Dean Wilkens

Person

Scottsdale, AZ, US

People

Patents Grantslast 30 patents

Information Patent Grant
Methods and systems for displaying simplified primary flight inform...
- Patent number 12,087,170
- Issue date Sep 10, 2024
- Honeywell International Inc.
- Jacob Kirk Maxfield
- G08 - SIGNALLING
Information Patent Grant
Systems and methods for model based vehicle navigation
- Patent number 11,790,793
- Issue date Oct 17, 2023
- Honeywell International Inc.
- Sally Ann Keyes
- G08 - SIGNALLING
Information Patent Grant
Systems and methods for model based inertial navigation for a spinn...
- Patent number 11,781,836
- Issue date Oct 10, 2023
- Honeywell International Inc.
- Sally Ann Keyes
- F41 - WEAPONS
Information Patent Grant
Redundant fly-by-wire systems with fault resiliency
- Patent number 11,155,341
- Issue date Oct 26, 2021
- Honeywell International Inc.
- Dean Wilkens
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Fly-by-wire systems and related operating methods
- Patent number 11,097,834
- Issue date Aug 24, 2021
- Honeywell International Inc.
- Dean Wilkens
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Hydrostatic automatic flight servo systems
- Patent number 10,118,689
- Issue date Nov 6, 2018
- Honeywell International Inc.
- Pablo Bandera
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Automatic flight control actuator systems
- Patent number 10,106,245
- Issue date Oct 23, 2018
- Honeywell International Inc.
- Dean Wilkens
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Automatic flight control actuator systems
- Patent number 10,030,756
- Issue date Jul 24, 2018
- Honeywell International Inc.
- Dean Wilkens
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Dual lane control of a permanent magnet brushless motor using non-t...
- Patent number 8,084,972
- Issue date Dec 27, 2011
- Honeywell International Inc.
- Ronald E. Strong
- H02 - GENERATION CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
Information Patent Grant
Electromechanical actuation system and method
- Patent number 8,070,091
- Issue date Dec 6, 2011
- Honeywell International Inc.
- Dwayne M. Benson
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Fine resolution motor control
- Patent number 8,058,833
- Issue date Nov 15, 2011
- Honeywell International Inc.
- Dean Wilkens
- H02 - GENERATION CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
Information Patent Grant
Rate limited active pilot inceptor system and method
- Patent number 8,002,220
- Issue date Aug 23, 2011
- Honeywell International Inc.
- Dean R. Wilkens
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Aircraft flight control user interface linkage system
- Patent number 7,640,743
- Issue date Jan 5, 2010
- Honeywell International Inc.
- Casey Hanlon
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Position sensor and actuating system
- Patent number 6,700,345
- Issue date Mar 2, 2004
- Honeywell Inc.
- Dean Wilkens
- F16 - ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINT...
Information Patent Grant
Methods and apparatus suitable for facilitating control of an aircr...
- Patent number 6,586,901
- Issue date Jul 1, 2003
- Honeywell International Inc.
- Donald James Singer
- G05 - CONTROLLING REGULATING
Information Patent Grant
Fail passive servo controller
- Patent number 6,573,672
- Issue date Jun 3, 2003
- Honeywell International Inc.
- Kenneth O'Rourke
- H02 - GENERATION CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
Information Patent Grant
Cockpit display having 3D flight path error symbology
- Patent number 6,320,579
- Issue date Nov 20, 2001
- Honeywell International Inc.
- Mark I. Snyder
- G01 - MEASURING TESTING
Information Patent Grant
Method and apparatus for navigating an aircraft from an image of th...
- Patent number 6,157,876
- Issue date Dec 5, 2000
- Honeywell International Inc.
- Norman G. Tarleton
- G05 - CONTROLLING REGULATING
Information Patent Grant
Three dimensional lateral displacement display symbology which is c...
- Patent number 5,745,863
- Issue date Apr 28, 1998
- Honeywell Inc.
- Dale A. Uhlenhop
- G01 - MEASURING TESTING
Information Patent Grant
Method and apparatus for conformal runway alignment on a head up di...
- Patent number 5,745,054
- Issue date Apr 28, 1998
- Honeywell Inc.
- Dean Richard Wilkens
- G05 - CONTROLLING REGULATING

