Coolable nozzle guide vane

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

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Details

415116, 416 97A, F01D 2512, F02C 718

Patent

active

040407675

ABSTRACT:
A coolable nozzle guide vane in the turbine section of a gas turbine engine is disclosed. The vane has a platform section and an airfoil section which are adapted to receive and distribute cooling air about the walls of the sections which are in contact with the hot working medium gases flowing through the turbine during operation of the engine. Impingement cooling and transpiration cooling techniques are combined to maximize the cooling effectiveness of the air supplied.

REFERENCES:
patent: 3240468 (1966-03-01), Watts
patent: 3433015 (1969-03-01), Sneeden
patent: 3610769 (1971-10-01), Schwedland
patent: 3628880 (1971-12-01), Smuland
patent: 3644059 (1972-02-01), Bryan
patent: 3706508 (1972-12-01), Moskowitz
patent: 3726604 (1973-04-01), Helms

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