Stuart C. Wright

Person

Woodbridge, CT, US

People

Patents Grantslast 30 patents

Information Patent Grant
Method and system for detecting forces on aircraft
- Patent number 8,862,377
- Issue date Oct 14, 2014
- Sikorsky Aircraft Corporation
- Karim Khial
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Helicopter turn coordination and heading hold mode control
- Patent number 5,299,759
- Issue date Apr 5, 1994
- United Technologies Corporation
- Porter D. Sherman
- G05 - CONTROLLING REGULATING
Information Patent Grant
Adaptive control system input limiting
- Patent number 5,224,664
- Issue date Jul 6, 1993
- United Technologies Corporation
- Don L. Adams
- G05 - CONTROLLING REGULATING
Information Patent Grant
Automatic turn coordination trim control for rotary wing aircraft
- Patent number 5,222,691
- Issue date Jun 29, 1993
- United Technologies Corporation
- Phillip J. Gold
- G05 - CONTROLLING REGULATING
Information Patent Grant
Maneuver feel system for a rotary wing aircraft
- Patent number 5,213,282
- Issue date May 25, 1993
- United Technologies Corporation
- Phillip J. Gold
- G05 - CONTROLLING REGULATING
Information Patent Grant
High speed yaw control system for rotary wing aircraft
- Patent number 5,178,307
- Issue date Jan 12, 1993
- United Technologies Corporation
- Stuart C. Wright
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Attitude synchronization for model following control systems
- Patent number 5,169,090
- Issue date Dec 8, 1992
- United Technologies Corporation
- Stuart C. Wright
- G05 - CONTROLLING REGULATING
Information Patent Grant
Model following control system
- Patent number 5,141,177
- Issue date Aug 25, 1992
- United Technologies Corporation
- Stuart C. Wright
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Method of and arrangement for controlling and h-bridge electric motor
- Patent number 4,816,726
- Issue date Mar 28, 1989
- United Technologies Corporation
- Ari M. Novis
- H02 - GENERATION CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
Information Patent Grant
Collective control system for a helicopter
- Patent number 4,696,445
- Issue date Sep 29, 1987
- United Technologies Corporation
- Stuart C. Wright
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Heading reference trim system
- Patent number 4,626,998
- Issue date Dec 2, 1986
- United Technologies Corporation
- Don L. Adams
- G05 - CONTROLLING REGULATING
Information Patent Grant
Aircraft trim actuator shutdown monitor system and method
- Patent number 4,599,698
- Issue date Jul 8, 1986
- United Technologies Corporation
- William C. Fischer
- G05 - CONTROLLING REGULATING
Information Patent Grant
Dual-actuator monitor
- Patent number 4,594,714
- Issue date Jun 10, 1986
- United Technologies Corporation
- William C. Fischer
- G05 - CONTROLLING REGULATING
Information Patent Grant
Outer-loop monitor for aircraft automatic flight control system
- Patent number 4,592,055
- Issue date May 27, 1986
- United Technologies Corporation
- William C. Fischer
- G05 - CONTROLLING REGULATING
Information Patent Grant
Incorporation of pitch bias actuator function into an existing AFCS
- Patent number 4,580,223
- Issue date Apr 1, 1986
- United Technologies Corporation
- Stuart C. Wright
- G05 - CONTROLLING REGULATING
Information Patent Grant
Flight director go-around mode
- Patent number 4,577,275
- Issue date Mar 18, 1986
- United Technologies Corporation
- Don L. Adams
- G05 - CONTROLLING REGULATING
Information Patent Grant
Shutdown monitor for a helicopter pitch bias actuator
- Patent number 4,528,628
- Issue date Jul 9, 1985
- United Technologies Corporation
- William C. Fischer
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Aircraft roll-yaw fault protocols
- Patent number 4,484,283
- Issue date Nov 20, 1984
- United Technologies Corporation
- David J. Verzella
- G05 - CONTROLLING REGULATING
Information Patent Grant
Dual response aircraft reference synchronization
- Patent number 4,477,876
- Issue date Oct 16, 1984
- United Technologies Corporation
- Stuart C. Wright
- G05 - CONTROLLING REGULATING
Information Patent Grant
Dual inner loop fault inhibit of aircraft outer loop
- Patent number 4,417,308
- Issue date Nov 22, 1983
- United Technologies Corporation
- Stuart C. Wright
- G05 - CONTROLLING REGULATING
Information Patent Grant
Aircraft coordinated turn with lagged roll rate
- Patent number 4,392,203
- Issue date Jul 5, 1983
- United Technologies Corporation
- William C. Fischer
- G05 - CONTROLLING REGULATING
Information Patent Grant
Pulsed aircraft actuator
- Patent number 4,387,432
- Issue date Jun 7, 1983
- United Technologies Corporation
- William C. Fischer
- G05 - CONTROLLING REGULATING
Information Patent Grant
Pitch stick force inhibit of aircraft automatic outer loop
- Patent number 4,387,430
- Issue date Jun 7, 1983
- United Technologies Corporation
- David J. Verzella
- G05 - CONTROLLING REGULATING
Information Patent Grant
Roll attitude inhibit of aircraft automatic outer loop
- Patent number 4,387,431
- Issue date Jun 7, 1983
- United Technologies Corporation
- Stuart C. Wright
- G05 - CONTROLLING REGULATING
Information Patent Grant
Automatic outer loop centering of aircraft inner loop
- Patent number 4,385,355
- Issue date May 24, 1983
- United Technologies Corporation
- David J. Verzella
- G05 - CONTROLLING REGULATING
Information Patent Grant
Non-saturating airspeed/attitude controls
- Patent number 4,385,356
- Issue date May 24, 1983
- United Technologies Corporation
- David J. Verzella
- G05 - CONTROLLING REGULATING
Information Patent Grant
Command-inhibited aircraft attitude reference adjustment
- Patent number 4,383,299
- Issue date May 10, 1983
- United Technologies Corporation
- William C. Fischer
- G05 - CONTROLLING REGULATING
Information Patent Grant
Attitude trimmed airspeed/attitude controls
- Patent number 4,371,936
- Issue date Feb 1, 1983
- United Technologies Corporation
- Don L. Adams
- G05 - CONTROLLING REGULATING
Information Patent Grant
Automatic airspeed engage/disengage
- Patent number 4,371,938
- Issue date Feb 1, 1983
- United Technologies Corporation
- Stuart C. Wright
- G05 - CONTROLLING REGULATING
Information Patent Grant
Roll attitude inhibit of aircraft coordinated turn disengagement
- Patent number 4,371,939
- Issue date Feb 1, 1983
- United Technologies Corporation
- Don L. Adams
- G05 - CONTROLLING REGULATING

