Textron Innovations Inc.

Bell Textron Inc.

Bell Helicopter Textron Inc.

Carey Cannon

James Gibson

Frank B Stamps

Brent Chadwick Ross

Levi Charles Hefner

Kip Gregory Campbell

Joseph Scott Drennan

Alan Carl Ewing

Yann Lavallee

Brett Rodney Zimmerman

Michael Kevin McNair

William Kyle Heironimus

Christopher John Stroncek

Jaret F Burgess

A control device for an aircraft has a control stick configured to be operated by hand of a user. The control stick is pivotable about a longitudinal axis, a lateral axis, and a yawing axis extending through the control stick. Motion of the stick about the longitudinal axis is configured to cause roll motion of the aircraft, motion of the stick about the lateral axis is configured to cause pitch motion of the aircraft, and motion of the stick about the yawing axis is configured to cause yaw motion of the aircraft. Rotation of a thumbwheel carried by the control stick changes a magnitude of a thrust vector of the aircraft.

Apparatus and method for piloting an aircraft

A method of operating a targeting system simulation tool (TSST) includes providing a TSST configured to receive an obstacle/effect parameterization, a simulation parameterization, a sensor parameterization, an aircraft parameterization, and an autonomy parameterization. The method further includes receiving by the TSST, at least one of each of an obstacle/effect parameterization and a simulation parameterization. The method further includes receiving by the TSST, either (1) a sensor parameterization or (2) an aircraft parameterization. The method further includes operating the TSST to apply the provided ones of the obstacle/effect parameterization, simulation parameterization, sensor parameterization, and aircraft parameterization to generate a value, value range, or value limit for the unprovided aircraft parameterization or unprovided sensor parameterization.

Targeting system and simulator therefor

A helicopter includes a full authority digital engine controlled (FADEC) engine, a first two-position throttle switch disposed on a first collective control stick, the first two-position throttle switch being movable between a Fly position and an Idle position, and a second two-position throttle switch disposed on a second collective control stick, the second two-position throttle switch being movable between a Fly position and an Idle position.

Collective control stick mounted throttle control assembly

A pusher rotorcraft is provided in one example embodiment and may include at least one engine in mechanical communication with a drop-down gearbox; a driveshaft in mechanical communication with the drop-down gearbox, a main rotor gearbox, and a tail system gearbox; a main rotor system in mechanical communication with the main rotor gearbox; an anti-torque system in mechanical communication with the tail system gearbox; and a pusher propeller system in mechanical communication with the tail system gearbox.

Pusher rotorcraft drivetrain

Control grip

Growing community of inventors

Colleyville, TX, United States of America

Carey Cannon