Accession Number : AD0674399

Title :   MIXER AND EXHAUST NOZZLE OF GAS TURBINE COMBUSTION CHAMBERS (SMESITEL I VYKHODNOI PATRUBOK KAMER SGORANIYA GAZOTURBINNOI USTANOVKI),

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Kovalevskii,M. M. ; Gorshkov,V. N. ; Zatkovetskii,G. N. ; Kumkov,P. A. ; Shulman,V. L.

Report Date : 03 NOV 1967

Pagination or Media Count : 6

Abstract : The proposed mixing chamber and exhaust duct is equipped with an external screen forming an annular clearance for feeding cooling air. The air then enters the mixing chamber through openings in its walls. To ensure a more uniform cooling of all combustion chamber components, the clearance is divided by a baffle which permits part of the cooling air to enter the chamber directly and the rest in a counter-flow. (Author)

Descriptors :   (*GAS TURBINES, *COMBUSTION CHAMBERS), EXHAUST NOZZLES, COOLING, GAS FLOW, DIFFUSERS, PATENTS, USSR

Subject Categories : Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE