• Source: General Electric T58

The General Electric T58 is an American turboshaft engine developed for helicopter use. First run in 1955, it remained in production until 1984, by which time some 6,300 units had been built. On July 1, 1959, it became the first turbine engine to gain FAA certification for civil helicopter use. The engine was license-built and further developed by de Havilland in the UK as the Gnome, in the West Germany by Klöckner-Humboldt-Deutz, and also manufactured by Alfa Romeo and the IHI Corporation.




Design and development


Development commenced with a 1953 US Navy requirement for a helicopter turboshaft to weigh under 400 lb (180 kg) while delivering 800 hp (600 kW). The engine General Electric eventually built weighed only 250 lb (110 kg) and delivered 1,050 hp (780 kW) and was soon ordered into production. First flight was on a modified Sikorsky HSS-1 in 1957, and civil certification for the CT58-100 variant was obtained two years later.
A number of unusual features are incorporated into the T58:

an all-axial compressor. Most other turboshafts in this power bracket have a centrifugal unit as a final compressor stage. As a result, the blades at the rear of the compressor are very small (less than 0.5in high) and extremely thin.
compressor handling at part speed is facilitated by several rows of variable pitch stators at the front part of the unit. This was a fairly novel feature when the engine was first introduced.
a single stage power turbine. which delivers power to the rear of the engine. The hot exhaust stream is diverted sideways, away from the output shaft.
the combustor is a straight-through annular design, rather than reverse flow.
The main production version of the engine was the T58-GE-10, developing 1,400 hp (1,044 kW). The most powerful version, the T58-GE-16, produces 1,870 hp (1,390 kW).




Variants



T58-GE-1
1,290 hp (960 kW)
T58-GE-2
1,325 hp (988 kW)
T58-GE-3
1,290 hp (960 kW)
T58-GE-4

T58-GE-5
1,500 hp (1,100 kW)
T58-GE-6
1,250 hp (930 kW)
T58-GE-8B
1,250 hp (930 kW)
T58-GE-8E
1,350 hp (1,010 kW)
T58-GE-8F
1,350 hp (1,010 kW)
T58-GE-10
1,400 hp (1,000 kW)
T58-GE-14
1,400 hp (1,000 kW) 2-stage power turbine
T58-GE-16
1,870 hp (1,390 kW)
T58-GE-100
1,500 hp (1,100 kW)
T58-GE-402
1,500 hp (1,100 kW)
CT58-100-1
1,050 hp (780 kW)
CT58-110-1
1,350 hp (1,010 kW)
CT58-140-1
1,500 hp (1,100 kW) commercial T58-GE-10
Ishikawajima-Harima CT58-IHI-110-1
1,400 hp (1,000 kW)
Ishikawajima-Harima CT58-IHI-140-1
1,400 hp (1,000 kW)
Ishikawajima-Harima T58-IHI-8B BLC
For Shin Meiwa PS-1 BLC system
Rolls-Royce Gnome
Licensed production and development of the T58 in the United Kingdom.




Applications






= Other

=
Two T58s, converted to turbojets by the removal of the power turbines, were used as the engines on the Maverick TwinJet 1200.
The Carroll Shelby turbine cars entered in the 1968 Indianapolis 500 race were powered by T58s. The cars were found to be using variable inlets to get around the USAC regulations on the maximum allowable inlet size and were disqualified.




Engines on display


There is a YT58-GE-2A cutaway on display at the New England Air Museum, Bradley International Airport, Windsor Locks, CT




Specifications (T58-GE-8)


Data from



General characteristics

Type: Free power turboshaft
Length: 55 in (1,397 mm)
Diameter: 16 in (406 mm)
Dry weight:



Components

Compressor: 10-stage axial-flow compressor with variable inlet guide vanes, and variable incidence stators in first three stages
Combustors: Annular combustion chamber with 16 burner nozzles on two manifolds
Turbine:
Fuel type: Aviation kerosene



Performance

Maximum power output: 1,250 hp (932.12 kW)
Overall pressure ratio: 8.3:1
Air mass flow: 12.4 lb/s (5.62 kg/s) at 26,300 rpm
Specific fuel consumption: 0.64 lb/(hp⋅h) (0.39 kg/(kW⋅h)) at maximum continuous rating
Power-to-weight ratio: 6.1 hp/lb (10.0 kW/kg) without reduction gearbox




See also



Related development

Rolls-Royce Gnome

Related lists

List of aircraft engines




References



Gunston, Bill (1986). World Encyclopedia of Aero Engines. Wellingborough: Patrick Stephens. p. 65.
GE Aviation T58 page Archived 2011-06-20 at the Wayback Machine and T58 history page Archived 2010-09-26 at the Wayback Machine
General Electric (September 4, 2018). 1E3. Federal Aviation Administration (FAA) (Report). Type Certificate Data Sheet (16th ed.).
Ishikawajima-Harima (August 10, 1970). E1PC. Federal Aviation Administration (FAA) (Report). Type Certificate Data Sheet (1st ed.).




External links


Minijets website

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