Accession Number : AD0711757

Title :   AVIATION GAS TURBINE ENGINES. CONSTRUCTION AND DESIGN OF PARTS,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Skubachevskii,G. S.

Report Date : 19 JUN 1970

Pagination or Media Count : 852

Abstract : In the textbook design fundamentals of aviation gas turbine engines are expounded. There is an examination of operating conditions of individual subassemblies of engines and their parts and the demands imposed on them, construction of parts, strength and vibration calculations; requirements are presented for materials from which parts are prepared, and certain technological indications are outlined. Examples of strength and vibration calculations of basic parts of gas turbine engines are provided. The third edition includes up-dated examples of engine structures and their parts, new methods for calculating strength and vibration and examples of calculations are given. The textbook is intended for students of aviation technical institutes.

Descriptors :   (*GAS TURBINES, TURBINE PARTS), (*TURBINE PARTS, DESIGN), TURBOJET ENGINES, TURBOPROP ENGINES, AXIAL FLOW COMPRESSORS, CENTRIFUGAL COMPRESSORS, MECHANICAL PROPERTIES, VIBRATION, ROTATION, OSCILLATION, DAMPING, EXHAUST NOZZLES, COMBUSTION CHAMBERS, GEARS, LUBRICATION, TEXTBOOKS, USSR

Subject Categories : Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE