Accession Number : ADD002997
Title : Interstage Bleed Assembly.
Descriptive Note : Patent,
Corporate Author : DEPARTMENT OF THE AIR FORCE WASHINGTON D C
Personal Author(s) : Tarter,David A ; Readnour,Jack L
Report Date : 24 Aug 1976
Pagination or Media Count : 5
Abstract : The patent relates to a two part metering adapter ring, for providing bleed air from the compressor of an aircraft engine, having a plurality of metering air flow passages. The adapter ring is secured to the outer casing stator support member and has a movable seal engaging a member on the inner casing stator support member. A pair of spring members holds the seal in contact with the seal engaging member on the inner casing stator support member.
Descriptors : *Jet engines, *Compressors, *Bleed systems, *Patents, Compressor stators, Seals, Regulators
Subject Categories : Aircraft
Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE