ULPower UL260i

Source: Wikipedia, the free encyclopedia.
UL260i
Type Piston aircraft engine
Manufacturer
ULPower
Major applications
Micro Aviation Bantam

The ULPower UL260i is a family of

ULPower
in Belgium.

Design

The UL260i series are all lightweight, four-cylinder,

horizontally-opposed, air-cooled, direct drive engine designs that feature FADEC with multipoint fuel injection and dual ignition systems.[1]

Variants

UL260i
Base model, fuel injection, compression ratio of 8.16:1, producing 97 hp (72 kW)[1][2]
UL260iS
Model with a higher compression ratio of 9.10:1, fuel injection, producing 107 hp (80 kW)[3]
UL260iSA
Aerobatic model with a higher compression ratio of 9.10:1, fuel injection, producing 107 hp (80 kW)[4]
UL260iF
Model with a higher compression ratio of 9.10:1, fuel injection, producing 100 hp (75 kW), due to French regulatory requirements.[5]

Applications

Specifications

Data from Tacke[1]

General characteristics

  • Type:
    Flat-4
  • Bore: 106 mm (4.2 in)
  • Stroke: 74 mm (2.9 in)
  • Displacement: 2,592 cm3 (158.2 cu in)
  • Length: 543 mm (21.4 in)
  • Width: 654 mm (25.7 in)
  • Height: 475 mm (18.7 in)
  • Dry weight
    :
    72 kg (159 lb)

Components

  • Valvetrain: single central camshaft, solid lifters, pushrods, rockers and OHV
  • Fuel system: dual
    electronic fuel injection
  • Fuel type: Mogas (95 Oct.RON / 91 AKI min.) / AVGAS
  • Oil system: Wet sump
  • Cooling system:
    Air-cooled

Performance

See also

Related development
Lists
Comparable engines

References

  1. ^
    ISSN 1368-485X
  2. ^ ULPower Aero Engines. "UL260i". ulpower.com. Retrieved 21 April 2018.
  3. ^ ULPower Aero Engines. "UL260iS". ulpower.com. Retrieved 21 April 2018.
  4. ^ ULPower Aero Engines. "UL260iSA". ulpower.com. Retrieved 21 April 2018.
  5. ^ ULPower Aero Engines. "UL260iF". ulpower.com. Retrieved 21 April 2018.
  6. ^ ULPower installation, Onex

External links