Joseph G. Irwin III

Person

Landenberg, PA, US

People

Patents Grantslast 30 patents

Information Patent Grant
Variable operator interface for backdriving control input devices
- Patent number 11,059,568
- Issue date Jul 13, 2021
- The Boeing Company
- Bryan C. Chu
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Propulsor trim prediction for aircraft
- Patent number 11,016,506
- Issue date May 25, 2021
- The Boeing Company
- Joseph G. Irwin
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Pitch and thrust control for tilt-rotor aircraft
- Patent number 10,935,985
- Issue date Mar 2, 2021
- The Boeing Company
- Joseph G. Irwin
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Variable rate damping based control system for backdriven control i...
- Patent number 10,908,560
- Issue date Feb 2, 2021
- The Boeing Company
- Joseph G. Irwin
- G05 - CONTROLLING REGULATING
Information Patent Grant
Pitch and thrust control for compound aircraft
- Patent number 10,877,487
- Issue date Dec 29, 2020
- The Boeing Company
- Joseph G. Irwin
- G05 - CONTROLLING REGULATING
Information Patent Grant
Pitch trim prediction for aircraft
- Patent number 10,747,235
- Issue date Aug 18, 2020
- The Boeing Company
- Joseph G. Irwin
- G05 - CONTROLLING REGULATING
Information Patent Grant
Point-and-shoot automatic landing system and method
- Patent number 9,891,632
- Issue date Feb 13, 2018
- The Boeing Company
- Joseph G. Irwin
- G05 - CONTROLLING REGULATING
Information Patent Grant
Active-inceptor tactile-cueing hands-off rate-limit
- Patent number 9,156,546
- Issue date Oct 13, 2015
- The Boeing Company
- Joseph G. Irwin
- B64 - AIRCRAFT AVIATION COSMONAUTICS

Patents Applicationslast 30 patents

Information Patent Application
VARIABLE OPERATOR INTERFACE FOR BACKDRIVING CONTROL INPUT DEVICES
- Publication number 20200290728
- Publication date Sep 17, 2020
- The Boeing Company
- Bryan C. Chu
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
VARIABLE RATE DAMPING BASED CONTROL SYSTEM FOR BACKDRIVEN CONTROL I...
- Publication number 20200293004
- Publication date Sep 17, 2020
- The Boeing Company
- Joseph G. Irwin
- G05 - CONTROLLING REGULATING
Information Patent Application
PROPULSOR TRIM PREDICTION FOR AIRCRAFT
- Publication number 20190332126
- Publication date Oct 31, 2019
- The Boeing Company
- Joseph G. Irwin
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
PITCH TRIM PREDICTION FOR AIRCRAFT
- Publication number 20190329879
- Publication date Oct 31, 2019
- The Boeing Company
- Joseph G. Irwin
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
PITCH AND THRUST CONTROL FOR COMPOUND AIRCRAFT
- Publication number 20190332124
- Publication date Oct 31, 2019
- The Boeing Company
- Joseph G. Irwin
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
PITCH AND THRUST CONTROL FOR TILT-ROTOR AIRCRAFT
- Publication number 20190332125
- Publication date Oct 31, 2019
- The Boeing Company
- Joseph G. Irwin
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
POINT-AND-SHOOT AUTOMATIC LANDING SYSTEM AND METHOD
- Publication number 20180046202
- Publication date Feb 15, 2018
- The Boeing Company
- JOSEPH G. IRWIN
- B64 - AIRCRAFT AVIATION COSMONAUTICS

Joseph G. Irwin III

Person

Patents Grantslast 30 patents

Variable operator interface for backdriving control input devices

Propulsor trim prediction for aircraft

Pitch and thrust control for tilt-rotor aircraft

Variable rate damping based control system for backdriven control i...

Pitch and thrust control for compound aircraft

Pitch trim prediction for aircraft

Point-and-shoot automatic landing system and method

Active-inceptor tactile-cueing hands-off rate-limit

Patents Applicationslast 30 patents

VARIABLE OPERATOR INTERFACE FOR BACKDRIVING CONTROL INPUT DEVICES

VARIABLE RATE DAMPING BASED CONTROL SYSTEM FOR BACKDRIVEN CONTROL I...

PROPULSOR TRIM PREDICTION FOR AIRCRAFT

PITCH TRIM PREDICTION FOR AIRCRAFT

PITCH AND THRUST CONTROL FOR COMPOUND AIRCRAFT

PITCH AND THRUST CONTROL FOR TILT-ROTOR AIRCRAFT

POINT-AND-SHOOT AUTOMATIC LANDING SYSTEM AND METHOD