avia.wikisort.org - Engine

Search / Calendar

The ULPower UL350i is a Belgian aircraft engine, designed and produced by ULPower Aero Engines of Geluveld for use in ultralight and homebuilt aircraft.[1]

UL350i
Type Aircraft engine
National origin Belgium
Manufacturer ULPower Aero Engines

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.[1][2]


Variants


UL350i
Base model that produces 118 hp (88 kW) at 3300 rpm.[1][2]
UL350iS
Higher compression model that produces 130 hp (97 kW) at 3300 rpm.[3]
UL350iSA
Same as UL350iS but with inverted oil system for aerobatic use.[4]
UL350iHPS
Special version for helicopter use. It produces 150 hp (112 kW) at 3500 rpm.[5]

Applications



Specifications (ULPower UL350i)


Data from World Directory of Leisure Aviation 2011-12 and manufacturer[1][2][6]

General characteristics

Components

Performance


See also


Related development

Related lists


References


  1. 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. "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.





Текст в блоке "Читать" взят с сайта "Википедия" и доступен по лицензии Creative Commons Attribution-ShareAlike; в отдельных случаях могут действовать дополнительные условия.

Другой контент может иметь иную лицензию. Перед использованием материалов сайта WikiSort.org внимательно изучите правила лицензирования конкретных элементов наполнения сайта.

2019-2025
WikiSort.org - проект по пересортировке и дополнению контента Википедии