ULPower UL350i

{{Infobox Aircraft Begin

| name=UL350i

| image=File:UL350iS.jpg

| caption=

}}{{Infobox Aircraft Engine

|type=Aircraft engine

|manufacturer=ULPower Aero Engines

|designer=

|national origin=Belgium

|first run=

|major applications=

|produced=

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The ULPower UL350i is a Belgian aircraft engine, designed and produced by ULPower Aero Engines of Geluveld for use in ultralight and homebuilt aircraft.Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, pages 242-243. WDLA UK, Lancaster UK, 2011. {{ISSN|1368-485X}}

Design and development

The engine is a four-cylinder, four-stroke, horizontally-opposed, {{convert|3503|cc|cuin|1|abbr=on}}, air-cooled, direct drive, gasoline engine design. It employs dual electronic ignition, multi-point EFI and produces {{convert|118|hp|kW|0|abbr=on}} at 3300 rpm.{{cite web|url=http://www.ulpower.com/engines/ul350i|title=UL350i|work=ulpower.com|access-date=16 July 2015}}

Variants

;UL350i

:Base model that produces {{convert|118|hp|kW|0|abbr=on}} at 3300 rpm.

;UL350iS

:Higher compression model that produces {{convert|130|hp|kW|0|abbr=on}} at 3300 rpm.{{cite web|url=http://www.ulpower.com/engines/ul350is|title=UL350iS|work=ulpower.com|access-date=16 July 2015}}

;UL350iSA

:Same as UL350iS but with inverted oil system for aerobatic use.{{cite web |title=UL350iSA |url=http://ulpower.com/en/engines/ul350/ul350isa |website=UL350iSA |access-date=28 February 2019}}

;UL350iHPS

:Special version for helicopter use. It produces {{convert|150|hp|kW|0|abbr=on}} at 3500 rpm.{{cite web |title=UL350iHPS |url=http://ulpower.com/en/engines/ul350/ul350ihps |website=UL350iHPS |access-date=28 February 2019}}

Applications

Specifications (ULPower UL350i)

{{pistonspecs|

|ref=World Directory of Leisure Aviation 2011-12 and manufacturer{{cite web|url = http://www.ulpower.com/sites/default/files/manuals/UL350iS-operating-manual.pdf|title = Operating Manual|access-date = 16 July 2015|author= ULPower|work = ulpower.com|date = 15 September 2014}}

|type=Four cylinder, four stroke aircraft engine

|bore={{convert|105.6|mm|in|1|abbr=on}}

|stroke={{convert|100|mm|in|1|abbr=on}}

|displacement={{convert|3503|cc|cuin|1|abbr=on}}

|length={{convert|553|mm|in|1|abbr=on}}

|diameter=

|width={{convert|735|mm|in|1|abbr=on}}

|height={{convert|500|mm|in|1|abbr=on}}

|weight={{convert|80|kg|lb|1|abbr=on}}

|valvetrain=

|supercharger=

|turbocharger=

|fuelsystem=

|fueltype=Regular unleaded automotive gasoline, minimum 95 Octane RON (87 MON = 91 AKI) or 100LL avgas may be used

|oilsystem=

|coolingsystem=air

|power={{convert|118|hp|kW|0|abbr=on}} at 3300 rpm

|specpower=

|compression=8.0:1 and 8.7:1 (S versions)

|fuelcon=

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See also

{{aircontent

|see also=

|related=*ULPower UL260i

|similar aircraft=

|lists= *List of aircraft engines

}}

References

{{Reflist}}