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