loadpatents
Patent applications and USPTO patent grants for Thayer; Edward B..The latest application filed is for "vectoring nozzle using injected high pressure air".
Patent | Date |
---|---|
Vectoring nozzle using injected high pressure air Grant 5,706,650 - Thayer January 13, 1 | 1998-01-13 |
Rocket nozzle for a rocket engine Grant 5,683,033 - Thayer November 4, 1 | 1997-11-04 |
Gas turbine vectoring exhaust nozzle Grant 5,335,489 - Thayer August 9, 1 | 1994-08-09 |
Aircraft reverser port door Grant 5,209,432 - Roberge , et al. May 11, 1 | 1993-05-11 |
In-flight reverser Grant 5,161,752 - Cockerham , et al. November 10, 1 | 1992-11-10 |
Flow diverting nozzle for a gas turbine engine Grant 5,098,022 - Thayer March 24, 1 | 1992-03-24 |
Gas turbine spherical exhaust nozzle Grant 4,993,641 - Kehret , et al. February 19, 1 | 1991-02-19 |
Yaw and pitch convergent-divergent thrust vectoring nozzle Grant 4,836,451 - Herrick , et al. June 6, 1 | 1989-06-06 |
Divergent flap actuation system for a two-dimensional exhaust nozzle Grant 4,819,876 - Thayer April 11, 1 | 1989-04-11 |
Control vent for diverting exhaust nozzle Grant 4,805,401 - Thayer , et al. February 21, 1 | 1989-02-21 |
Area controlled, thrust vectoring vane cascade with nutating control vane Grant 4,798,328 - Thayer , et al. January 17, 1 | 1989-01-17 |
Two dimensional gas turbine engine exhaust nozzle Grant 4,753,392 - Thayer , et al. June 28, 1 | 1988-06-28 |
2-D propulsive lift nozzle Grant 4,714,197 - Thayer , et al. December 22, 1 | 1987-12-22 |
Thrust reverser/exhaust nozzle assembly for a gas turbine engine Grant 4,591,097 - Thayer May 27, 1 | 1986-05-27 |
Flap-type nozzle with built-in reverser Grant 4,382,551 - Thayer May 10, 1 | 1983-05-10 |
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