Donald W. Fowler

Person

Oxford, CT, US

People

Patents Grantslast 30 patents

Information Patent Grant
Harmonic data transfer in rotary wing aircraft
- Patent number 9,203,459
- Issue date Dec 1, 2015
- Sikorsky Aircraft Corporation
- Harshad S. Sane
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Module for integrated approach to an offshore facility
- Patent number 8,442,706
- Issue date May 14, 2013
- Sikorsky Aircraft Corporation
- Ronald S. Doeppner
- G05 - CONTROLLING REGULATING
Information Patent Grant
Flight control system for rotary wing aircraft
- Patent number 8,271,151
- Issue date Sep 18, 2012
- Sikorsky Aircraft Corporation
- Muhammad Emadul Hasan
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Helicopter integrated fire and flight control having a pre-launch a...
- Patent number 5,465,212
- Issue date Nov 7, 1995
- United Technologies Corporation
- Donald W. Fowler
- G05 - CONTROLLING REGULATING
Information Patent Grant
Helicopter integrated fire and flight control having azimuth and pi...
- Patent number 5,431,084
- Issue date Jul 11, 1995
- United Technologies Corporation
- Donald W. Fowler
- G05 - CONTROLLING REGULATING
Information Patent Grant
Helicopter integrated fire and flight control having azimuth and pi...
- Patent number 5,331,881
- Issue date Jul 26, 1994
- United Technologies Corporation
- Donald W. Fowler
- G05 - CONTROLLING REGULATING
Information Patent Grant
Helicopter integrated fire and flight control having constraint lim...
- Patent number 5,310,136
- Issue date May 10, 1994
- United Technologies Corporation
- Donald W. Fowler
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Helicopter integrated fire and flight control having coordinated ar...
- Patent number 5,310,135
- Issue date May 10, 1994
- United Technologies Corporation
- Donald W. Fowler
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Helicopter integrated fire and flight control system having turn co...
- Patent number 5,263,662
- Issue date Nov 23, 1993
- United Technologies Corporation
- Donald W. Fowler
- G05 - CONTROLLING REGULATING
Information Patent Grant
Helicopter force feel actuator automatic static null compensation
- Patent number 4,382,281
- Issue date May 3, 1983
- United Technologies Corporation
- Donald W. Fowler
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Updated lock-positioning of foldable helicopter blades
- Patent number 4,376,979
- Issue date Mar 15, 1983
- United Technologies Corporation
- Donald W. Fowler
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Adaptive aircraft actuator fault detection
- Patent number 4,355,358
- Issue date Oct 19, 1982
- United Technologies Corporation
- Douglas H. Clelford
- G05 - CONTROLLING REGULATING
Information Patent Grant
Force feel actuator with limited proportional/integral error feedback
- Patent number 4,313,165
- Issue date Jan 26, 1982
- United Technologies Corporation
- Douglas H. Clelford
- G05 - CONTROLLING REGULATING
Information Patent Grant
Force feel actuator fault detection with directional threshold
- Patent number 4,294,162
- Issue date Oct 13, 1981
- United Technologies Corporation
- Donald W. Fowler
- G05 - CONTROLLING REGULATING
Information Patent Grant
Aerodynamic surface control feel augmentation system
- Patent number 3,960,348
- Issue date Jun 1, 1976
- United Technologies Corporation
- Donald W. Fowler
- B64 - AIRCRAFT AVIATION COSMONAUTICS

Patents Applicationslast 30 patents

Information Patent Application
Harmonic Data Transfer In Rotary Wing Aircraft
- Publication number 20140314130
- Publication date Oct 23, 2014
- Harshad S. Sane
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
FLIGHT CONTROL SYSTEM FOR ROTARY WING AIRCRAFT
- Publication number 20120072056
- Publication date Mar 22, 2012
- Muhammad Emadul Hasan
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
MODULE FOR INTEGRATED APPROACH TO AN OFFSHORE FACILITY
- Publication number 20100168939
- Publication date Jul 1, 2010
- Ronald S. Doeppner
- G05 - CONTROLLING REGULATING

Donald W. Fowler

Person

Patents Grantslast 30 patents

Harmonic data transfer in rotary wing aircraft

Module for integrated approach to an offshore facility

Flight control system for rotary wing aircraft

Helicopter integrated fire and flight control having a pre-launch a...

Helicopter integrated fire and flight control having azimuth and pi...

Helicopter integrated fire and flight control having azimuth and pi...

Helicopter integrated fire and flight control having constraint lim...

Helicopter integrated fire and flight control having coordinated ar...

Helicopter integrated fire and flight control system having turn co...

Helicopter force feel actuator automatic static null compensation

Updated lock-positioning of foldable helicopter blades

Adaptive aircraft actuator fault detection

Force feel actuator with limited proportional/integral error feedback

Force feel actuator fault detection with directional threshold

Aerodynamic surface control feel augmentation system

Patents Applicationslast 30 patents

Harmonic Data Transfer In Rotary Wing Aircraft

FLIGHT CONTROL SYSTEM FOR ROTARY WING AIRCRAFT

MODULE FOR INTEGRATED APPROACH TO AN OFFSHORE FACILITY