The engine is a six-cylinder four-stroke, in-line, 5,970 cc (364.3 cu in) displacement, air-cooled, direct drive, gasoline engine design. It employs dual magneto ignition and produces 132.4 kW (178 hp) for take-off at 2750 rpm, with a compression ratio of 6.3.[1][2]
Variants
M137A
Model for limited aerobatics, to a maximum of 5 seconds inverted flight.[1][2]
M137AZ
Model for advanced aerobatics, including inverted flight. This model can mount an air filter.[1][2]
m137, czech, aircraft, engine, designed, produced, praha, letecke, opravny, malesice, praha, prague, light, aircraft, avia, 137atype, aircraft, enginenational, origin, czech, republicmanufacturer, praha, contents, design, development, variants, applications, s. The LOM M137 is a Czech aircraft engine designed and produced by LOM Praha Letecke Opravny Malesice Praha of Prague for use in light aircraft 1 LOM M137Avia M 137AType Aircraft engineNational origin Czech RepublicManufacturer LOM Praha s p Contents 1 Design and development 2 Variants 3 Applications 4 Specifications M132A 4 1 General characteristics 4 2 Components 4 3 Performance 5 See also 6 References 7 External linksDesign and development EditThe engine is a six cylinder four stroke in line 5 970 cc 364 3 cu in displacement air cooled direct drive gasoline engine design It employs dual magneto ignition and produces 132 4 kW 178 hp for take off at 2750 rpm with a compression ratio of 6 3 1 2 Variants EditM137A Model for limited aerobatics to a maximum of 5 seconds inverted flight 1 2 M137AZ Model for advanced aerobatics including inverted flight This model can mount an air filter 1 2 Applications EditZlin Z 50Specifications M132A EditData from Tacke and manufacturer 1 2 General characteristics Type Six cylinder four stroke aircraft engine Bore 105 mm 4 1 in Stroke 115 mm 4 5 in Displacement 5 970 cc 364 3 cu in Length 1 344 mm 52 9 in Width 468 mm 18 4 in Height 688 mm 27 1 in Dry weight 146 5 kg 323 0 lb Components Fuel type gasoline Cooling system air Reduction gear nonePerformance Power output 132 9 kW 178 hp for takeoff 117 6 kW 158 hp continuous Compression ratio 6 3 1See also EditRelated development LOM M337 LOM M132Related lists List of aircraft enginesReferences Edit 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 a b c d LOM Praha M137A M137AZ www pistovemotory cz Retrieved 19 March 2018 External links EditOfficial website Retrieved from https en wikipedia org w index php title LOM M137 amp oldid 1021136310, wikipedia, wiki, book, books, library,