Patents Applicationslast 30 patents

Information Patent Application
Method and System for Detecting Forces on Aircraft
- Publication number 20120253652
- Publication date Oct 4, 2012
- SIKORSKY AIRCRAFT CORPORATION
- Karim Khial
- B64 - AIRCRAFT AVIATION COSMONAUTICS

Stuart C. Wright

Person

Patents Grantslast 30 patents

Method and system for detecting forces on aircraft

Helicopter turn coordination and heading hold mode control

Adaptive control system input limiting

Automatic turn coordination trim control for rotary wing aircraft

Maneuver feel system for a rotary wing aircraft

High speed yaw control system for rotary wing aircraft

Attitude synchronization for model following control systems

Model following control system

Method of and arrangement for controlling and h-bridge electric motor

Collective control system for a helicopter

Heading reference trim system

Aircraft trim actuator shutdown monitor system and method

Dual-actuator monitor

Outer-loop monitor for aircraft automatic flight control system

Incorporation of pitch bias actuator function into an existing AFCS

Flight director go-around mode

Shutdown monitor for a helicopter pitch bias actuator

Aircraft roll-yaw fault protocols

Dual response aircraft reference synchronization

Dual inner loop fault inhibit of aircraft outer loop

Aircraft coordinated turn with lagged roll rate

Pulsed aircraft actuator

Pitch stick force inhibit of aircraft automatic outer loop

Roll attitude inhibit of aircraft automatic outer loop

Automatic outer loop centering of aircraft inner loop

Non-saturating airspeed/attitude controls

Command-inhibited aircraft attitude reference adjustment

Attitude trimmed airspeed/attitude controls

Automatic airspeed engage/disengage

Roll attitude inhibit of aircraft coordinated turn disengagement

Patents Applicationslast 30 patents

Method and System for Detecting Forces on Aircraft