.5 in (150 mm × 170 mm)
= Robinson
=(Grinnell Aeroplane Co. / William C. Robinson)
Robinson 60 hp
Robinson 100 hp
= Robinson
=Robinson R-13
= Roché
=(Jean A Roché)
Roché L-267
= Rocket Propulsion Establishment
=RPE Gamma
= Rocketdyne
== Rocky Mountain
=Rocky Mountain Pegasus
= Rollason
=Rollason Ardem RTW
Rollason Ardem 4 CO2 FH mod
= Rolls-Royce Limited
=Sources: Piston engines, Lumsden, gas turbine and rocket engines, Gunston.
Note: For alternative 'RB' gas turbine designations please see the Rolls-Royce aero engine template.
= Rolls-Royce Holdings
=Note: For alternative 'RB' gas turbine designations please see the Rolls-Royce aero engine template.
= Rolls-Royce Turbomeca
=Rolls-Royce Turbomeca Adour
Rolls-Royce Turbomeca RTM322
= Rolls-Royce/SNECMA
=Rolls-Royce/Snecma Olympus 593
Rolls-Royce/SNECMA M45H
= Rossel-Peugeot
=(Frédéric Rossel et les frères Peugeot)
Rossel-Peugeot 100 hp 4-cyl in-line 140 mm × 140 mm (5.5 in × 5.5 in)
Rossel-Peugeot 30 hp 7-cyl rotary 109 mm × 110 mm (4.3 in × 4.3 in)
Rossel-Peugeot 40 hp 7-cyl rotary 110 mm × 110 mm (4.3 in × 4.3 in)
Rossel-Peugeot 50 hp 7-cyl rotary 110 mm × 110 mm (4.3 in × 4.3 in)
= Rotax
== Rotec
=Rotec R2800
Rotec R3600
= Rotex Electric
=Rotex Electric REB 20
Rotex Electric REB 30
Rotex Electric REB 50
Rotex Electric REB 90
Rotex Electric REG 20
Rotex Electric REG 30
Rotex Electric RET 30
Rotex Electric RET 60
Rotex Electric REX 30
Rotex Electric REX 50
Rotex Electric REX 90
= RotorWay
=RotorWay RI-162F
RotorWay RW-100
RotorWay RW-133
RotorWay RW-145
RotorWay RW-152
= Rotron
=Rotron RT300
Rotron RT600
= Rover
=Rover Gas Turbines Ltd.
Rover W.2B
Rover Marton
Rover Moreton
Rover Napton
Rover Wolston
Rover T.P.90
Rover/Lucas TJ125 (CT3201)
Rover 1S60
Rover 1S/60
Rover 2S/150A
Rover 748
Rover 801
Rover TJ-125
= Royal Aircraft Establishment
=RAE 21
RAE 22
= Royal Aircraft Factory
=RAF 1
RAF 2
RAF 3
RAF 4
RAF 5
RAF 7
RAF 8
= RRJAEL
=(Rolls-Royce and Japanese Aero-engines Ltd.)
RRJAEL RJ.500
= Rumpler
=Rumpler Aeolus
= Ruston-Proctor
=Ruston-Proctor 200 hp 6-stroke rotary(6-cyl 2-stroke?)
= Ryan-Siemens
=(Ryan Aeronautical Corp/Siemens-Halske)
Ryan-Siemens 5 (Sh-13)
Ryan-Siemens 7 (Sh-14)
Ryan-Siemens 9 (Sh-12)
Ryan-Siemens Sh-14
= Rybinsk Motor Factory
=DN-200
Rybinsk RD-36-35
Rybinsk RD-38
S
= SACMA
=(Guy Negre)
SACMA 100
SACMA 120
SACMA 150
SACMA 180
SACMA 240
= Safran Helicopter Engines
=Safran Arrano
Safran Aneto
= SAI Ambrosini
=Ambrosini P-25 – 2-cyl. horizontally opposed
= Salmson
=Salmson air-cooled aero-engines
Salmson 3A, 3Ad
Salmson 5A, 5Ac, 5Ap, 5Aq
Salmson 6A, 6Ad, 6Af
Salmson 6TE, 6TE.S
Salmson 7A, 7AC, 7ACa, 7Aq
Salmson 7M
Salmson 7O, 7Om
Salmson 9AB, 9ABa, 9ABc
Salmson 9AC
Salmson 9AD
Salmson 9AE, 9AEr, 9AErs
Salmson 9NA, 9NAs, 9NC, 9ND, 9NE, 9NH
Salmson 11B
Salmson 12C W-12?
