The A.60 had a valve control mechanism and the distribution shaft seal, which had a special cover ensuring uniform cooling of the cylinders. In addition to the basic A.60, an A.60-R version was developed which featured a front reduction unit, self-centered, and an output of 145 hp at 2,500 rpm, or 1,580 rpm per minute for the propeller.[1]
Variantsedit
A.60
Standard version with direct drive, 135 hp (100.7 kW)
A.60 R.
Geared version : output 145 hp (108.1 kW) at 2,500 engine rpm driving a 0.632:1 reduction gear.
^Gunston, Bill (1989). World Encyclopaedia of Aero Engines (2nd ed.). Cambridge, England: Patrick Stephens Limited. p. 62. ISBN978-1-85260-163-8.
^Jotti, da Badia Polesine (1934). Annuario dell'aeronautica Italiana 1934. Milan: Libreria Aeronautica. p. 55.
May 15, 2024
fiat, four, cylinder, cooled, inline, engine, developed, italy, 1930s, side, view, version, type, piston, engine, national, origin, italy, manufacturer, fiat, first, 1932, contents, design, variants, applications, specifications, general, characteristics, comp. The Fiat A 60 was a four cylinder air cooled inline engine developed in Italy in the 1930s A 60 Side view of A 60 140 hp version Type Piston engine National origin Italy Manufacturer Fiat First run 1932 Contents 1 Design 2 Variants 3 Applications 4 Specifications 4 1 General characteristics 4 2 Components 4 3 Performance 5 See also 6 ReferencesDesign editThe A 60 had a valve control mechanism and the distribution shaft seal which had a special cover ensuring uniform cooling of the cylinders In addition to the basic A 60 an A 60 R version was developed which featured a front reduction unit self centered and an output of 145 hp at 2 500 rpm or 1 580 rpm per minute for the propeller 1 Variants editA 60 Standard version with direct drive 135 hp 100 7 kW A 60 R Geared version output 145 hp 108 1 kW at 2 500 engine rpm driving a 0 632 1 reduction gear Applications editFiat G 2 Fiat G 5 Caproni Ca 100Specifications editData from 2 General characteristics Type 4 cylinder air cooled inline Bore 120 mm 4 72 inches Stroke 145 mm 5 71 inches Displacement 6 560 L Dry weight 135 kg 298 kg Components Cooling system Air cooled Performance Power output 135 hp 101 kW Compression ratio 5 75 1 Power to weight ratio 225 g cv hSee also editRelated lists List of aircraft enginesReferences edit nbsp Wikimedia Commons has media related to Fiat A 60 Gunston Bill 1989 World Encyclopaedia of Aero Engines 2nd ed Cambridge England Patrick Stephens Limited p 62 ISBN 978 1 85260 163 8 Jotti da Badia Polesine 1934 Annuario dell aeronautica Italiana 1934 Milan Libreria Aeronautica p 55 Retrieved from https en wikipedia org w index php title Fiat A 60 amp oldid 1078931485, wikipedia, wiki, book, books, library,
