Hollow blading with means to supply fluid thereinto for turbines or compressors
United States Patent 2847185
US Patent References:
Airplane anti-icing system
- - 2447095

Airfoil conditioning means
- - 2514105

Antenna system
- - 2533078

Deicing system for aircraft
- - 2556736

Air-cooled turbine blade
- - 2568726


Inventors:
Alexander, Petrie James
William, Robey Charles
Publication Date:
08/12/1958
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Assignee:
Rolls, Royce
Primary Class:
415/115
Other Classes:
415/116
International Classes:
F01D5/18; F01D9/04
US Patent References:
2647368Method and apparatus for internally cooling gas turbine blades with air, fuel, and water
2648520Air-cooled turbine blade
2779565Air cooling of turbine blades
Foreign References:
CA491903A
GB602530A
GB666536A
FR897709A
FR1007303A