Accession Number : AD0164076
Title : Combustion Air Control Shutter.
Descriptive Note : Patent,
Corporate Author : DEPARTMENT OF THE NAVY WASHINGTON D C
Personal Author(s) : Pillsbury,Paul W. ; Suter,Jeffrey K.
Report Date : 20 JAN 1970
Pagination or Media Count : 3
Abstract : The patent relates to a device whereby a turbojet combustor is provided with scoop ducts mounted on a rotary shutter to control injection of additional air to the burner dome. At low altitude, when smoke is objectionable, the pilot causes rotation of the shutter. The scoop ducts are tilted to produce a swirling air pattern directed at the fuel spray.
Descriptors : (*INJECTORS, *PATENTS), (*TURBOJET ENGINES, *COMBUSTION CHAMBERS), JET ENGINE INLETS, DUCTS, AIR POLLUTION, FUEL SPRAYS, COMBUSTION
Subject Categories : Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE