Accession Number : AD0693852

Title :   INVESTIGATION OF AN INDEPENDENT COOLING SYSTEM FOR A GAS TURBINE,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Manushin,E. A. ; Pugin,G. A.

Report Date : 22 MAY 1969

Pagination or Media Count : 14

Abstract : The necessity for experimental study on an autonomous cooling system for gas turbine rotor blades is examined. The design and technological peculiarities of a test facility for investigating a high-temperature turbine with an independent cooling system are described, and investigation problems are presented. (Author)

Descriptors :   (*GAS TURBINES, *COOLING), GAS TURBINE BLADES, HEAT TRANSFER, COOLANTS, USSR

Subject Categories : Thermodynamics
      Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE