A Two-Cascade Fuel Jet for a Gas Turbine Engine,

Abstract

The report describes a Soviet patent for a gas turbine fuel nozzle designed to maintain pressurization at high temperatures.

Document Details

Document Type
Technical Report
Publication Date
Aug 06, 1973
Accession Number
AD0765578

Entities

People

  • E. E. Luss
  • M. A. Shamban
  • M. P. Khayurov
  • N. S. Akinshin

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Energy Generators
  • Energy Systems
  • Engines
  • Fuel Nozzles
  • Gas Turbines
  • Generators
  • High Temperature
  • Mechanical Equipment
  • Nozzles
  • Pressurization
  • Turbine Components
  • Turbines

Fields of Study

  • Physics