Cantor Colburn LLP
Cooling system for gas turbine engines
A cooling system for gas turbine engines includes a turbine rotor compartment defining a cooling air plenum. A plurality of turbine discs are rotatably housed within the rotor compartment. A cooling air inlet is in fluid communication with the plenum. Each turbine disc includes a cooling outlet in fluid communication with the plenum for cooling the rotor compartment.
UNITED TECHNOLOGIES CORPORATION
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F02C F01D
inventional inventional
Brian D James D Gabriel L
Merry Hill Suciu