ULPower UL260i
 | This article includes a list of general references, but it lacks sufficient corresponding inline citations. (September 2011) |
| UL260i | |
|---|---|
| |
| A ULPower UL260i aero engine | |
| Type | Piston aircraft engine |
| Manufacturer | ULPower |
| Major applications | Micro Aviation Bantam |
The ULPower UL260i is a lightweight, 4-cylinder, 4-stroke, horizontally opposed, air-cooled aircraft engine, produced by ULPower in Belgium. The engine is direct drive and features FADEC with multipoint fuel injection and double ignition.
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
- Sonex Aircraft Onex[1]
- 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 (158.2 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: Air-cooled
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
- Related development
- Lists
- 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
- ^ ULPower installation, Onex
External links
Wikimedia Commons has media related to ULPower UL260i.