MIXER AND EXHAUST NOZZLE OF GAS TURBINE COMBUSTION CHAMBERS (SMESITEL I VYKHODNOI PATRUBOK KAMER SGORANIYA GAZOTURBINNOI USTANOVKI),
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)
Document Details
- Document Type
- Technical Report
- Publication Date
- Nov 03, 1967
- Accession Number
- AD0674399
Entities
People
- G. N. Zatkovetskii
- M. M. Kovalevskii
- P. A. Kumkov
- V. L. Shulman
- V. N. Gorshkov
Organizations
- National Air and Space Intelligence Center