Diffuser clean air bleed assembly

Power plants – Combustion products used as motive fluid

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60 3907, 60751, F02C 618, F02G 300

Patent

active

052110036

ABSTRACT:
A method and apparatus are provided for bleeding compressed air downstream from a diffuser outlet and upstream from a fuel injector in a gas turbine engine. A bleed manifold aft wall is disposed between the diffuser outlet and the fuel injectors and is configured for blocking recirculation flow of air discharged from the diffuser outlet to create a sheltered zone disposed in direct flow communication with the diffuser outlet. Bleed holes are disposed in the sheltered zone for channeling a portion of the diffuser discharge air directly therefrom as bleed air for use in an aircraft environmental system.

REFERENCES:
patent: 3394543 (1968-06-01), Slattery
patent: 3777489 (1973-12-01), Johnson et al.
patent: 3898799 (1975-08-01), Pollert et al.
patent: 3905191 (1975-09-01), Matto
patent: 4459802 (1984-07-01), Mowill
patent: 4463552 (1984-08-01), Monhardt et al.
patent: 4554789 (1985-11-01), Napoli et al.
patent: 4657482 (1987-04-01), Neal
patent: 4989403 (1991-02-01), Rodgers
patent: 5077967 (1992-01-01), Widener et al.
General Electric Company (GE), Four GE diffuser-Combustors Jan. 1, 1991.

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