Accession Number:

AD0831451

Title:

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

Descriptive Note:

Corporate Author:

ASSISTANT CHIEF OF STAFF FOR INTELLIGENCE (ARMY) WASHINGTON DC

Personal Author(s):

• Chistyakov, A. A.

Report Date:

1968-01-01

Pagination or Media Count:

21.0

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