V16 GE-1015 Jane's Aero Engine March 2000.Pdf
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Copyright fees have not been paid on these materials. It is the acknowledged FEIN# E 042-103-594 responsiblllty of the requester to pay all appropriate copyright fees. GE-1015.001 GE-1015.002 Jane's AERO-ENGINES Edited by Bill Gunston OBE, FRAeS Bookmark Jane's homepage on http://www.janes.com Jane's award-winning web site provides you with continuously updated news and information. As well as extracts from our world renowned magazines, you can browse the online catalogue, visit the Press Centre, discover the origins of Jane's, use the extensive glossary, download our screen saver and much more. Jane's now offers powerful electronic solutions to meet the rapid changes in your information requirements. All our data, analysis and im;igery is available on CD-ROM or via a new secure web service - Jane's Online at www.janesonline.com. Tailored electronic delivery can be provided through Jane's Data Services. Contact an information consultant at any of our international offices to lindout how Jane's can change the way you work or e-mail us at info.janes.co.uk or [email protected] ISBN 0 71061405 5 Copyright© 2000 by Jane's Information Group Limited, Sentinel House, 163 Brighton Road, Coulsdon, Surrey CR5 2YH, UK In the USA and its dependencies Jane's Information Group Inc, 1340 Braddock Place, Suite 300, Alexandria, Virginia 22314-1651, USA Riil\!2R4 ~PUBLISHERS AS50CIATION All rights reserved. No part of this publication may be reproduced, stored in retrieval systems or transmitted in any form or by any means, electronic, mechanical, photocopying, recording or otherwise, without the prior written permission of the Publishers. Licences, particularly for use of the data in databases or local area networks are available on application to the Publishers. Infringements of any of the above rights will be liable to prosecution under UK or US civil or criminal law. 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LIBRARIES APR z7 2000 I RECEIVED GE-1015.004 Contents How to use Jane's Aero Engines (issue 7) Military jet engines: Overall pressure ratio (issue 0) Glossary (issue 1) Civil jet engines: Specific thrust (issue 0) Specific fuel consumption (Civil jet engines) (issue 0) Aircraft propulsion (issue 6) Collaborative programmes (issue 7) The turbojet (issue 6) Specific fuel consumption - Shaft Engines (issue 0) The turbofan (issue 6) Bypass Ratio (issue 3) The parts of an engine (issue 6) Civil jet engines - 1 (issue 6) Compressors (issue 6) Civil Jet I (i) (issue 6) Fans (issue 6) Civil Jet II (ii) (issue 6) Combustion chambers (issue 6) Turboshaft and turboprop engines (issue 6) Turbines (issue 6) Pressure ratio (subsonic transport engines) (issue 6) Afterburners (issue 6) Military jet markets (i) (issue 3) Reversers (issue 6) Military jet markets (ii) (issue 3) Vectoring (issue 6) Military jet engines 1 (issue 3) The spectrum from turbojet to turboprop (issue 6) Military jet engines 2 (i) (issue 3) Propfans (issue 6) Military jet engines 2 (ii) (issue 3) The installation (issue 6) Introduction to aircraft gas-turbine engine technology AERO-ENGINES - A- E (issue 1) Jet Propulsion (issue 1) Belgium The Turbojet (issue 1) TA (issue 7) Engine Thrust (issue 1) Other Engine Components (issue 1) Canada Measures of Turbojet Performance (issue 1) P&WC (issue 7) The Turbofan (issue 1) P&WC JT1 5D (issue 7) Other Aircraft Engine Configurations (issue 1) P&WC PT6A (issue 7) P&WC PT6B. PT6C. PT6D (issue 7) Technological issues in engine development (issue 0) P&WC PT6T Twin-Pac (issue 7) P&WC PW100 (issue 7) Gas-turbine engine cycles (issue 