Patents Applicationslast 30 patents

Information Patent Application
HIGH-INTEGRITY ACTUATOR CONTROLLER AND CONTROL SYSTEMS
- Publication number 20230291336
- Publication date Sep 14, 2023
- Honeywell International Inc.
- Darrell Horner
- H03 - BASIC ELECTRONIC CIRCUITRY
Information Patent Application
SYSTEMS AND METHODS FOR MODEL BASED INERTIAL NAVIGATION FOR A SPINN...
- Publication number 20220282955
- Publication date Sep 8, 2022
- Honeywell International Inc.
- Sally Ann Keyes
- F41 - WEAPONS
Information Patent Application
SYSTEMS AND METHODS FOR MODEL BASED VEHICLE NAVIGATION
- Publication number 20220223054
- Publication date Jul 14, 2022
- Honeywell International Inc.
- Sally Ann Keyes
- G08 - SIGNALLING
Information Patent Application
METHODS AND SYSTEMS FOR DISPLAYING SIMPLIFIED PRIMARY FLIGHT INFORM...
- Publication number 20220122471
- Publication date Apr 21, 2022
- Honeywell International Inc.
- Jacob Maxfield
- G08 - SIGNALLING
Information Patent Application
FLY-BY-WIRE SYSTEMS AND RELATED OPERATING METHODS
- Publication number 20200262544
- Publication date Aug 20, 2020
- HONEYWELL INTERNATIONAL INC.
- Dean Wilkens
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
REDUNDANT FLY-BY-WIRE SYSTEMS WITH FAULT RESILIENCY
- Publication number 20200031454
- Publication date Jan 30, 2020
- HONEYWELL INTERNATIONAL INC.
- Dean Wilkens
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
AUTOMATIC FLIGHT CONTROL ACTUATOR SYSTEMS
- Publication number 20170350491
- Publication date Dec 7, 2017
- HONEYWELL INTERNATIONAL INC.
- Dean Wilkens
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
AUTOMATIC FLIGHT CONTROL ACTUATOR SYSTEMS
- Publication number 20170106971
- Publication date Apr 20, 2017
- HONEYWELL INTERNATIONAL INC.
- Dean Wilkens
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
HYDROSTATIC AUTOMATIC FLIGHT SERVO SYSTEMS
- Publication number 20170043861
- Publication date Feb 16, 2017
- Honeywell International Inc.
- Pablo Bandera
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
FINE RESOLUTION MOTOR CONTROL
- Publication number 20100102765
- Publication date Apr 29, 2010
- Honeywell International Inc.
- Dean Wilkens
- H02 - GENERATION CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
Information Patent Application
HYBRID ELECTROMECHANICAL/HYDRO-MECHANICAL ACTUATION CONTROL SYSTEM
- Publication number 20100089053
- Publication date Apr 15, 2010
- Honeywell International Inc.
- Casey Hanlon
- F15 - FLUID-PRESSURE ACTUATORS HYDRAULICS OR PNEUMATICS IN GENERAL
Information Patent Application
ELECTROMECHANICAL ACTUATION SYSTEM AND METHOD
- Publication number 20100084517
- Publication date Apr 8, 2010
- Honeywell International Inc.
- Dwayne M. Benson
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
RATE LIMITED ACTIVE PILOT INCEPTOR SYSTEM AND METHOD
- Publication number 20090302171
- Publication date Dec 10, 2009
- Honeywell International, Inc.
- Dean R. Wilkens
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
DUAL LANE CONTROL OF A PERMANENT MAGNET BRUSHLESS MOTOR USING NON-T...
- Publication number 20090128072
- Publication date May 21, 2009
- Honeywell International, Inc.
- Ronald E. Strong
- H02 - GENERATION CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
Information Patent Application
AIRCRAFT FLIGHT CONTROL USER INTERFACE LINKAGE SYSTEM
- Publication number 20090039205
- Publication date Feb 12, 2009
- Honeywell International, Inc.
- Casey Hanlon
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
Active pilot flight control stick system with passive electromagnet...
- Publication number 20080156939
- Publication date Jul 3, 2008
- Honeywell International, Inc.
- Casey Hanlon
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
METHOD AND APPARATUS FOR FINE RESOLUTION BRUSHLESS MOTOR CONTROL
- Publication number 20040080290
- Publication date Apr 29, 2004
- Bryan H. Hill
- G01 - MEASURING TESTING
Information Patent Application
Position sensor and actuating system
- Publication number 20030090228
- Publication date May 15, 2003
- Dean Wilkens
- G05 - CONTROLLING REGULATING
Information Patent Application
Fail passive servo controller
- Publication number 20030001530
- Publication date Jan 2, 2003
- Kenneth O'Rourke
- G05 - CONTROLLING REGULATING

