United States Patent 3023980
Inventors:
Martin, Cecil G.
Cummings, Robert L.
Publication Date:
03/06/1962
Assignee:
THOMPSON RAMO WOOLDRIDGE INC
International Classes:
B64C39/02; F02C3/08; B64C39/00; F02C3/00
US Patent References:
| 2596378 | Helicopter blade pitch control mechanism | | | |
| 2630676 | Axial flow jet motor with rotating combustion products generator and turbine | | | |
| 2640549 | Jet-driven sustaining propeller for aircraft | | | |
| 2709889 | Gas turbine using revolving ram jet burners | | | |
| 2801058 | Saucer-shaped aircraft | | | |
| 2912188 | Jet propelled aircraft with tiltable combustion chambers | | | |
| 2920841 | Helicopter with body attaching means | | | |