Salmson 12V, 12Vars – V-12
Salmson water-cooled aero-engines
Salmson A – 2x7-cylinder barrel engine, 1 built
Salmson B – 2x7-cylinder barrel engine, 1 built
Salmson C – 2x7-cylinder barrel engine, 1 built
Salmson E – 2x9-cylinder barrel engine, 1 built
Salmson F – 2x9-cylinder barrel engine, 1 built
Salmson G – 2x7-cylinder barrel engine, 1 built
Salmson K – 2x7-cylinder barrel engine, 1 built
Salmson A.7
Salmson A.9
Salmson 2A.9 – a 2-row radial engine
Salmson B.9 water-cooled radial engine
Salmson C.9 water-cooled radial engine
Salmson M.9 water-cooled radial engine
Salmson P.9 water-cooled radial engine
Salmson R.9 water-cooled radial engine
Salmson M.7 water-cooled radial engine
Salmson 2M.7 water-cooled 2-row radial engine
Salmson 9.Z, 9.Za, 9.Zc, 9.Zm
Salmsons 18 cylinder in-line radial engines
Salmson 18Z (1919) 9-bank water-cooled in-line radial 2 x 9Z on common 2-throw crankshaft
Salmson 18AB (1920s) 9-bank air-cooled in-line radial
Salmson 18Cm, 18Cma, 18Cmb – (late 20s early 30s) 9-bank water-cooled (air-cooled heads) in-line radial
Salmson-Szydlowski SH.18 – 18-cyl 2-stroke radial diesel engine (nine banks of two in-line)
Licence-built
Argus As 10 – as Salmson 8As.00, 8As.04
= Saroléa
=Saroléa V-4
Saroléa Albatros 30 hp 2HO
Saroléa Aiglon
Saroléa Vautour 32 hp 2HO
Saroléa Epervier 25 hp 2HO
= S.A.N.A.
=S.A.N.A. 700 hp
= Saunders-Roe
=Saunders-Roe 45 lbf pulse-jet
Saunders-Roe 120 lbf pulse-jet
= Sauer
=Sauer S 1800
Sauer S 1800 UL
Sauer S 1900 UL
Sauer S 2100
Sauer S 2100 UL
Sauer S 2200 UL
Sauer S 2400 UL
Sauer S 2500
Sauer S 2500 UL
Sauer S 2700 UL
= Saurer
=GT-15
YS-2
YS-3
YS-4
= Scania-Vabis
=Scania-Vabis PD
= Schliha
=(Schlüpmannsche Industrie und Handelsgesellschaft)
Schliha 36 hp 2-cyl
Schliha F-1200
= Schmidding
=Schmidding 109-505 rocket (solid fuel)
Schmidding 109-513
Schmidding 109-533
Schmidding 109-543
Schmidding 109-553
Schmidding 109-563
Schmidding 109-573
Schmidding 109-593
Schmidding 109-603
= Schroeter
=Schroeter 89 hp 6-cyl in-line 124 mm × 160 mm (4.9 in × 6.3 in)
= Schwade
=(Otto Schwade GmbH, Erfurt, Germany)
Schwade Stahlherz engine
= SCI Aviation
=R6-80
R6-150
B4-160
= Scott
=Scott A2S Flying Squirrel
Scott 40 hp 2-stroke
Scott 1939 2-stroke
Scott 1950 2-stroke V4
= Security
=(Security Aircraaft Corporation)
Security S-5-120
= Sega
=Sega trunnion radial engine
= SELA
=(Société d'Etude pour la Locomotion Aérienne [SELA])
SELA V-8
= Seld
=(Seld-Kompressorbau G.m.b.H.)
Seld F2
= SEPR
== Sergant
=Sergant A
= SERMEL
=SERMEL TRS 12
SERMEL TRS 18
SERMEL TRS 25
= SFFA
=(Société Française de Fabrication Aéronautique, France)
SFFA Type A 100 hp 7-cyl
SFFA Type B 45 hp 3-cyl
= SFECMAS
=SFECMAS Ars 600
SFECMAS Ars 900
SFECMAS 12H
SFECMAS 12K
= Shenyang
=Shenyang PF-1
Shenyang Aircraft Development Office PF-1A
Shenyang WP-5
Shenyang WP-6
Shenyang WP-7
Shenyang WP-14 ("Kunlun")
Shenyang WS-5
Shenyang WS-6
Shenyang WS-8
Shenyang WS-10
= Shimadzu
=Shimadzu 80 hp 9-cyl rotary 105 mm × 140 mm (4.1 in × 5.5 in)
Shimadzu 90 hp V-8 110 mm × 110 mm (4.5 in × 4.5 in)
= Shvetsov
=Data from:Russian Piston Aero Engines
= S.H.K.
