Robert E. Winkel

Person

Phoenix, AZ, US

People

Patents Grantslast 30 patents

Information Patent Grant
Vibration reduction system employing active bearing mounts
- Patent number 8,002,251
- Issue date Aug 23, 2011
- Honeywell International Inc.
- Timothy A. Hindle
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Self-powered spacecraft attitude control system and method
- Patent number 7,721,998
- Issue date May 25, 2010
- Honeywell International Inc.
- Louis R. Jackson
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Satellite active motion damping
- Patent number 7,690,602
- Issue date Apr 6, 2010
- Honeywell International Inc.
- Louis R. Jackson
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Fast-pivot missile flight control surface
- Patent number 7,325,769
- Issue date Feb 5, 2008
- Honeywell International, Inc.
- Paul E. Harnisch
- F42 - AMMUNITION BLASTING
Information Patent Grant
Passive, double acting, vacuum actuated vent valve
- Patent number 7,299,817
- Issue date Nov 27, 2007
- Honeywell International, Inc.
- Gary L. Gisler
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Method of constructing a rotor for a gyroscopic device
- Patent number 7,000,308
- Issue date Feb 21, 2006
- Honeywell International Inc.
- Stephen E. Fiske
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Tilt table
- Patent number 6,182,582
- Issue date Feb 6, 2001
- Honeywell International Inc.
- David Arthur Bailey
- B64 - AIRCRAFT AVIATION COSMONAUTICS

Patents Applicationslast 30 patents

Information Patent Application
VIBRATION REDUCTION SYSTEM EMPLOYING ACTIVE BEARING MOUNTS
- Publication number 20090121399
- Publication date May 14, 2009
- Honeywell International, Inc.
- Timothy A. Hindle
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ROTOR ASSEMBLIES HAVING SHAFTS WITH INTEGRAL BEARING RACEWAYS
- Publication number 20090100957
- Publication date Apr 23, 2009
- Honeywell International, Inc.
- Robert E. Winkel
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
SELF-POWERED SPACECRAFT ATTITUDE CONTROL SYSTEM AND METHOD
- Publication number 20080223990
- Publication date Sep 18, 2008
- Honeywell International, Inc.
- Louis R. Jackson
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
FAST-PIVOT MISSILE FLIGHT CONTROL SURFACE
- Publication number 20080029642
- Publication date Feb 7, 2008
- Honeywell International, Inc.
- Paul E. Harnisch
- F42 - AMMUNITION BLASTING
Information Patent Application
Satellite active motion damping
- Publication number 20070252044
- Publication date Nov 1, 2007
- Louis R. Jackson
- G05 - CONTROLLING REGULATING
Information Patent Application
Passive, double acting, vacuum actuated vent valve
- Publication number 20060042697
- Publication date Mar 2, 2006
- Gary L. Gisler
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
Anti-backlash method and system for multiple mesh gear train
- Publication number 20040089089
- Publication date May 13, 2004
- Carlos J. Stevens
- F16 - ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINT...
Information Patent Application
Rotor for control moment gyroscopes and reaction wheel assemblies
- Publication number 20030140479
- Publication date Jul 31, 2003
- Stephen E. Fiske
- G01 - MEASURING TESTING

Robert E. Winkel

Person

Patents Grantslast 30 patents

Vibration reduction system employing active bearing mounts

Self-powered spacecraft attitude control system and method

Satellite active motion damping

Fast-pivot missile flight control surface

Passive, double acting, vacuum actuated vent valve

Method of constructing a rotor for a gyroscopic device

Tilt table

Patents Applicationslast 30 patents

VIBRATION REDUCTION SYSTEM EMPLOYING ACTIVE BEARING MOUNTS

ROTOR ASSEMBLIES HAVING SHAFTS WITH INTEGRAL BEARING RACEWAYS

SELF-POWERED SPACECRAFT ATTITUDE CONTROL SYSTEM AND METHOD

FAST-PIVOT MISSILE FLIGHT CONTROL SURFACE

Satellite active motion damping

Passive, double acting, vacuum actuated vent valve

Anti-backlash method and system for multiple mesh gear train

Rotor for control moment gyroscopes and reaction wheel assemblies