The Soloviev D-20P, built by the Soloviev Design Bureau, was a low-bypass turbofan engine rated at 52.9 kN (11,900 lbf) thrust used on the Tupolev Tu-124. Elements of the design were used in the development of the larger Soloviev D-30 family of low and medium bypass engines.[1]
Gunston, Bill. World Encyclopedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. ISBN 1-85260-163-9
Taylor, John W.R. Jane's All the World's Aircraft 1972-73., London, Sampson Low, Marston and Company Ltd, 1972. ISBN 978-0354001090.
January 01, 1970
soloviev, built, soloviev, design, bureau, bypass, turbofan, engine, rated, thrust, used, tupolev, elements, design, were, used, development, larger, soloviev, family, medium, bypass, engines, left, side, view, engine, type, turbofan, manufacturer, soloviev, d. The Soloviev D 20P built by the Soloviev Design Bureau was a low bypass turbofan engine rated at 52 9 kN 11 900 lbf thrust used on the Tupolev Tu 124 Elements of the design were used in the development of the larger Soloviev D 30 family of low and medium bypass engines 1 D 20 Left side view of the Soloviev D 20 engine Type Turbofan Manufacturer Soloviev Design Bureau Major applications Tupolev Tu 124 Contents 1 Specifications 1 1 General characteristics 1 2 Components 1 3 Performance 2 See also 3 References 3 1 Notes 3 2 BibliographySpecifications editData from Gunston and Jane s 2 3 General characteristics Type Twin spool turbofan engine Length 330 4 cm 130 in Diameter 97 6 cm 38 3 in Dry weight 1 468 kg 3 236 lb Components Compressor Three stage LP eight stage HP axial flow Combustors 12 chamber cannular Turbine Two stage LP turbine single stage HP turbine Fuel type Avtur Performance Maximum thrust 5 400 kg 11 905 lb Overall pressure ratio 13 1 Bypass ratio 1 1 Air mass flow 113 kg s 249 lb s at 8 550 rpm Specific fuel consumption 0 72 Max take off 0 9 cruise Thrust to weight ratio 3 7See also editComparable engines Rolls Royce Spey Related lists List of aircraft enginesReferences edit nbsp Wikimedia Commons has media related to Soloviev D 20 Notes edit Taylor 1972 p 752 Gunston 1989 p 164 Taylor 1972 p 751 Bibliography edit Gunston Bill World Encyclopedia of Aero Engines Cambridge England Patrick Stephens Limited 1989 ISBN 1 85260 163 9 Taylor John W R Jane s All the World s Aircraft 1972 73 London Sampson Low Marston and Company Ltd 1972 ISBN 978 0354001090 Retrieved from https en wikipedia org w index php title Soloviev D 20 amp oldid 1165154270, wikipedia, wiki, book, books, library,
