Accession Number : ADD006848

Title :   Turbojet Engine with Combustor Bypass.

Descriptive Note : Patent,

Corporate Author : DEPARTMENT OF THE AIR FORCE WASHINGTON DC

Personal Author(s) : Wilkinson,David B

Report Date : 29 Jan 1980

Pagination or Media Count : 3

Abstract : A propulsion system having an afterburning turbojet with the fuel supplied at the inlet to the turbojet compressor. The turbojet combustor has a bypass with a flow control connected at the inlets to the combustor and the bypass to control the amount of fuel-air mixture from the comprssor that enters the combustor. (Author)

Descriptors :   *Patents, *Turbojet engines, *Combustors, *Bypass valves, *Ducts, Inventions, Flame holders, Afterburners, Fuel air ratio, Turbojet inlets, Fuel systems, Engineering drawings

Subject Categories : Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE