Inventor · disambiguated record
Dudley O. Nash
Also filed as: NASH DUDLEY O
30 granted patents·1,306 citations·filing 1974–1993
98Inventor score
Top patents by PatentIndex Score
30 records- 0198US4575099AHigh excursion seal with flexible membrane to prevent gas leakage through hingeGEN ELECTRIC·Filed 1984·Granted Mar 11, 1986·105 cites·7 claims
- 0296US4920742AHeat shield for gas turbine engine frameGEN ELECTRIC·Filed 1988·Granted May 1, 1990·137 cites·31 claims
- 0395US4409788AActuation system for use on a gas turbine engineGEN ELECTRIC·Filed 1981·Granted Oct 18, 1983·96 cites·11 claims
- 0495US4285194AApparatus and method for controlling fan duct flow in a gas turbine engineGEN ELECTRIC·Filed 1979·Granted Aug 25, 1981·71 cites·3 claims
- 0595US4106587ASound-suppressing structure with thermal reliefNASA·Filed 1976·Granted Aug 15, 1978·110 cites·12 claims
- 0690US5136840AGas turbine engine actuation systemGEN ELECTRIC·Filed 1982·Granted Aug 11, 1992·50 cites·12 claims
- 0788US4571936ALength adjustable strut link with low aerodynamic dragUS AIR FORCE·Filed 1985·Granted Feb 25, 1986·65 cites·13 claims
- 0888US4175385AThrust reverser for an asymmetric aircraft exhaust nozzleGEN ELECTRIC·Filed 1977·Granted Nov 27, 1979·43 cites·10 claims
- 0987US4637550ADual material exhaust nozzle flapUS AIR FORCE·Filed 1985·Granted Jan 20, 1987·44 cites·7 claims
- 1085US4000854AThrust vectorable exhaust nozzleGEN ELECTRIC·Filed 1975·Granted Jan 4, 1977·56 cites·22 claims
- 1184US5016818AIntegral transition and convergent section exhaust nozzleGEN ELECTRIC·Filed 1989·Granted May 21, 1991·47 cites·18 claims
- 1282US4901527ALow turbulence flame holder mountGEN ELECTRIC·Filed 1988·Granted Feb 20, 1990·40 cites·41 claims
- 1381US4772033AFlexible duct joint utilizing lip in recess in a flangeGEN ELECTRIC·Filed 1983·Granted Sep 20, 1988·31 cites·3 claims
- 1480US5351888AMulti-axis vectorable exhaust nozzleGEN ELECTRIC·Filed 1993·Granted Oct 4, 1994·56 cites·16 claims
- 1580US4361281AExhaust nozzleGEN ELECTRIC·Filed 1980·Granted Nov 30, 1982·35 cites·8 claims
- 1679US4000612ACooling system for a thrust vectoring gas turbine engine exhaust systemGEN ELECTRIC·Filed 1975·Granted Jan 4, 1977·28 cites·16 claims
- 1778US5101624AExhaust nozzle hingeGEN ELECTRIC·Filed 1991·Granted Apr 7, 1992·38 cites·27 claims
- 1877US4000610AFlight maneuverable nozzle for gas turbine enginesGEN ELECTRIC·Filed 1975·Granted Jan 4, 1977·31 cites·13 claims
- 1976US4064691ACooling of fastener means for a removable flameholderGEN ELECTRIC·Filed 1975·Granted Dec 27, 1977·25 cites·7 claims
- 2075US3979067AActuating means for a thrust vectoring gas turbine engine exhaust nozzleGEN ELECTRIC·Filed 1975·Granted Sep 7, 1976·24 cites·7 claims
- 2172US4926633ACoolant pressure regulating apparatusUS AIR FORCE·Filed 1989·Granted May 22, 1990·27 cites·8 claims
- 2269US4312185ALow profile fuel injection systemGEN ELECTRIC·Filed 1980·Granted Jan 26, 1982·25 cites·18 claims
- 2368US4840026ABand clamp apparatusUS AIR FORCE·Filed 1988·Granted Jun 20, 1989·29 cites·6 claims
- 2462US4181260AHydraulic actuation ringGEN ELECTRIC·Filed 1977·Granted Jan 1, 1980·16 cites·29 claims
- 2560US3943707AGas turbine engine exhaust nozzle diverter valveGEN ELECTRIC·Filed 1974·Granted Mar 16, 1976·14 cites·14 claims
- 2658US5557932ALow thermal stress impingement cooling apparatusUS ARMY·Filed 1986·Granted Sep 24, 1996·17 cites·23 claims
- 2757US5176323AReduced weight nozzle actuation mechanismGEN ELECTRIC·Filed 1991·Granted Jan 5, 1993·21 cites·17 claims
- 2853US4073441AGas turbine engine nozzle apparatus including a nozzle flap slot sealGEN ELECTRIC·Filed 1976·Granted Feb 14, 1978·12 cites·10 claims
- 2943US4934600AExhaust nozzle thermal distortion control deviceGEN ELECTRIC·Filed 1988·Granted Jun 19, 1990·10 cites·13 claims
- 3028US5197694AOverwing thrust reverserGEN ELECTRIC·Filed 1990·Granted Mar 30, 1993·3 cites·25 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →