Accession Number : AD0713041

Title :   STAND FOR TESTING A GAS-TURBINE ENGINE,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Kuznetsov,N. D. ; Semenov,E. M. ; Stenkin,E. D. ; Zinin,A. I. ; Dvorkin,Ya. I.

Report Date : 08 AUG 1970

Pagination or Media Count : 4

Abstract : The proposed stand differs from those known in that the line contains a gas-intake duct with a baffle plate to select a portion of the hot gas, which permits regulation of the flow parameters at the inlet to the tested engine. (Author)

Descriptors :   (*TEST EQUIPMENT, *GAS TURBINES), DUCTS, DESIGN, PATENTS, USSR

Subject Categories : Test Facilities, Equipment and Methods
      Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE