Air Mixing Ejector and Jet Pump System.

Raudenbush, Allen K.

Air Mixing Ejector and Jet Pump System.

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Abstract:

The patent application describes an ejector jet arrangement for mixing air flow from two different compressor stages of a jet aircraft engine where the highest stage air is introduced into the central mixing section through a continuous jet opening surrounding the section to mix with and pump the bleed air from the other, or lower stage, and to be conducted to the wing for boundary layer control use.

Author(s):

Raudenbush, Allen K.

Author Organization(s):

DEPARTMENT OF THE AIR FORCE WASHINGTON D C

Descriptive Note:

Patent Application,

Pagination:

0011

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:

Approved For Public Release

Distribution Statement:

This Government-owned Invention Available For U.s. Licensing And, Possibly, For Foreign Licensing. Copy Of Application Available Ntis.

RECORD

Collection: TR

Identifying Numbers

Report Number(s):

PAT-APPL-652 955

Subject Terms

Communities of Interest:

Air Platforms

Descriptor(s):

*Jet engines, *Jet aircraft, *Air flow, *Boundary layer control, Bleed systems, Mixing, Low velocity, Patents, Ejectors, Jet mixing flow, Compressors

Field(s)/Group(s):

Fluid Mechanics, Jet and Gas Turbine Engines

Keyword(s):

Jet engine stages, *Patent applications, PAT CL 239 265 17

Report Date:

1976 Jan 28