Accession Number : ADD008767

Title :   Radial and Axial Flow Variable Exhaust Nozzle for a Gas Turbine Engine.

Descriptive Note : Patent,

Corporate Author : DEPARTMENT OF THE AIR FORCE WASHINGTON DC

Personal Author(s) : Wilson,Paul , Jr

Report Date : 21 Jul 1981

Pagination or Media Count : 6

Abstract : The exhaust fairings are opened during idle to direct the exhaust gases overboard in radial directions between the opened fairings. They are closed during speeds above idle to direct the exhaust gases overboard in an axial direction through an axially aligned rearwardly located exit opening of the exhaust nozzle.

Descriptors :   *Patents, *Exhaust nozzles, *Gas turbines, *Radial flow, *Axial flow, Exhaust gases, Thrust, Control systems, Fairings, Inventions

Subject Categories : Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE