Title:
BLADES AND BLADE ASSEMBLIES FOR TURBINE ENGINES,COMPRESSORS AND THE LIKE
United States Patent 3515499
US Patent References:
Turbine blade construction with provision for cooling
- - 2701120
Bladed rotors for axial flow turbines and similarly bladed fluid flow machines
- - 2786646
Air-cooled, strut supported turbine blade
- - 2825530
Laminated internal finned air-cooled strut-supported turbine blade
- - 2828106
Blade structure
- - 2853271
Turbine blade construction with provision for cooling
- - 2701120
Bladed rotors for axial flow turbines and similarly bladed fluid flow machines
- - 2786646
Air-cooled, strut supported turbine blade
- - 2825530
Laminated internal finned air-cooled strut-supported turbine blade
- - 2828106
Blade structure
- - 2853271
Inventors:
Beer, Rudolf E.
Klessig, Clarence E.
Botz, Richard J. LA.
Klessig, Clarence E.
Botz, Richard J. LA.
Publication Date:
06/02/1970
View Patent Images:
Export Citation:
Assignee:
AEROJET GENERAL CO
Primary Class:
Other Classes:
416/97A, 416/229R, 416/229A, 416/193A
International Classes:
F01D5/18; F01D5/08; F01D5/18
US Patent References:
| 3301526 | Stacked-wafer turbine vane or blade |
Foreign References:
| DE1064757B |