Auxiliary air system for gas turbine engine

Details Auxiliary air system for gas turbine engine Auxiliary air system for gas turbine engine

1980-02-25

1982-09-28

Hart, Douglas

Power plants

Reaction motor

Interrelated reaction motors

60 3907, 60 3932, 60 3983, 60266, 60726, F02K 304, F02C 606, F02C 720

Patent

active

043511503

ABSTRACT:
An auxiliary air system contained within the nacelle of a gas turbine engine having the functions of cooling engine components and measuring air inlet temperature. The system comprises an air ducting pipe, temperature sensors extending into the pipe, a structure to be cooled, such as an electronics module, preferably with a heat transfer chamber, an air flow inducer, and, if desired, means for directing air onto other engine components.

REFERENCES:
patent: 2625009 (1953-01-01), Leggett
patent: 2652216 (1953-09-01), Hoffman
patent: 2717489 (1955-09-01), Hasbrouck
patent: 2970437 (1961-02-01), Anderson
patent: 3833837 (1974-09-01), West
patent: 4182119 (1980-01-01), Hurley

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