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ULPower UL350i

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ULPower UL350i

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

Contents

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 and produces 118 hp (88 kW) at 3300 rpm.

Variants

UL350i
Base model that produces 118 hp (88 kW) at 3300 rpm.
UL350iS
Model that produces 130 hp (97 kW) at 3300 rpm.

Applications

  • BRM Aero Bristell
  • Rans S-20 Raven
  • Rokospol Via

    • Specifications (ULPower UL350i)

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

    General characteristics

  • Type: Four cylinder, four stroke aircraft engine
  • Bore: 105.6 mm (4.2 in)
  • Stroke: 100 mm (3.9 in)
  • Displacement: 3,503 cc (213.8 cu in)
  • Length: 553 mm (21.8 in)
  • Width: 735 mm (28.9 in)
  • Height: 500 mm (19.7 in)
  • Dry weight: 80 kg (176.4 lb)

    • Components

  • Fuel type: Regular unleaded automotive gasoline, minimum 95 Octane RON (87 MON = 91 AKI) or 100LL avgas may be used
  • Cooling system: air

    • Performance

  • Power output: 118 hp (88 kW) at 3300 rpm
  • Compression ratio: 8.41:1

    • References

    ULPower UL350i Wikipedia
    (Text) CC BY-SA


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