ULPower UL350i
| Industry | Aerospace |
|---|---|
| Headquarters | Geluveld , Belgium |
| Products | Aircraft engines |
Template:Infobox aero engine The ULPower UL350i is an aircraft engine originating from Belgium, engineered and manufactured by ULPower Aero Engines based in Geluveld. It is intended primarily for use in ultralight and homebuilt aircraft.[1]
Design and development
This powerplant features a four-cylinder, four-stroke, horizontally opposed configuration with a displacement of 3,503 cc (213.8 cu in). It operates on air cooling and utilizes a direct-drive system running on gasoline. The design incorporates dual electronic ignition and multi-point electronic fuel injection (EFI), delivering an output of 118 hp (88 kW) at 3300 rpm.[1][2]
Variants
- UL350i
- Standard version generating 118 hp (88 kW) at 3300 rpm.[1][2]
- UL350iS
- Model with increased compression ratio that produces 130 hp (97 kW) at 3300 rpm.[3]
- UL350iSA
- Identical to the UL350iS but equipped with an inverted oil system to support aerobatic maneuvers.[4]
- UL350iHPS
- Specialized variant tailored for helicopter applications, delivering 150 hp (112 kW) at 3500 rpm.[5]
Applications
Specifications (ULPower UL350i)
See also
References
- ↑ 1.0 1.1 1.2 Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, pages 242-243. WDLA UK, Lancaster UK, 2011. Template:ISSN
- ↑ 2.0 2.1 "UL350i". ulpower.com. Retrieved 16 July 2015.
- ↑ "UL350iS". ulpower.com. Retrieved 16 July 2015.
- ↑ "UL350iSA". UL350iSA. Retrieved 28 February 2019.
- ↑ "UL350iHPS". UL350iHPS. Retrieved 28 February 2019.
External links
Wikimedia Commons has media related to ULPower UL350i.