- Source: ULPower UL260i
The ULPower UL260i is a family of aircraft engines, produced by ULPower in Belgium.
Design
The UL260i series are all lightweight, four-cylinder, four-stroke, horizontally-opposed, air-cooled, direct drive engine designs that feature FADEC with multipoint fuel injection and dual ignition systems.
Variants
UL260i
Base model, fuel injection, compression ratio of 8.16:1, producing 97 hp (72 kW)
UL260iS
Model with a higher compression ratio of 9.10:1, fuel injection, producing 107 hp (80 kW)
UL260iSA
Aerobatic model with a higher compression ratio of 9.10:1, fuel injection, producing 107 hp (80 kW)
UL260iF
Model with a higher compression ratio of 9.10:1, fuel injection, producing 100 hp (75 kW), due to French regulatory requirements.
Applications
Specifications
Data from Tacke
= General characteristics
=Type: Flat-4
Bore: 106 mm (4.2 in)
Stroke: 74 mm (2.9 in)
Displacement: 2,592 cm3 (158.2 cu in)
Length: 543 mm (21.4 in)
Width: 654 mm (25.7 in)
Height: 475 mm (18.7 in)
Dry weight: 72 kg (159 lb)
= Components
=Valvetrain: single central camshaft, solid lifters, pushrods, rockers and OHV
Fuel system: dual electronic fuel injection
Fuel type: Mogas (95 Oct.RON / 91 AKI min.) / AVGAS
Oil system: Wet sump
Cooling system: Air-cooled
= Performance
=Power output: 95 hp (70.8 kW) at 3,300 RPM
Compression ratio: 8.16:1
See also
Related development
ULPower UL350i
Lists
List of aircraft engines
Comparable engines
HKS 700E
Jabiru 2200
KFM 112M
Pegasus PAL 95
Revmaster R-2300
Rotax 912
Sauer S 2200 UL
Sauer S 2400 UL
Sauer S 2100 ULT
References
External links
Official website
Kata Kunci Pencarian:
- ULPower UL260i
- ULPower UL350i
- ULPower Aero Engines
- Rotax 912
- Flat-four engine
- KFM 112M
- Weslake A80
- HKS 700E
- Lambert Mission 106
- Aerocomp VM-1 Esqual
