Compressor bore cooling manifold

Rotary kinetic fluid motors or pumps – With passage in blade – vane – shaft or rotary distributor...

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415116, F03B 1102

Patent

active

052717119

ABSTRACT:
To control disc temperature, provide blade tip clearance control, and purge the rotor bore of a high pressure compressor in a gas turbine engine, an axially elongated manifold is disposed coaxially in the rotor bore to distribute cooling air bleed from the compressor inlet airstream to selected cavities between successive rotor discs in amounts tailored to the particular cooling needs of the neighboring discs.

REFERENCES:
patent: 3647313 (1972-03-01), Koff
patent: 4184797 (1980-01-01), Anderson et al.
patent: 4190398 (1980-02-01), Corsmeier et al.
patent: 4719747 (1988-01-01), Willkop et al.
patent: 4880354 (1989-11-01), Teranishi et al.
patent: 4893984 (1990-01-01), Davison et al.
patent: 5054996 (1991-10-01), Carreno

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