=S.H.K. 70 hp 7-cyl rotary 110 mm × 140 mm (4.3 in × 5.5 in)
S.H.K. 140 hp 14-cyl rotary 110 mm × 140 mm (4.3 in × 5.5 in)
S.H.K. 90 hp 7-cyl rotary 124 mm × 140 mm (4.9 in × 5.5 in)
S.H.K. 180 hp 14-cyl rotary 124 mm × 140 mm (4.9 in × 5.5 in)
= Siddeley-Deasy
=Siddeley Ounce
Siddeley Pacific
Siddeley Puma
Siddeley Tiger
= Siemens
=Siemens SP90G
Siemens SP260D
= Siemens-Halske
== Silnik
=Silnik M 11
Silnik Sh 14
= Simms
=Simms 51 hp V-6 4.33 in × 4.33 in (110 mm × 110 mm)
= Simonini Racing
=Simonini 200cc
Simonini Mini 2 Evo
Simonini Mini 2 Plus
Simonini Mini 3
Simonini Mini 4
Simonini Victor 1 Super
Simonini Victor 2
Simonini Victor 2 Plus
Simonini Victor 2 Super
= Škoda
=Skoda G-594 Czarny Piotruś
Skoda L
Skoda Lr
Skoda S.14
Skoda S.20
Skoda Hispano-Suiza W-12
= Skymotors
=Skymotors 70
Skymotors 70A
= Smallbone
=(Harry Eales Smallbone)
Smallbone 4-cyl wobble-plate axial piston engine
= Smalley
=(General Machinery Co)
Smalley Aero
= SMA Engines
=SMA SR305-230
SMA SR460
= Smith
=Smith Static
Smith 300 hp radial
= SMPMC
=(South Motive Power and Machinery Complex SMPMC prev Zhuzhou Aeroengine Factory)
SMPMC HS-5 – Chinese production of ShvetsovvASh-62
SMPMC HS-6 – Chinese production of Ivchenko AI-14
SMPMC WZ-8 – Chinese production of Turbomeca Arriel
SMPMC WZ-9
SMPMC WZ-16
= SNCAN
=SNCAN Ars 600
SNCAN Ars 900
SNCAN Pulse-jet
= SNECMA
=Société nationale d'études et de construction de moteurs d'aviation formed by nationalisation of Gnome et Rhône in 1945. On French engine designations even sub-series numbers (for example Gnome-Rhône 14N-68) rotated anti-clockwise (LH rotation) and were generally fitted on the starboard side, odd numbers (for example Gnome-Rhône 14N-69) rotated clockwise (RH rotation) and were fitted on the port side.
= SNCM
=(Société Nationale de Constructions de Moteurs – Lorraine post 1936)
Lorraine Type 120 Algol
Lorraine Type 111 Sterna
Lorraine Type 112 Sirius
= SOCEMA
=(Société de Construction et d'Équipments Méchaniques pour l'Aviation)
SOCEMA TGA 1
SOCEMA TG 1008
SOCEMA TGAR 1008
SOCEMA TP.1
SOCEMA TP.2
= Sodemo
=Sodemo V2-1.0
Sodemo V2-1.2
= Solar
== Solo
=(Solo Kleinmotoren GmbH)
Solo 560, also known as the Hirth F-10, used in the Scheibe SF-24 Motorspatz
Solo 2350, widely used in motor-gliders
Solo 2625 01
Solo 2625 02, used in the Glaser-Dirks DG-500, Schempp-Hirth Ventus-2, Sportinė Aviacija LAK-20 etc.
Solo 2625 02i, a fuel-injected version used in the Schempp-Hirth Arcus and Schempp-Hirth Quintus self-launching gliders
= Soloviev
=Source:Gunston.
Soloviev D-15
Soloviev D-20
Soloviev D-25V (TB-2BM)
Soloviev D-30
Soloviev D-30K (completely revised)
Soloviev D-90A
= Soloy
=(Soloy Conversions / Soloy Dual Pak Inc.)
Soloy Dual Pac
Soloy Turbine Pac
= Soverini
=(Soverini Freres et Cie)
Soverini-Echard 4D
Soverini-Echard 4DR
= Soviet union experimental engines
== Soyuz
=(AMNTK Soyuz)
Soyuz R-79V-300
Soyuz R-79M
Soyuz R-179-300
Soyuz VK-21
Soyuz R134-300
= SPA
=SPA 6A
= Speer
=Speer S-2-C
= Sperry
=(Lawrence Sperry Aircraft Co)
Sperry WBB 2-stroke
= Spyker
=Spijker 135 hp rotary
= Sport Plane Power
=(Sport Plane Power Inc.)
Sport Plane Power K-100A
= STAL
=STAL Skuten
STAL Dovern
= Star
=(Star Engineering Co. ltd.)
