Cooling scheme for combustor vane interface

Details Cooling scheme for combustor vane interface Cooling scheme for combustor vane interface

1984-10-11

1988-04-26

Croyle, Carlton R.

Power plants

Combustion products used as motive fluid

Combustion products generator

60 3983, 415175, F02C 100

Patent

active

047396210

ABSTRACT:
The turbine vanes of a gas turbine engine immediately downstream of the combustor are maintained at a cool temperature by judiciously directing cooling air at the stagnation point ahead of the vane's leading edge at the juncture of the vane's airfoil section and platform.

REFERENCES:
patent: 3186168 (1965-06-01), Ormerod et al.
patent: 3307354 (1967-03-01), Macaulay et al.
patent: 3527053 (1970-09-01), Horn
patent: 3565545 (1971-02-01), Bobo et al.
patent: 3670497 (1972-06-01), Sheldon
patent: 4025226 (1977-05-01), Hovan

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