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LOM M132

From Wikipedia, the free encyclopedia

Type Aircraft engine
National origin Czech Republic
Manufacturer LOM Praha s.p.

The LOM M132 is a Czech aircraft engine, designed and produced by LOM Praha (Letecke Opravny Malesice, Praha) of Prague for use in light aircraft.[1]

Design and development

The engine is a four-cylinder four-stroke, in-line, 3,980 cc (242.9 cu in) displacement, air-cooled, direct drive gasoline engine design. It employs dual magneto ignition and produces 90 kW (121 hp) for take-off at 2700 rpm, with a compression ratio of 6.3.[1][2]

Variants

M132A
Model for limited aerobatics, to a maximum of 5 seconds inverted flight.[1][2]
M132AK
Model for advanced aerobatics, including inverted flight.[1][2]

Applications

Specifications (M132A)

Data from Tacke and manufacturer[1][2]

General characteristics

  • Type: Four cylinder, four stroke aircraft engine
  • Bore: 105 mm (4.1 in)
  • Stroke: 115 mm (4.5 in)
  • Displacement: 3,980 cc (242.9 cu in)
  • Length: 1,052 mm (41.4 in)
  • Width: 425 mm (16.7 in)
  • Height: 688 mm (27.1 in)
  • Dry weight: 105 kg (231.5 lb)

Components

Performance

  • Power output: 90 kW (121 hp) for takeoff, 80 kW (107 hp) continuous
  • Compression ratio: 6.3:1

See also

Related development

Related lists

References

  1. ^ a b c d e Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, pages 258-259. Flying Pages Europe SARL, 2015. ISSN 1368-485X
  2. ^ a b c d LOM Praha. "M132A / M132AK". www.pistovemotory.cz. Retrieved 19 March 2018.

External links

This page was last edited on 8 May 2019, at 01:00
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