Star 40 hp
= Stark
=(Stark Flugzeugbau KG)
Stark Stamo 1400
= Statax
=(Statax Engine Company Ltd. – prev. Statax-Motor of Zurich)
Statax 3cyl 10 hp axial
Statax 5cyl 40 hp axial
Statax 7cyl 80 hp axial
Statax 10cyl 100 hp axial
= Stoewer
=Stoewer 125 hp
Stoewer 150 hp
Stoewer 180 hp
= Stratus 2000
=Stratus EJ 22
= Straughan
=(Straughn Aircraft Corp)
Straughan AL-1000 (Ford model 1A)
= Studebaker
=H-9350 (24cyl 153.2 litres)
= Studebaker-Waterman
=Studebaker-Waterman S-1
= Sturtevant
=Sturtevant 1913 40 hp
Sturtevant 1913 60 hp
Sturtevant 5 140 hp V-8 4.5 hp × 5.5 hp (3.4 kW × 4.1 kW)
Sturtevant 5A 140 hp V-8 4.5 hp × 5.5 hp (3.4 kW × 4.1 kW)
Sturtevant 5A-4
Sturtevant 5A-41⁄2 210 hp V-8 5 hp × 5.5 hp (3.7 kW × 4.1 kW)
Sturtevant 7 300 hp V-12 5 hp × 5.5 hp (3.7 kW × 4.1 kW)
Sturtevant D-4 48 hp 4IL 4.5 hp × 4.5 hp (3.4 kW × 3.4 kW)
Sturtevant D-6 86 hp 6IL 4.5 hp × 4.5 hp (3.4 kW × 3.4 kW)
Sturtevant E-6 100 hp 6IL 4.5 hp × 6 hp (3.4 kW × 4.5 kW)
= Subaru
=Subaru EJ25
Subaru EA82
= Sulzer
=Sulzer ATAR 09C
= Sunbeam
=Source: Lumsden.
Sunbeam 2,000 hp – engine for Kaye Don's Silver Bullet land speed record car
= Superior
=Superior Air Parts XP-320
Superior Air Parts XP-360
Superior Air Parts XP-382
Superior Air Parts XP-400
Superior Air Parts Gemini Diesel 100
Superior Air Parts Gemini Diesel 125
Superior Air Parts Vantage
= Survol-de Coucy
=Survol-de Coucy Pygmée 40 hp
= Svenska
=Svenska Flygmotor P/15-54
IA R-19-SR/1 Indio
Svenska Flygmotor RM1 Goblin
Svenska Flygmotor RM2 Ghost
Svenska Flygmotor RM5 Avon
Svenska Flygmotor RM6 Avon
Svenska Flygmotor RR2
Svenska RM8
Svenska F-451-A Trollet
Svenska Flygmotor VR-3
= Szekely
=Szekely SR-3 O 3-cyl (SR – "Sky Roamer")
Szekely SR-3 L
Szekely SR-5 5-cyl
Szekely 100 7-cyl
Szekely O-125
T
= Take Off
=Take Off TBM 10
Take Off TBM 11
Take Off TBM 12
= Tatra
=Tatra T100
Tatra T101
= TBS
=(Turbinenbau Schuberth Schwabhausen GmbH)
TBS 400N-J40P
= TEC
=See: Mosler
= Technopower
=(Technopower Inc.)
Technopower Twin O-101
= TEI
=TEI PD170
TEI TS1400
= Teledyne CAE
== Thaheld
=Thaheld O-290 diesel
= Thermo-Jet
=(Thermo-Jet Standard Inc.)
Thermo-Jet J3-200
Thermo-Jet J5-200
Thermo-Jet J7-300
Thermo-Jet J8-200
Thermo-Jet J10-200
Thermo-Jet J13-202
= Thames
=(Thames Ironworks and Ship[building Co.Ltd.)
Thames 30 hp 4OW
= Thielert
=Thielert Centurion 1.7
Thielert Centurion 4.0
= Thiokol
=Data from:Jane's All the World's Aircraft 1962-3
= Thomas
=(Thomas Aeromotor Company, United States)
Thomas 120 hp 4-cyl in-line
Thomas 8 135 hp 4 in × 5.5 in (100 mm × 140 mm)
Thomas 88 150 hp 4.125 in × 5.5 in (104.8 mm × 139.7 mm)
Thomas 890 250 hp 4.8125 in × 6 in (122.24 mm × 152.40 mm)
= Thorotzkai
=(Thorotzkai Péter alt, spelling Thoroczkay)
Thorotzkai 12 hp
Thorotzkai 22 hp 3cyl. radial
Thorotzkai 35 hp opposed twin
Thorotzkai typ.7 35 hp
Thorotzkai 120 hp
Thorotzkai Gamma-III (35 hp 3cyl. radial)
= Thulin
=Thulin A (engine)
Thulin D (engine) (Le Rhône 18E ?)
Thulin E (engine)
Thulin G (engine) (Le Rhône 11F ?)
= Thunder
=(Thunder Engines Inc.)
