ULPower UL350i

UL350i
TypeAircraft engine
National originBelgium
ManufacturerULPower Aero Engines

The ULPower UL350i is a Belgian aircraft engine, designed and produced by ULPower Aero Engines of Geluveld for use in ultralight and homebuilt aircraft.

Design and development

The engine is a four-cylinder, four-stroke, horizontally-opposed, 3,503 cc (213.8 cu in), air-cooled, direct drive, gasoline engine design. It employs dual electronic ignition, multi-point EFI and produces 118 hp (88 kW) at 3300 rpm.

Variants

UL350i
Base model that produces 118 hp (88 kW) at 3300 rpm.
UL350iS
Higher compression model that produces 130 hp (97 kW) at 3300 rpm.
UL350iSA
Same as UL350iS but with inverted oil system for aerobatic use.
UL350iHPS
Special version for helicopter use. It produces 150 hp (112 kW) at 3500 rpm.

Applications

Specifications (ULPower UL350i)

Data from World Directory of Leisure Aviation 2011-12 and manufacturer

General characteristics

Components

Performance

See also

Related development

Related lists

References

  1. 1 2 3 4 Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, pages 242-243. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
  2. 1 2 3 "UL350i". ulpower.com. Retrieved 16 July 2015.
  3. ↑ "UL350iS". ulpower.com. Retrieved 16 July 2015.
  4. ↑ "UL350iSA". UL350iSA. Retrieved 28 February 2019.
  5. ↑ "UL350iHPS". UL350iHPS. Retrieved 28 February 2019.
  6. ↑ ULPower (15 September 2014). "Operating Manual" (PDF). ulpower.com. Retrieved 16 July 2015.