ULPower UL260i
From Wikipedia, the free encyclopedia
The ULPower UL260i is a lightweight, 4-cylinder, 4-stroke, horizontally opposed, aircooled aircraft engine, produced by ULPower in Belgium. The engine is direct drive and features fuel injection and FADEC.
Applications
- A2 CZ Elipse Spirit
- Aerocomp VM-1 Esqual
- BRM Aero Bristell
- Corvus Fusion
- Kohl Mythos
- Lanitz Escapade Two
- Micro Aviation Bantam
- Reality Escapade UK
- Trixy G 4-2 R
Specifications
General characteristics
- Type: Flat-4
- Bore: 105.6 mm (4.157 in)
- Stroke: 74 mm (2.91 in)
- Displacement: 2,592 cm³ (158.17 in³)
- Length: 540 mm (21.3 in)
- Width: 654 mm (25.7 in)
- Height: 472 mm (18.6 in)
- Dry weight: 74.5 kg (164.2 lbs) with exhaust, starter motor, alternator, injection & ignition system, oil cooler, oil, fuel pump and filters - fully installed & operational
Components
- Valvetrain: single central camshaft, solid lifters, pushrods, rockers and OHV
- Fuel system: Electronic Fuel Injection
- Fuel type: Mogas (95 Oct.RON / 91 AKI min.) / AVGAS
- Oil system: Wet sump
- Cooling system: Aircooled
Performance
- Power output: 71 kW (95 hp) at 3,300 RPM
- Compression ratio: 8.16:1
- Fuel consumption: 12 liters/h at typical cruise of 2,500 RPM
- Specific fuel consumption: 180-200 g/hp/h
- Oil consumption: close to none
- Power-to-weight ratio: 0.95 kW/kg (fully operational)
See also
Comparable engines:
References
External links
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