Thunder TE495-TC700
= Tierney Turbines
=MEP362A
= Tiger
=(The Light Manufacturing and Foundry Company)
Tiger 100
Tiger 125
Tiger Kitten-20
Tiger Kitten-30
Tiger Junior 50
= Tips
=Tips 480 hp 250 hp 4.5 in × 6 in (110 mm × 150 mm) (18 cyl., 1717.67 ci, air- and water-cooled rotary engine. At rated RPM the crankshaft rotated at 1800 rpm, propeller shaft at 1080 rpm and the engine body at 60 rpm. Cooling was by direct air flow and tubular radiators between the cylinders, with water circulating without hoses or pumps.)
= Tips & Smith
=Tips & Smith Super-Rhône
= Tomonoo
=(Tomon Naoji)
Tomono 90 hp 6-cyl in-line 4.5 in × 4.375 in (114.3 mm × 111.1 mm)
= Tone
=Tone 2V9 180 hp 4.5 in × 4.375 in (114.3 mm × 111.1 mm)
= TNCA
=TNCA Aztatl
TNCA Trebol
= Tokyo Gasu Denk/Gasuden
=Tokyo Gasu Denki Amakaze
Tokyo Gasu Denki Hatakaze
Tokyo Gasu Denki Jimpu 3
Tokyo Gasu Denki Kamikaze
Tokyo Gasu Denki Tempu
Gasuden Amakaze
Gasuden Hatakaze
Gasuden Jimpu 3
Gasuden Kamikaze
Gasuden Tempu
= Torque Master
=(Valley Engineering)
Torque Master 1835cc
Torque Master 1915cc
Torque Master 2180cc
= Tosi
=Tosi 450 hp V-12 130 mm × 190 mm (5.1 in × 7.5 in)
= Total Engine Concepts
=Total Engine Concepts MM CB-40
= Trace Engines
=Trace turbocharged V-8
= Train
=(Établissements E. Train / Société des Constructions Guinard)
Train 2T
Train 4A
Train 4E
Train 4T
Train 6C
Train 6D
Train 6T
= Trebert
=Trebert 60 hp 6-cyl rotary barrel engine 3.75 in × 4.25 in (95 mm × 108 mm)
Trebert 100 hp V-8
= Tumansky
=Tumansky M-87
Tumansky M-88
Tumansky R-11
Tumansky R-13
Tumansky R-15
Tumansky RU-19
Tumansky R-21
Tumansky R-25
Tumansky R-266
Tumansky R-27
Tumansky R-29
Tumansky RD-9
= Turbomeca
=Source:Gunston except where noted
= Turbo Research
=Turbo Research was taken over by Avro Canada
Turbo Research TR.1 – abandoned design study
Turbo Research TR.2 – abandoned design study
Turbo Research TR.3 – abandoned design study
Turbo Research TR.4 – see Avro Canada Chinook
Turbo Research TR.5 – see Avro Canada Orenda
= Turbo-Union
=Turbo-Union was a joint venture between Rolls-Royce Ltd, MTU and Aeritalia to produce engine for Panavia Tornado
Turbo-Union RB199
= Twombly Motor Company
=Twombly Motor Company (Willard Irving Twombly)
A 50 hp 7-cylinder rotary; 4 in × 4.5 in (100 mm × 110 mm), 1912.
U
= Ufimtsev
=(A.G. Ufimtsev)
Ufimtsev 1908 20 hp 2-cyl 2-stroke rotary
Ufimtsev 1910 35-40 hp 4-cyl contra-rotating rotary
Ufimtsev ADU-4 – 60 hp 6-cyl contra-rotating rotary
= ULPower
=ULPower UL260i
ULPower UL350i
ULPower UL390i
ULPower UL520i
= Union
=(Union Gas Engine Company, United States)
Union 120 hp 6-cyl in-line 4.75 in × 6.5 in (121 mm × 165 mm)
= Ursinus
=(Ursinus Leichtmotorenbau)
Ursinus U.1
Ursinus U.2
= UTC
=(United Technology Corporation)
UTC P-1
V
= Valley
=(Valley Engineering)
Valley 1915cc
Valley 2276cc
= Van Blerck
=(Van Blerck Motor Co., Monroe, Michigan)
Van Blerck 124 hp V-8
Van Blerck 135 hp V-8 4.5 in × 5.5 in (110 mm × 140 mm)
Van Blerck 185 hp V-12 4.5 in × 5.5 in (110 mm × 140 mm)
= Vaslin
=(Henri Vaslin)
Vaslin 15 hp 1.13 L (69 cu in) flat-4
Vaslin 24 hp 1.3 L (80 cu in)
Vaslin 55 hp 2 L (120 cu in) 6 in-line water-cooled
= Vauxhall
=(Vauxhall Motors Ltd.)
