Compressor bleed manifold for a gas turbine engine

Details Compressor bleed manifold for a gas turbine engine Compressor bleed manifold for a gas turbine engine

1992-06-09

1993-04-20

Bertsch, Richard A.

Power plants

Combustion products used as motive fluid

60 39091, F02C 618

Patent

active

052031624

ABSTRACT:
The compressor customer bleed includes annular spaced walls defining the bleed manifold and staggered openings bleeding compressor air externally of the gas turbine engine avoiding a clear path for a hot particle to the most outer wall and including a thickened wall serving as a heat sink to dissipate the heat of the particle.

REFERENCES:
patent: 2986231 (1961-05-01), Hellstrom
patent: 3108767 (1963-10-01), Eltis et al.
patent: 4155681 (1979-05-01), Linko et al.
patent: 4870826 (1989-10-01), Daguet et al.
patent: 5117629 (1992-06-01), Shaw

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