Accession Number : AD0831451

Title :   DETERMINING PERMISSIBLE IMBALANCES FOR THE ROTORS OF AVIATION GAS TURBINE ENGINES (OPREDELENIYE DOPUSTIMOY NEURAVNOVESHENNOSTI ROTOROV AVIATSIONNYKH GTD),

Corporate Author : ASSISTANT CHIEF OF STAFF FOR INTELLIGENCE (ARMY) WASHINGTON DC

Personal Author(s) : Chistyakov, A. A.

Report Date : 1968

Pagination or Media Count : 21

Abstract : A brief review of previous research is given. A general discussion is presented concerning the establishment of tolerances in the design of gas turbines.

Descriptors :   (*GAS TURBINE ROTORS, PERFORMANCE(ENGINEERING)), (*AIRCRAFT ENGINES, GAS TURBINES), VIBRATION, OSCILLATION, ROTATION, FAILURE, CENTER OF GRAVITY, MATHEMATICAL ANALYSIS, TOLERANCES(MECHANICS), USSR.

Subject Categories : Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE