Device for bleeding off and cooling hot air in an aircraft engin

Power plants – Reaction motor – Interrelated reaction motors

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60 3907, F02C 608, F02K 304

Patent

active

057299692

ABSTRACT:
The present invention relates to a device for bleeding off and cooling hot air in an aircraft engine, including:

REFERENCES:
patent: 3475906 (1969-11-01), Madelung
patent: 4645415 (1987-02-01), Hovan et al.
patent: 5123242 (1992-06-01), Miller
patent: 5203163 (1993-04-01), Parsons
patent: 5319927 (1994-06-01), Maguire
patent: 5363641 (1994-11-01), Dixon et al.
patent: 5511374 (1996-04-01), Glickstein et al.

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