From Wikipedia, the free encyclopedia
The ULPower UL260i is a family of
aircraft engines, produced by
ULPower in Belgium.
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.
[1]
- UL260i
- Base model, fuel injection, compression ratio of 8.16:1, producing 97 hp (72 kW)
[1]
[2]
- UL260iS
- Model with a higher compression ratio of 9.10:1, fuel injection, producing 107 hp (80 kW)
[3]
- UL260iSA
-
Aerobatic model with a higher compression ratio of 9.10:1, fuel injection, producing 107 hp (80 kW)
[4]
- UL260iF
- Model with a higher compression ratio of 9.10:1, fuel injection, producing 100 hp (75 kW), due to French regulatory requirements.
[5]
Data from Tacke
[1]
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
- Related development
- Lists
- Comparable engines
- ^
a
b
c Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, pages 262-263. Flying Pages Europe SARL, 2015.
ISSN
1368-485X
-
^ ULPower Aero Engines.
"UL260i". ulpower.com. Retrieved 21 April 2018.
-
^ ULPower Aero Engines.
"UL260iS". ulpower.com. Retrieved 21 April 2018.
-
^ ULPower Aero Engines.
"UL260iSA". ulpower.com. Retrieved 21 April 2018.
-
^ ULPower Aero Engines.
"UL260iF". ulpower.com. Retrieved 21 April 2018.
-
^
ULPower installation, Onex