Английская Википедия:Avia M 337
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The Avia M 337 (originally designated the Walter M337) is an inverted six-cylinder air-cooled inline engine. It was developed by the Czechoslovak company as a six-cylinder derivative of the four-cylinder M 332 engine, going into production in 1960. An unsupercharged version of the M 337 is designated as the LOM M137. Production transferred to Avia in 1964, and to Letecke Opravny Malesice (LOM) in 1992.
Variants
- M 337A
- Basic supercharged engine - not rated for aerobatics
- M 337R
- Modified for pusher installation
- M 337AK
- modified oil system for unlimited inverted flying. "Snap" aerobatics permitted.
- M 337AK1
- AK fitted with alternator instead of generator
- M 337B
- Increased max running speed (3000 rpm) - increased power - Шаблон:Cvt.
- M 337BK
- Aerobatic version of B.
- M 337C
- Increased compression ratio - Шаблон:Cvt
- M 137A
- Unsupercharged version of M 337 Шаблон:Cvt take-off power. Aerobatics allowed.
- M 137AZ
- As M 137A, with filtered air feed
- M 437
- Gear ratio 0.7:1 Шаблон:Cvt
Applications
Specifications (M 337)
References
Шаблон:Commons category Шаблон:Reflist
Шаблон:Avia aeroengines Шаблон:Walter aeroengines
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- Английская Википедия
- Aircraft air-cooled inline piston engines
- 1960s aircraft piston engines
- Inverted aircraft piston engines
- Walter aircraft engines
- LOM Praha aircraft engines
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