Dudley O. Nash

Person

Cincinnati, OH, US

People

Patents Grantslast 30 patents

Information Patent Grant
Low thermal stress impingement cooling apparatus
- Patent number 5,557,932
- Issue date Sep 24, 1996
- The United States of America as represented by the Secretary of the Air Force
- Dudley O. Nash
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Multi-axis vectorable exhaust nozzle
- Patent number 5,351,888
- Issue date Oct 4, 1994
- General Electric Company
- John B. Taylor
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Overwing thrust reverser
- Patent number 5,197,694
- Issue date Mar 30, 1993
- General Electric Company
- Dudley O. Nash
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Reduced weight nozzle actuation mechanism
- Patent number 5,176,323
- Issue date Jan 5, 1993
- General Electric Company
- Dudley O. Nash
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Gas turbine engine actuation system
- Patent number 5,136,840
- Issue date Aug 11, 1992
- General Electric Company
- Dudley O. Nash
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Exhaust nozzle hinge
- Patent number 5,101,624
- Issue date Apr 7, 1992
- General Electric Company
- Dudley O. Nash
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Integral transition and convergent section exhaust nozzle
- Patent number 5,016,818
- Issue date May 21, 1991
- General Electric Company
- Dudley O. Nash
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Exhaust nozzle thermal distortion control device
- Patent number 4,934,600
- Issue date Jun 19, 1990
- General Electric Company
- Dudley O. Nash
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Coolant pressure regulating apparatus
- Patent number 4,926,633
- Issue date May 22, 1990
- The United States of America as represented by the Secretary of the Air Force
- Dudley O. Nash
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Heat shield for gas turbine engine frame
- Patent number 4,920,742
- Issue date May 1, 1990
- General Electric Company
- Dudley O. Nash
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Low turbulence flame holder mount
- Patent number 4,901,527
- Issue date Feb 20, 1990
- General Electric Company
- Dudley O. Nash
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Band clamp apparatus
- Patent number 4,840,026
- Issue date Jun 20, 1989
- The United States of America as represented by the Secretary of the Air Force
- Dudley O. Nash
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Flexible duct joint utilizing lip in recess in a flange
- Patent number 4,772,033
- Issue date Sep 20, 1988
- General Electric Company
- Dudley O. Nash
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Dual material exhaust nozzle flap
- Patent number 4,637,550
- Issue date Jan 20, 1987
- The United States of America as represented by the Secretary of the Air Force
- Dudley O. Nash
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
High excursion seal with flexible membrane to prevent gas leakage t...
- Patent number 4,575,099
- Issue date Mar 11, 1986
- General Electric Company
- Dudley O. Nash
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Length adjustable strut link with low aerodynamic drag
- Patent number 4,571,936
- Issue date Feb 25, 1986
- The United States of America as represented by the Secretary of the Air Force
- Dudley O. Nash
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Actuation system for use on a gas turbine engine
- Patent number 4,409,788
- Issue date Oct 18, 1983
- General Electric Company
- Dudley O. Nash
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Exhaust nozzle
- Patent number 4,361,281
- Issue date Nov 30, 1982
- General Electric Company
- Dudley O. Nash
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Low profile fuel injection system
- Patent number 4,312,185
- Issue date Jan 26, 1982
- General Electric Company
- Dudley O. Nash
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Apparatus and method for controlling fan duct flow in a gas turbine...
- Patent number 4,285,194
- Issue date Aug 25, 1981
- General Electric Company
- Dudley O. Nash
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Hydraulic actuation ring
- Patent number 4,181,260
- Issue date Jan 1, 1980
- General Electric Company
- Dudley O. Nash
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Thrust reverser for an asymmetric aircraft exhaust nozzle
- Patent number 4,175,385
- Issue date Nov 27, 1979
- General Electric Company
- Dudley O. Nash
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Sound-suppressing structure with thermal relief
- Patent number 4,106,587
- Issue date Aug 15, 1978
- The United States of America as represented by the administrator of the Natio...
- Dudley O. Nash
- G10 - MUSICAL INSTRUMENTS ACOUSTICS
Information Patent Grant
Gas turbine engine nozzle apparatus including a nozzle flap slot seal
- Patent number 4,073,441
- Issue date Feb 14, 1978
- General Electric Company
- Dudley O. Nash
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Cooling of fastener means for a removable flameholder
- Patent number 4,064,691
- Issue date Dec 27, 1977
- General Electric Company
- Dudley O. Nash
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Flight maneuverable nozzle for gas turbine engines
- Patent number 4,000,610
- Issue date Jan 4, 1977
- General Electric Company
- Dudley O. Nash
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Cooling system for a thrust vectoring gas turbine engine exhaust sy...
- Patent number 4,000,612
- Issue date Jan 4, 1977
- General Electric Company
- Thomas G. Wakeman
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Thrust vectorable exhaust nozzle
- Patent number 4,000,854
- Issue date Jan 4, 1977
- General Electric Company
- Mieczyslaw Konarski
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Actuating means for a thrust vectoring gas turbine engine exhaust n...
- Patent number 3,979,067
- Issue date Sep 7, 1976
- General Electric Company
- Dudley O. Nash
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Gas turbine engine exhaust nozzle diverter valve
- Patent number 3,943,707
- Issue date Mar 16, 1976
- General Electric Company
- Dudley O. Nash
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

Dudley O. Nash

Person

Patents Grantslast 30 patents

Low thermal stress impingement cooling apparatus

Multi-axis vectorable exhaust nozzle

Overwing thrust reverser

Reduced weight nozzle actuation mechanism

Gas turbine engine actuation system

Exhaust nozzle hinge

Integral transition and convergent section exhaust nozzle

Exhaust nozzle thermal distortion control device

Coolant pressure regulating apparatus

Heat shield for gas turbine engine frame

Low turbulence flame holder mount

Band clamp apparatus

Flexible duct joint utilizing lip in recess in a flange

Dual material exhaust nozzle flap

High excursion seal with flexible membrane to prevent gas leakage t...

Length adjustable strut link with low aerodynamic drag

Actuation system for use on a gas turbine engine

Exhaust nozzle

Low profile fuel injection system

Apparatus and method for controlling fan duct flow in a gas turbine...

Hydraulic actuation ring

Thrust reverser for an asymmetric aircraft exhaust nozzle

Sound-suppressing structure with thermal relief

Gas turbine engine nozzle apparatus including a nozzle flap slot seal

Cooling of fastener means for a removable flameholder

Flight maneuverable nozzle for gas turbine engines

Cooling system for a thrust vectoring gas turbine engine exhaust sy...

Thrust vectorable exhaust nozzle

Actuating means for a thrust vectoring gas turbine engine exhaust n...

Gas turbine engine exhaust nozzle diverter valve