Vauxhall 175 hp V-12 90 mm × 120 mm (3.5 in × 4.7 in)
= Vaxell
=Vaxell 60i
Vaxell 80i
Vaxell 100i
= Vedeneyev
=Vedeneyev M14P
= Velie
=Velie M-5
Velie L-9
= Verdet
=Verdet 55 hp 7-cyl rotary 112 mm × 140 mm (4.4 in × 5.5 in)
= Vereinegung Volkseigener Betriebe Flugzeugbau
=See: Pirna
= Verner Motor
=Source: RMV, Verner Motor range of engines,
Verner Scarlett mini 3 – 3 cyl radial
Verner Scarlett mini 5 – 5 cyl radial
Verner Scarlett 7H – 7 cyl radial
Verner Scarlett 36Hi
Verner JCV 360
Verner VM 125
Verner VM 133
Verner VM 144Hi
Verner VM 1400
Verner Scarlett 3V
Verner Scarlett 5V
Verner Scarlett 5Si
Verner Scarlett 7U
Verner Scarlett 9S
= Viale
=Viale 35 hp (1910 35-50 hp 5-cyl. radial)
Viale 30 hp 3-cyl fan 105 mm × 130 mm (4.1 in × 5.1 in)
Viale 50 hp 5-cyl radial 105 mm × 130 mm (4.1 in × 5.1 in)
Viale 70 hp 7-cyl radial 105 mm × 130 mm (4.1 in × 5.1 in)
Viale 100 hp 10-cyl radial 105 mm × 130 mm (4.1 in × 5.1 in)
= VIJA
=VIJA J-10Si
VIJA J-10Sbi
VIJA AG-12Si
VIJA AG-12Sbi
VIJA J-16Ti
= Viking
=(Viking Aircraft Engines)
Viking 100
Viking 110
= Viking
=(Detroit Manufacturers Syndicate Inc)
Viking 140 hp X-16 3.25 in × 4 in (83 mm × 102 mm)
= Villiers-Hay
=(Villiers-Hay Development Ltd.)
Villiers-Hay 4-L-318 Maya I
Villiers-Hay 4-L-319 Maya II
= Vittorazi
=(Morrovalle, Italy)
Vittorazi Easy 100 Plus
Vittorazi Fly 100 Evo 2
Vittorazi Moster 185
= Vivinus
=Data from:
Vivinus 32.5 hp 4-cyl in-line 4.17 in × 4.73 in (106 mm × 120 mm)
Vivinus 37.5 hp 4-cyl in-line 4.42 in × 5.12 in (112 mm × 130 mm)
Vivinus 39.2 hp 4-cyl in-line 4.53 in × 5.12 in (115 mm × 130 mm)
Vivinus 50 hp 4-cyl in-line 4.17 in × 4.73 in (106 mm × 120 mm)
Vivinus 60 hp 4-cyl in-line 4.42 in × 5.12 in (112 mm × 130 mm)
Vivinus 70 hp 4-cyl in-line
= Volkswagen
=1/2 VW
= Volvo Aero
=RM1
RM2 – licence built de Havilland Ghost
RM3
RM4
RM5, RM6 – licence built Rolls-Royce Avon
Volvo RM8 – modified Pratt & Whitney JT8D
Volvo RM12 – variant of General Electric F404
= von Behren
=von Behren O-113 Air Horse
= Voronezh
=(Voronezh engine factory)
Voronezh MV-6
W
= Wackett
=Source: RMV
Wackett 2-cylinder 20/25 hp
Wackett 2-cylinder 40 hp
Wackett Victa 1-cylinder 1924
= Walter Aircraft Engines
== Walter (HWK)
=Walter RI-201 "Cold" Take Off Pack
Walter RI-203 "Hot" Take Off Pack
Walter RII.203
Walter RII.211
Walter HWK 109-500
Walter HWK 109-501
Walter HWK 109-507
Walter HWK 109-509
Walter HWK 109-559
Walter HWK 109-719
Walter HWK 109-729 (SV-stoff and R-stoff)
Walter HWK 109-739
Walter Heimatschützer I
Walter Heimatschützer IV
Walter Me.109 Climb Assister
= Wankel
=Wankel AG LCR – 407 SGti
Wankel AG LCR – 814 TGti
= Warbirds-engines
=(Cesky znalecky institut sro, Prague, Czech Republic)
Warbirds ASz-62 IR
= Warner
=Warner Scarab/Super Scarab
Warner Scarab Junior
Warner R-420
Warner R-500
Warner R-550
Warner 145
Warner 165
Warner 185
= WASAG
=(Westphalisch-Anhaltische Springstoff A.G.)Source: RMV
WASAG 109-506
WASAG 109-512
WASAG 109-522
WASAG 109-532
= Watson
=(Gary Watson of Newcastle, Texas)
Watson 917cc 1/2 VW
= Weir
=Weir 2HOA
Weir 40/50 hp 4IL
= Weiss
=(Weiss Manfréd Repülögép- és Motorgyár Rt – Manfréd Weiss Aircraft and Engine works)
Weiss WM Sh 10 – licence built Siemens-Halske Sh 10
Weiss WM Sh 11 – licence built Siemens-Halske Sh 11
Weiss WM Sh 12 – licence built Siemens-Halske Sh 12
Weiss Sport I 100-130 hp air-cooled 4-cylinder inline engines
Weiss Sport II 100-130 hp air-cooled 4-cylinder inline engines
Weiss Sport III 100-130 hp air-cooled 4-cylinder inline engines
Weiss – Bristol Jupiter VI
Weiss MW 9K Mistral (520 hp Gnome-Rhône 9Krsd)
Weiss WM-K-14A (870 hp licence built and modified Gnome-Rhône 14K Mistral Major)
Weiss WM-K-14B (910 hp and 1030 hp licence built and modified Gnome-Rhône 14K Mistral Major)
Weiss-Daimler-Benz DB 605B (for Hungarian built Messerschmitt Me 210Ca-1/C-1s).
