The Avia M 332 (originally known as the Walter M332) is an air-cooled four-cylinder inverted inline engine. It was designed by Bohumil Šimůnek, of Motorlet Walter Aircraft Engines, as a more powerful replacement for the four-cylinder Walter Minor engine, going into production in 1958. Piston aircraft engine production was transferred from Walter to Avia in 1964, the engine becoming the Avia M 332.
Taylor, John W R, ed. (1971). Jane's All The World's Aircraft 1971-72. London: Sampson Low. ISBN0-354-00094-2.
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Moravia Inc
January 29, 2023
avia, originally, known, walter, m332, cooled, four, cylinder, inverted, inline, engine, designed, bohumil, Šimůnek, motorlet, walter, aircraft, engines, more, powerful, replacement, four, cylinder, walter, minor, engine, going, into, production, 1958, piston,. The Avia M 332 originally known as the Walter M332 is an air cooled four cylinder inverted inline engine It was designed by Bohumil Simunek of Motorlet Walter Aircraft Engines as a more powerful replacement for the four cylinder Walter Minor engine going into production in 1958 Piston aircraft engine production was transferred from Walter to Avia in 1964 the engine becoming the Avia M 332 M 332Type four cylinder inverted inline piston engineNational origin CzechoslovakiaManufacturer Walter Aircraft Engines Avia LOMDesigner Bohumil SimunekMajor applications Aero 145Orlican L 40 Meta Sokol Contents 1 Applications 2 Specifications 2 1 General characteristics 2 2 Components 2 3 Performance 3 See also 4 References 5 External linksApplications EditAero 145 Carlson Criquet Frontier MD II Fry Esprit VFII Kharkov KhAI 24 Orlican L 40 Meta Sokol Rolandas Kalinauskas RK 5 RuthSpecifications EditData from Jane s All The World s Aircraft 1971 72 1 General characteristics Type 4 cylinder inverted air cooled supercharged inline engine Bore 105 mm 4 13 in Stroke 115 mm 4 53 in Displacement 3 98 L 247 9 in Length 1 102 mm 43 4 in Width 425 mm 16 7 in Height 628 mm 24 7in Dry weight 102 kg 225 lb Components Valvetrain two camshaft operated valves per cylinder sodium filled exhaust valve Supercharger Centrifugal Fuel system Low pressure fuel injection Fuel type Min 72 octane unleaded or 80 octane leaded Oil system Dry sump pressure feed Cooling system Air coolingPerformance Power output 104 kW 140 hp at 2 700 rpm take off See also EditRelated lists List of aircraft enginesReferences Edit J W R Taylor 1971 pp 629 630 Taylor John W R ed 1971 Jane s All The World s Aircraft 1971 72 London Sampson Low ISBN 0 354 00094 2 External links EditMoravia Inc Retrieved from https en wikipedia org w index php title Avia M 332 amp oldid 1102337976, wikipedia, wiki, book, books, library,