Phillip J. Gold

Person

Shelton, CT, US

People

Patents Grantslast 30 patents

Information Patent Grant
Fly-by-wire flight control system with electronic lead/lag damper a...
- Patent number 8,548,648
- Issue date Oct 1, 2013
- Sikorsky Aircraft Corporation
- Vineet Sahasrabudhe
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Fly by wire static longitudinal stability compensator system
- Patent number 7,433,765
- Issue date Oct 7, 2008
- Sikorsky Aircraft Corporation
- Todd M. Fanciullo
- G05 - CONTROLLING REGULATING
Information Patent Grant
Trim augmentation system for a rotary wing aircraft
- Patent number 6,648,269
- Issue date Nov 18, 2003
- Sikorsky Aircraft Corporation
- Phillip Jeremy Gold
- G05 - CONTROLLING REGULATING
Information Patent Grant
Model-following control system using acceleration feedback
- Patent number 6,189,836
- Issue date Feb 20, 2001
- Sikorsky Aircraft Corporation
- Phillip Jeremy Gold
- G05 - CONTROLLING REGULATING
Information Patent Grant
Integrated fire and flight control system for controlling the angle...
- Patent number 6,145,428
- Issue date Nov 14, 2000
- Sikorsky Aircraft Corporation
- Phillip J. Gold
- G05 - CONTROLLING REGULATING
Information Patent Grant
Integrated fire and flight control system with automatic engine tor...
- Patent number 6,012,676
- Issue date Jan 11, 2000
- Sikorsky Aircraft Corporation
- Phillip J. Gold
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Compensation for rotorcraft pitch axis control saturation
- Patent number 5,971,325
- Issue date Oct 26, 1999
- Sikorsky Aircraft Corporation
- Phillip J. Gold
- G05 - CONTROLLING REGULATING
Information Patent Grant
Inertial velocity command system
- Patent number 5,553,812
- Issue date Sep 10, 1996
- United Technologies Corporation
- Phillip J. Gold
- G05 - CONTROLLING REGULATING
Information Patent Grant
Turn coordination inhibit for rotary wing aircraft control system
- Patent number 5,553,817
- Issue date Sep 10, 1996
- United Technologies Corporation
- Phillip J. Gold
- G05 - CONTROLLING REGULATING
Information Patent Grant
Vertical control system for rotary wing aircraft
- Patent number 5,428,543
- Issue date Jun 27, 1995
- United Technologies Corporation
- Phillip J. Gold
- G05 - CONTROLLING REGULATING
Information Patent Grant
Transient free synchronizer for autopilot systems
- Patent number 5,301,112
- Issue date Apr 5, 1994
- United Technologies Corporation
- Phillip J. Gold
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
High speed turn coordination for rotary wing aircraft
- Patent number 5,238,203
- Issue date Aug 24, 1993
- United Technologies Corporation
- Joseph P. Skonieczny
- 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
Low speed turn coordination for rotary wing aircraft
- Patent number 5,213,283
- Issue date May 25, 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
Low speed model following velocity command system for rotary wing a...
- Patent number 5,195,700
- Issue date Mar 23, 1993
- United Technologies Corporation
- Donald L. Fogler
- G05 - CONTROLLING REGULATING
Information Patent Grant
Hover position hold system for rotary winged aircraft
- Patent number 5,195,039
- Issue date Mar 16, 1993
- United Technologies Corporation
- Phillip J. Gold
- B64 - AIRCRAFT AVIATION COSMONAUTICS
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
Control law system for X-Wing aircraft
- Patent number 4,980,835
- Issue date Dec 25, 1990
- United Technologies Corporation
- Thomas H. Lawrence
- B64 - AIRCRAFT AVIATION COSMONAUTICS

Patents Applicationslast 30 patents

Information Patent Application
FLY-BY-WIRE FLIGHT CONTROL SYSTEM WITH ELECTRONIC LEAD/LAG DAMPER A...
- Publication number 20100023186
- Publication date Jan 28, 2010
- Vineet Sahasrabudhe
- G05 - CONTROLLING REGULATING
Information Patent Application
Fly by wire static longitudinal stability compensator system
- Publication number 20060253230
- Publication date Nov 9, 2006
- Sikorsky Aircraft Corporation
- Todd M. Fanciullo
- G05 - CONTROLLING REGULATING
Information Patent Application
Trim augmentation system for a rotory wing aircraft
- Publication number 20030106958
- Publication date Jun 12, 2003
- Phillip Jeremy Gold
- G05 - CONTROLLING REGULATING

Phillip J. Gold

Person

Patents Grantslast 30 patents

Fly-by-wire flight control system with electronic lead/lag damper a...

Fly by wire static longitudinal stability compensator system

Trim augmentation system for a rotary wing aircraft

Model-following control system using acceleration feedback

Integrated fire and flight control system for controlling the angle...

Integrated fire and flight control system with automatic engine tor...

Compensation for rotorcraft pitch axis control saturation

Inertial velocity command system

Turn coordination inhibit for rotary wing aircraft control system

Vertical control system for rotary wing aircraft

Transient free synchronizer for autopilot systems

High speed turn coordination for rotary wing aircraft

Automatic turn coordination trim control for rotary wing aircraft

Low speed turn coordination for rotary wing aircraft

Maneuver feel system for a rotary wing aircraft

Low speed model following velocity command system for rotary wing a...

Hover position hold system for rotary winged aircraft

High speed yaw control system for rotary wing aircraft

Attitude synchronization for model following control systems

Control law system for X-Wing aircraft

Patents Applicationslast 30 patents

FLY-BY-WIRE FLIGHT CONTROL SYSTEM WITH ELECTRONIC LEAD/LAG DAMPER A...

Fly by wire static longitudinal stability compensator system

Trim augmentation system for a rotory wing aircraft