= Welch
=(Welch Aircraft Co)
Welch O-2 (O-135)
= Wells & Adams
=Wells & Adams 50 hp
Wells & Adams 135 hp V-8 4.5 in × 6 in (110 mm × 150 mm)
= Werner
=Werner 30 hp 4-cyl in-line
= Werner & Pfleiderer
=Werner & Pfleiderer 90/95 hp 4-cyl inline 130 mm × 150 mm (5.1 in × 5.9 in)
Werner & Pfleiderer 95 hp 4-cyl inverted inline 130 mm × 150 mm (5.1 in × 5.9 in)
Werner & Pfleiderer 140/150 hp 6-cyl inline 130 mm × 160 mm (5.1 in × 6.3 in)
Werner & Pfleiderer 220 hp 8-cyl 130 mm × 150 mm (5.1 in × 5.9 in)
= Wessex
=a 130 hp 6-cylinder in-line 105 mm × 150 mm (4.1 in × 5.9 in)
= West Engineering
=West Engineering XJ38
= Westermayer
=(Oskar Westermayer)
Westermayer W-5-33
= Western
=(Western Enterprise Engine Co)
Western L-7
= Westinghouse
== Wherry
=Wherry 4-cyl rotary barrel engine
= White & Poppe
=Source: RMV
White & Poppe 23 hp 6-cyl in-line
White & Poppe 130 hp V-8 120 mm × 160 mm (4.7 in × 6.3 in)
= Whitehead
=Source: RMV
Whitehead 1910 40 hp
Whitehead 1910 75 hp
= Wickner
=Wickner Wicko F
= Wiley Post
=Wiley Post AL-1000
= Wilksch
=Source: RMV
Wilksch WAM100
Wilksch WAM120
Wilksch WAM160
= Williams
=a water-cooled 125 hp V-8
= Williams International
=Source: RMV
= Wills
=(C. Howard Wills)
WBB V-4 2-stroke for Sperry aerial torpedo
= Winterthur
=(The Swiss Locomotive and machine Works)
Winterthur V-8
Winterthur V-12
= Wisconsin
=140 hp 6-cyl in-line 5 in × 6.5 in (130 mm × 170 mm)
250 hp V-125 in × 6.5 in (130 mm × 170 mm)
= Woelfe Aixro
=Woelfe Aixro XF40
= Wojcicli
=(S.Wojcicli)
Wojcicli 10 kg pulsejet
Wojcicli 20 kg pulsejet
Wojcicli 40 kg pulsejet
Wojcicli 70 kg pulsejet
Wojcicli 11 kg ramjet
Wojcicli 200 kg ramjet
= Wolseley
=Source: Lumsden.
