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