7) P&WC low-cost engine (issue 7) Thermodynamic Cycles (issue 7) P&WC PW200 (issue 7) The Aircraft Gas-Turbine Cycle (issue 7) P&WC PW300 (issue 7) Turbojet Cycle Parameters (issue 7) P&WC PW500 (issue 7) Turbojet Performance Variation with OPR and TET (issue 7) P&WC PW6XX (issue 7) Turbofan Cycle Parameters (issue 7) Turbofan Performance Variation withµ. OPR and TET (issue 7) China. People's Republic Limitations onµ. OPR and TET (issue 7) AVIC (issue 3) Turbojet and Turbofan Behaviour (issue 7) CATIC (issue 3) CAREC (issue 3) Military engines (issue 7) CEC (issue 3) Basic requirements (issue 7) CLXMW (issue 3) New materials (issue 7) DEMC (issue 7) Fewer parts (issue 7) WJ5 (issue 7) Inlets (issue 7) LM (issue 0) Variable nozzles (issue 7) LM WP6 (issue 0) Vectoring (issue 7) LM WP7 (issue 0) JSF (issue 7) LM WS6 (issue 0) Fighter engine research (issue 7) LMC (issue 0) Flight envelope (issue 7) LMC WP7B (issue 0) Helicopters (issue 7) LMC WP13 (issue 0) SAMP (issue 4) Civil engines (issue 7) SARI (issue 4) Reducing (or increasing?) costs (issue 7) SMPMC (issue 4) New or derivative? (issue 7) SPWAEC (issue 4) Fuel burn (issue 7) XAE (issue 4) Repeated re-engining (issue 7) XRA (issue 4) Fans (issue 7) Combustion chambers (issue 7) Czech Republic Turbines (issue 7) Walter (issue 7) Reversers (issue 7) Walter M601 (issue 7) Noise (issue 7) Walter M602 (issue 7) ETOPS (issue 7) Walter (Motorlet) M701 (issue 7) Props or jets (issue 7) Gearboxes (issue 7) The SST problem (issue 7) AERO-ENGINES - F - H Environmental factors (issue 0) France Noise legislation (issue 0) SNECMA (issue 7) Chapter 3 (issue 0) SNECMA ATAR (issue 7) Emissions (issue 0) SNECMA M53 (issue 7) SNECMA M88 (issue 7) Diagrams Turbomeca (issue 7) Military engine performance (issue 3) Turbomeca Arriel (issue 7) World record power (issue 3) Turbomeca Arrius (issue 7) JAEng-ISSUE 7 March 2000 [3] GE-1015.005 www .janes.com CONTENTS Turbomeca Arrius 1 D (issue 2) General Electric CF6 (issue 7) Turbomeca Artouste (issue 0) General Electric GE90 (issue 7) Turbomeca Astazou turboprop (issue 7) General Electric T64-P4D (issue 7) Turbomeca Astazou turboshaft (issue 7) General Electric T700/CT7 (issue 7) Turbomeca Aubisque (issue 7) IAE V2500 (issue 7) Turbomeca Bastan (issue 0) Pratt & Whitney PW2000 and PW4000 (issue 7) Turbomeca Makila (issue 7) Pratt & Whitney Canada PW308 (issue 7) Turbomeca Marbon~ (issue 7) Rolls-Royce Spey 807 (issue 7) Turbomeca TM 333 (issue 7) SNECMA M138 (issue 7) Turbomeca Turmo (issue 7) Turbo-Union RB 199 (issue 7) Turbomeca-SNECMA (issue 0) Piaggio (issue 7) Turbomeca-SNECMA Larzac (issue 7) Japan Germany Honda (issue 7) MTU (issue 7) HFX-01 (issue 7) Engine 3E (issue 7) HFX-20 (issue 6) Eurojet Turbo EJ200 (issue 7) IHI (issue 3) General Electric CF6 (issue 7) IHI F3 (issue 7) IAE V 2500 (issue 7) IHI XF3-400 (issue 7) M 138 (issue 7) IHI J3 (issue 0) MTFE (issue 7) Kawasaki (issue 7) MTU-Turbomeca-RR MTR390 (issue 7) KSX (issue 7) Pratt & Whitney JT8D-200 (issue 7) Mitsubishi (issue 3) P&WC PW300 (issue 7) MHI Turboshafts (issue 3) P&WC PW500 (issue 7) NAL (issue 0) Pratt & Whitney PW2000 (issue 7) MITl/NAL FJR710 (issue 7) Pratt & Whitney PW4084 (issue 7) Rolls-Royce Allison 250-C20B (issue 7) Rolls-Royce Tyne (issue 7) AERO-ENGINES - P - R Turbomeca-SNECMA Larzac (issue 7) Turbo-Union RB 199 (issue 7) Poland Rolls-Royce (issue 7) IL (issue 0) BR710 (issue 7) IL D-18A (issue 0) BR715 (issue 7) IL K-15 (issue 0) IL S0-1 (issue 0) IL S0-3 (issue 0) AERO-ENGINES - I - 0 PZL Rzesz6w (issue 7) K-1 5 (issue 7) India GTD-350 (issue 7) GTRE (issue 6) PZL-10W ~ssue 7) GTRE Kaveri (issue 6) TWD-108 (issue 7) HAL (issue 0) Romania International