Wolseley 30 hp 4-cylinder
Wolseley 50 hp V-8 air-cooled
Wolseley 54 hp V-8 water-cooled 3.75 in × 5 in (95 mm × 127 mm)
Wolseley 60 hp, also known as Type C – V-8 water-cooled 3.75 in × 5 in (95 mm × 127 mm)
80 hp "Type B"
Wolseley 75 hp V-8 air-cooled 3.75 in × 5.5 in (95 mm × 140 mm)
Wolseley 90 hp V-8 air-cooled 4 in × 5.5 in (100 mm × 140 mm)
Wolseley 90 hp V-8 water-cooled 3.75 in × 5.5 in (95 mm × 140 mm)
Wolseley 120/150 hp V-8 water-cooled 5 in × 7 in (130 mm × 180 mm)
Wolseley 1911 Type A V-8
Wolseley 1911 Type D V-8
Wolseley 160 hp – 1912 V-8
Wolseley Aquarius, also known as Wolseley AR7
Wolseley Aries, also known as Wolseley AR9
Wolseley Leo
Wolseley Libra
Wolseley Scorpio
Wolseley Viper – licence built Hispano Suiza HS-8
Wolseley Python 4.72 in × 5.51 in (120 mm × 140 mm)
Wolseley Adder
= Wright
== Wright Company
=Wright Vertical 4
= Wright-Gypsy
=Wright-Gypsy L-320
= Wright-Hisso
=(Wright-Martin/Wright-Hisso)
Wright-Hisso A
Wright-Hisso B 4-cyl in-line water-cooled 56 kW (75 hp) 120 mm × 130 mm (4.7 in × 5.1 in)
Wright-Hisso C 150 kW (200 hp) geared A
Wright-Hisso D 150 kW (200 hp) geared A with cannon
Wright-Hisso E 130 kW (180 hp) (HC 'I')
Wright-Hisso E-2 (HC 'E')
Wright-Hisso E-3
Wright-Hisso E-4
Wright-Hisso F ('D' without cannon)
Wright-Hisso H 220 kW (300 hp)
Wright-Hisso H-2 improved 'H'
Wright-Hisso I
Wright-Hisso K H with 37mm Baldwin cannon
Wright-Hisso K-2
Wright-Hisso M experimental 300 hp
Wright-Hisso T
Wright-Hisso 180 hp V-8 direct drive
Wright-Hisso 220 hp V-8 geared drive
Wright-Hisso 300 hp V-8 geared drive
= Wright-Morehouse
=Wright-Morehouse 2-cyl horizontally opposed 26 hp (Lincoln Rocket)
= Wright-Siemens
=Wright-Siemens Sh-14
= Wright-Tuttle
=Wright-Tuttle WT-5
= Wynne
=(William Wynne)
(The Corvair Authority)
Wynne O-164B 100 HP
Wynne O-164-BE 110 HP
Wynne TSIO-164-BE 145 HP
X
= XCOR Aerospace
=XCOR XR-4A3
XCOR XR-4K14
= Xian
=Xian WS-9 ("Qinling")
Xian WS-15 ("Emei")
Y
= Yamaha
=Yamaha KT100
= York
=(Jo York)
York 4-cyl in-line
= Yuneec International
=Yuneec Power Drive 10
Yuneec Power Drive 20
Yuneec Power Drive 40
Yuneec Power Drive 60
Z
= Zanzottera
=Zanzottera MZ 34
Zanzottera MZ 100
Zanzottera MZ 201
Zanzottera MZ 202
Zanzottera MZ 301
Zanzottera MZ 313
= Z.B.
=(Ceskoslovenska Zbrojovka A.S. Brno / Zbrojovka Brno)
Z.B. ZOD-260
= Zeitlin
=(Joseph Zeitlin)
Zeitlin 220 hp 7-cyl rotary 135 mm (5.3 in) bore, variable stroke
= Zenoah
=Zenoah G-25
Zenoah G-50
Zenoah G-72
= Zhuzhou
=(Zhuzhou Aeroengine Factory -ZEF now South Motive Power and Machinery Complex (SMPMC))
ZEF HS-5
ZEF HS-6
ZEF WZ-8
ZEF WZ-9
ZEF WZ-16
= Zlin
=Source:
Zlin Persy
Zlin Persy II
Zlin Persy III
Zlin Toma 4
Zlin Toma 6
= Zoche
=Zoche Z 01
Zoche Z 02
Zoche Z 03
Zoche Z 04
= ZOD
=(Československá zbrojovka Brno – ZOD)
ZOD-240 (2-stroke radial)
ZOD-260 (2-stroke radial)
= Zündapp
=Zündapp 9–090
Zündapp 9-092
See also
United States military aircraft engine designations
Notes
References
Angle, Glenn D. (1921). Airplane Engine Encyclopedia. Dayton, Ohio: The Otterbein Press.
Lumsden, Alec (2003). British Piston Engines and their Aircraft. Marlborough, Wiltshire: Airlife Publishing. ISBN 978-1-85310-294-3.
Kotelnikov, Vladimir (2005). Russian Piston Aero Engines. Marlborough: The Crowood Press. ISBN 978-1-86126-702-3.
Vidal, Miguel Ricardo (2012). El Motor de Aviación de la A a la Z (in Spanish). Aeroteca. ISBN 978-84-612-7902-9.
Further reading
External links
Zlin Website
Kata Kunci Pencarian:
- Turbomeca Marboré
- Turbomeca Palouste
- Turbomeca Gabizo
- Turbomeca Palas
- SNECMA Atar
- ADM-20 Quail
- Boeing B-17 Flying Fortress
- F-4 Phantom II
- Dassault MD 315 Flamant
- British Aerospace BAe 125
- List of aircraft engines
- List of aircraft engine manufacturers
- Clerget aircraft engines
- List of aircraft engines of Germany during World War II
- List of Chinese aircraft engines
- List of aircraft
- Aircraft diesel engine
- Walter Aircraft Engines
- MTU Aero Engines
- List of BMW engines
