Inventor

HANLON CASEY

US44 patents

⚠️ This page may combine multiple inventors who share the name “HANLON CASEY”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.

HANLON CASEY

HONEYWELL INT INC

Distributed flight control surface actuation system

Load optimized redundant flight control surface actuation system and method

Pilot flight control stick haptic feedback system and method

Flight control surface actuator assembly including a free trial mechanism

Flight control surface actuation system with redundantly configured and lockable actuator assemblies

Electric flight control surface actuation system for aircraft flaps and slats

Thrust reverser system actuator having an integral torque limiter

Ball screw actuator including a compliant ball screw stop

Ballscrew with an integral high-efficiency thrust bearing

Rudder pedal assembly including non-parallel slide rails

Component position determination circuit using a brushless DC motor commutation sensor

Thrust reverser system electro-mechanical brake manual release mechanism

Two-dimensional position sensing system

Aircraft accessory monitor

Motor balanced active user interface assembly

Electromechanical flight control system and method for rotorcraft

Ball screw actuator including an axial soft stop

Fully redundant spacecraft power and attitude control system

Power drive unit electromagnetic latch

Active rudder pedal mechanism with foreign object strike tolerance and articulating brake

Aircraft flight control user interface linkage system

User interface force sensor system

Active human-machine interface with force sensor overload protection

Threaded fastener positive anti-rotation locking device

Ball screw actuator including a compliant ball screw stop

Apparatus for releasably securing a rotatable object in a predetermined position

HANLON CASEY

Active control stick assembly including traction drive

Actuation assembly

High accuracy, zero backlash rotary-to-linear electromechanical actuator

Electromechanical brake actuator motor brake

Active pilot inceptor with self warm-up

Aircraft electric brake actuator assembly with line replaceable actuator brake

Active control stick assembly

Redundant electromechanical actuator for control surfaces

Active feedback user interface system and gimbal assembly therefor

Human-machine interface with integrated position sensors and passive haptic feedback devices

Aircraft control stick operational in active and passive modes

Brake actuator assembly with line replaceable motor features

Aircraft electric brake actuation system and method

JOHNSON ANDREW T

Motor having controllable torque

Dual drive electromechanical actuator with center output

Active user interface haptic feedback and linking control system using either force or position data

POTTER CALVIN C

Motor control architecture for simultaneously controlling multiple motors

BENSON DWAYNE M

Electromechanical actuation system and method