Inventor
NASH DUDLEY O
US30 patents
⚠️ This page may combine multiple inventors who share the name “NASH DUDLEY O”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
GEN ELECTRIC
24 patentsUS5351888AOct 4, 1994
Multi-axis vectorable exhaust nozzle
GEN ELECTRIC56 citations96
US4920742AMay 1, 1990
Heat shield for gas turbine engine frame
GEN ELECTRIC137 citations96
US4575099AMar 11, 1986
High excursion seal with flexible membrane to prevent gas leakage through hinge
GEN ELECTRIC105 citations96
US4285194AAug 25, 1981
Apparatus and method for controlling fan duct flow in a gas turbine engine
GEN ELECTRIC71 citations96
US4409788AOct 18, 1983
Actuation system for use on a gas turbine engine
GEN ELECTRIC96 citations94
US4000854AJan 4, 1977
Thrust vectorable exhaust nozzle
GEN ELECTRIC56 citations93
US5176323AJan 5, 1993
Reduced weight nozzle actuation mechanism
GEN ELECTRIC21 citations92
US5136840AAug 11, 1992
Gas turbine engine actuation system
GEN ELECTRIC50 citations92
US5101624AApr 7, 1992
Exhaust nozzle hinge
GEN ELECTRIC38 citations92
US4772033ASep 20, 1988
Flexible duct joint utilizing lip in recess in a flange
GEN ELECTRIC31 citations92
US4361281ANov 30, 1982
Exhaust nozzle
GEN ELECTRIC35 citations92
US4175385ANov 27, 1979
Thrust reverser for an asymmetric aircraft exhaust nozzle
GEN ELECTRIC43 citations92
US5016818AMay 21, 1991
Integral transition and convergent section exhaust nozzle
GEN ELECTRIC47 citations90
US4901527AFeb 20, 1990
Low turbulence flame holder mount
GEN ELECTRIC40 citations90
US4064691ADec 27, 1977
Cooling of fastener means for a removable flameholder
GEN ELECTRIC25 citations82
US4000612AJan 4, 1977
Cooling system for a thrust vectoring gas turbine engine exhaust system
GEN ELECTRIC28 citations82
US3979067ASep 7, 1976
Actuating means for a thrust vectoring gas turbine engine exhaust nozzle
GEN ELECTRIC24 citations82
US4312185AJan 26, 1982
Low profile fuel injection system
GEN ELECTRIC25 citations79
US4000610AJan 4, 1977
Flight maneuverable nozzle for gas turbine engines
GEN ELECTRIC31 citations78
US4181260AJan 1, 1980
Hydraulic actuation ring
GEN ELECTRIC16 citations74
US3943707AMar 16, 1976
Gas turbine engine exhaust nozzle diverter valve
GEN ELECTRIC14 citations74
US4073441AFeb 14, 1978
Gas turbine engine nozzle apparatus including a nozzle flap slot seal
GEN ELECTRIC12 citations72
US4934600AJun 19, 1990
Exhaust nozzle thermal distortion control device
GEN ELECTRIC10 citations69
US5197694AMar 30, 1993
Overwing thrust reverser
GEN ELECTRIC3 citations60
US AIR FORCE
4 patentsUS4571936AFeb 25, 1986
Length adjustable strut link with low aerodynamic drag
US AIR FORCE65 citations94
US4637550AJan 20, 1987
Dual material exhaust nozzle flap
US AIR FORCE44 citations92
US4926633AMay 22, 1990
Coolant pressure regulating apparatus
US AIR FORCE27 citations91
US4840026AJun 20, 1989
Band clamp apparatus
US AIR FORCE29 citations88