Dean Wilkens

Person

Patents Grantslast 30 patents

Methods and systems for displaying simplified primary flight inform...

Systems and methods for model based vehicle navigation

Systems and methods for model based inertial navigation for a spinn...

Redundant fly-by-wire systems with fault resiliency

Fly-by-wire systems and related operating methods

Hydrostatic automatic flight servo systems

Automatic flight control actuator systems

Automatic flight control actuator systems

Dual lane control of a permanent magnet brushless motor using non-t...

Electromechanical actuation system and method

Fine resolution motor control

Rate limited active pilot inceptor system and method

Aircraft flight control user interface linkage system

Position sensor and actuating system

Methods and apparatus suitable for facilitating control of an aircr...

Fail passive servo controller

Cockpit display having 3D flight path error symbology

Method and apparatus for navigating an aircraft from an image of th...

Three dimensional lateral displacement display symbology which is c...

Method and apparatus for conformal runway alignment on a head up di...

Patents Applicationslast 30 patents

HIGH-INTEGRITY ACTUATOR CONTROLLER AND CONTROL SYSTEMS

SYSTEMS AND METHODS FOR MODEL BASED INERTIAL NAVIGATION FOR A SPINN...

SYSTEMS AND METHODS FOR MODEL BASED VEHICLE NAVIGATION

METHODS AND SYSTEMS FOR DISPLAYING SIMPLIFIED PRIMARY FLIGHT INFORM...

FLY-BY-WIRE SYSTEMS AND RELATED OPERATING METHODS

REDUNDANT FLY-BY-WIRE SYSTEMS WITH FAULT RESILIENCY

AUTOMATIC FLIGHT CONTROL ACTUATOR SYSTEMS

AUTOMATIC FLIGHT CONTROL ACTUATOR SYSTEMS

HYDROSTATIC AUTOMATIC FLIGHT SERVO SYSTEMS

FINE RESOLUTION MOTOR CONTROL

HYBRID ELECTROMECHANICAL/HYDRO-MECHANICAL ACTUATION CONTROL SYSTEM

ELECTROMECHANICAL ACTUATION SYSTEM AND METHOD

RATE LIMITED ACTIVE PILOT INCEPTOR SYSTEM AND METHOD

DUAL LANE CONTROL OF A PERMANENT MAGNET BRUSHLESS MOTOR USING NON-T...

AIRCRAFT FLIGHT CONTROL USER INTERFACE LINKAGE SYSTEM

Active pilot flight control stick system with passive electromagnet...

METHOD AND APPARATUS FOR FINE RESOLUTION BRUSHLESS MOTOR CONTROL

Position sensor and actuating system

Fail passive servo controller