THE AIRCRAFT Gas Turbine Engine AND ITS OPERATION : INSTALLATION ENGINEERING (COPY No. 2)
PWA Oper. Instr. 200
Bok · Engelsk · 1960
| Utgitt | East Hartford, Connecticut : United Aircraft Corporation , 1960
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| Omfang | 201 s. : ill.
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| Opplysninger | Published 1951, United Aircraft Corporation. June 1952. Rewritten November 1960 Fifth Printing August 1967. - TABLE OF CONTENTS: PREFACE SECTION I - GAS TURBINE ENGINE FUNDAMENTALS A Basic Understanding is Necessary The Flight Spectrum The Basic Gas Turbine Engine How The Gas Turbine Operates Thrust Factors Affecting Thrust Gas Generator Mach Number Thrust Specific Fuel Consumption Engine Station Designations Diffusers and Diffusion Types of Gas Turbine Engines SECTION II - GAS TURBINE ENGINE COMPONENTS Turboprop And Turboshaft Engine Nose Sections Air-Inlet Duct Turbofan-Engine Fan Sections Compressors Diffusers Fuel Manifold And Nozzles Burner Section Turbines Exhaust Ducts Thrust Reversers Engine Noise - Suppressors Afterburners Accessories Starters Fuel System Controls And Propeller - Governors Lubrication Systems Ignition Systems Engine Cooling Engine Insulation Blankets Liquid Injections Protection Against Icing Turboprop Asymmetric Thrust Control Deivces Turboprop Engine Brakes SECTION III - GAS TURBINE ENGINE PERFORMANCE Definitions And Symbols Laws Governing Energy Exchanges Basic Internal Aerodynamics And Thermodynamics Basic Engine Performance Analysis Component Performance Details SECTION IV - GAS TURBINE ENGINE OPERATION Engine Ratings Engine Operating Variable For Setting Thrust Engine Instrumentation Preflight And Starting Take-Off Climb Cruise Letdown, Approach And Landing Engine Shutdown Emergencies Turboprop Operation SECTION V - ENGINE OPERATIONAL CHARACTERISTICS Cleaning Engine Air-Passages Compressor Stal Engine-Inlet Anti-Icing Engine Ratings, Thrust-Settings and Limits Exhaust Gas Temperature Fuels Lubricants Trimming P&WA Axial - Compressor Engines Turbojet, Turboprop And Turbofan Characteristics
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| Emner |