1
Andrew T Johnson, Casey Hanlon: Motor having controllable torque. Honeywell International, Ingrassia Fisher & Lorenz P C, February 28, 2012: US08125168 (34 worldwide citation)

A controllable motor includes a rotor. A first stator winding set is operable, upon being energized, to generate and apply a first torque to the rotor. A second stator winding set independent of the first stator winding set is operable, upon being energized, to generate and apply a second torque to ...


2
Andrew T Johnson, Casey Hanlon, Calvin C Potter: Distributed flight control surface actuation system. Honeywell International, Ingrassia Fisher & Lorenz P C, July 7, 2009: US07556224 (18 worldwide citation)

An aircraft flight control surface actuation system includes a plurality of flap actuators, and a plurality of slat actuators. The actuators receive actuator position commands from an actuator control unit and, in response, move flaps and slats between stowed and deployed positions. The flight contr ...


3
Casey Hanlon, Paul T Wingett, Calvin C Potter: Electric flight control surface actuation system for aircraft flaps and slats. Honeywell International, Ingrassia Fisher & Lorenz P C, June 23, 2009: US07549605 (14 worldwide citation)

An aircraft flight control surface actuation system includes a plurality of electric motors-driven flap actuators, and a plurality of electric motor-driven slat actuators. The motor-driven actuators receive activation signals from flap and slat actuator controllers and is, in response to the activat ...


4
Larry J Yount, Casey Hanlon, Andrew T Johnson, Joseph Jackson: Load optimized redundant flight control surface actuation system and method. Honeywell International, Ingrassia Fisher & Lorenz P C, October 11, 2011: US08033509 (13 worldwide citation)

An aircraft flight surface control system and method simultaneously provides the benefits of both an active/active system architecture and in active/standby system architecture. The system is preferably implemented using hydraulic actuator assemblies and electromechanical actuator assemblies coupled ...


5
Paul T Wingett, Casey Hanlon, Calvin C Potter: Flight control surface actuator assembly including a free trial mechanism. Honeywell International, Ingrassia Fisher & Lorenz P C, November 3, 2009: US07610828 (12 worldwide citation)

A flight control surface actuator includes a mechanism that enables the actuator translation member to be selectively decoupled from the actuator rotating member. The actuator includes an actuation member, a translation member, an extension member, and a locking member. The actuation member is adapt ...


6
Calvin C Potter, Casey Hanlon, Paul T Wingett: Motor control architecture for simultaneously controlling multiple motors. Honeywell International, Robert Desmond Esq, December 20, 2011: US08080966 (12 worldwide citation)

A motor control architecture is provided that simultaneously controls multiple motors. The motor control system includes memory, a plurality of motor control processors, and a communication controller. The motor control processors are each responsive to control signals supplied from the communicatio ...


7
Donald J Christensen, Casey Hanlon, Douglas T Hopper, Andrew Johnson, Robert D Kortum: Thrust reverser system actuator having an integral torque limiter. Honeywell International, Ingrassia Fisher & Lorenz, December 13, 2005: US06974107 (11 worldwide citation)

A thrust reverser system actuator assembly is provided that includes a torque limiter to limit the number of torque that may be applied to the actuator assembly. The actuator assembly includes an actuator and a torque limiter assembly. The actuator is adapted to receive a drive force and is configur ...


8
J Casey Hanlon, Pablo Bandera: Control system for an exoatmospheric kill vehicle. Honeywell International, Ingrassia Fisher & Lorenz, December 27, 2011: US08084726 (11 worldwide citation)

A control system for a maneuverable kill vehicle is provided. The control system includes a pressurized fluid source configured to provide a pressurized fluid, a valve in fluid communication with the pressurized fluid source, and a voice coil actuator comprising a magnet and a conductive coil orient ...


9
Calvin C Potter, Casey Hanlon, Paul T Wingett: Component position determination circuit using a brushless DC motor commutation sensor. Honeywell International, Ingrassia Fisher & Lorenz P C, February 3, 2009: US07486042 (10 worldwide citation)

A position determination circuit uses the commutation sensor of a brushless DC motor to determine the position of an actuator and/or actuated component 125. The commutation sensor supplies a rotational position signal representative of the rotational position of the motor to a pulse generator. The p ...


10
Casey Hanlon, Dave Eschborn: Active control stick assembly including traction drive. Honeywell International, Ingrassia Fisher & Lorenz, January 3, 2012: US08087619 (8 worldwide citation)

An active control stick assembly. In one embodiment, the active control stick assembly includes a housing assembly, a control stick coupled to the assembly housing for rotation about at least a first rotational axis, a first artificial force feel (AFF) motor disposed in the housing assembly, and a f ...