loadpatents
Patent applications and USPTO patent grants for Nash; Dudley O..The latest application filed is for "multi-axis vectorable exhaust nozzle".
Patent | Date |
---|---|
Multi-axis vectorable exhaust nozzle Grant 5,351,888 - Taylor , et al. October 4, 1 | 1994-10-04 |
Gas turbine engine actuation system Grant 5,136,840 - Nash August 11, 1 | 1992-08-11 |
Exhaust nozzle hinge Grant 5,101,624 - Nash , et al. April 7, 1 | 1992-04-07 |
Exhaust nozzle thermal distortion control device Grant 4,934,600 - Nash , et al. June 19, 1 | 1990-06-19 |
Coolant pressure regulating apparatus Grant 4,926,633 - Nash , et al. May 22, 1 | 1990-05-22 |
Heat shield for gas turbine engine frame Grant 4,920,742 - Nash , et al. May 1, 1 | 1990-05-01 |
Low turbulence flame holder mount Grant 4,901,527 - Nash , et al. February 20, 1 | 1990-02-20 |
Band clamp apparatus Grant 4,840,026 - Nash , et al. June 20, 1 | 1989-06-20 |
Flexible duct joint utilizing lip in recess in a flange Grant 4,772,033 - Nash September 20, 1 | 1988-09-20 |
High excursion seal with flexible membrane to prevent gas leakage through hinge Grant 4,575,099 - Nash March 11, 1 | 1986-03-11 |
Length adjustable strut link with low aerodynamic drag Grant 4,571,936 - Nash , et al. February 25, 1 | 1986-02-25 |
Actuation system for use on a gas turbine engine Grant 4,409,788 - Nash , et al. October 18, 1 | 1983-10-18 |
Exhaust nozzle Grant 4,361,281 - Nash November 30, 1 | 1982-11-30 |
Low profile fuel injection system Grant 4,312,185 - Nash , et al. January 26, 1 | 1982-01-26 |
Apparatus and method for controlling fan duct flow in a gas turbine engine Grant 4,285,194 - Nash August 25, 1 | 1981-08-25 |
Sound-suppressing structure with thermal relief Grant 4,106,587 - Nash , et al. August 15, 1 | 1978-08-15 |
Cooling of fastener means for a removable flameholder Grant 4,064,691 - Nash December 27, 1 | 1977-12-27 |
Flight maneuverable nozzle for gas turbine engines Grant 4,000,610 - Nash , et al. January 4, 1 | 1977-01-04 |
Cooling system for a thrust vectoring gas turbine engine exhaust system Grant 4,000,612 - Wakeman , et al. January 4, 1 | 1977-01-04 |
Thrust vectorable exhaust nozzle Grant 4,000,854 - Konarski , et al. January 4, 1 | 1977-01-04 |
Diverter Valve For A Gas Turbine With An Augmenter Grant 3,837,411 - Nash , et al. September 24, 1 | 1974-09-24 |
Air Cooled Augmenter Igniter Assembly Grant 3,800,530 - Nash April 2, 1 | 1974-04-02 |
Augmenter Fuel Injection Mounting System Grant 3,793,838 - Nash February 26, 1 | 1974-02-26 |
Cooled Augmentor Liner Grant 3,712,062 - Nash January 23, 1 | 1973-01-23 |
Swivelable Jet Nozzle Grant 3,687,374 - Nash August 29, 1 | 1972-08-29 |
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