Turbine nozzle and rotor cooling systems

Power plants – Combustion products used as motive fluid – Multiple fluid-operated motors

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Details

415115, F02C 310, E01D 2514

Patent

active

041731204

ABSTRACT:
A gas turbine engine having a turbine with internally cooled, stationary nozzles, a rotor with internally cooled blades, and systems for supplying air to the nozzles and rotor and for cooling the nozzle case.

REFERENCES:
patent: 3034298 (1962-05-01), White
patent: 3220697 (1965-11-01), Smuland et al.
patent: 3362681 (1968-01-01), Smuland
patent: 3427000 (1969-02-01), Scalzo
patent: 3558237 (1971-01-01), Wall
patent: 3575528 (1971-04-01), Beam et al.
patent: 3989410 (1976-11-01), Ferrari
patent: 4063851 (1977-12-01), Weldon

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