Accession Number : AD0164450

Title :   V/Stol Aircraft-by-Pass Engine Having a Double, Thrust Diverter Valve Assembly.

Descriptive Note : Patent,

Corporate Author : DEPARTMENT OF THE AIR FORCE WASHINGTON D C

Personal Author(s) : Stevens,Emerson W.

Report Date : 24 JUL 1973

Pagination or Media Count : 7

Abstract : The invention relates generally to the application of the by-pass or turbofan engine to VTOL and/or V/STOL aircraft and, in particular, to an improved thrust diverter valve assembly therefor.

Descriptors :   *Jet engines, *Bypass valves, *Patents, Short takeoff aircraft, Turbofan engines, Thrust control, Cascade structures

Subject Categories : Pumps, Filters, Pipes, Tubing, Fittings & Vlvs
      Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE