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:

1976-08-24

Pagination or Media Count:

5.0

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