Textron Innovations Inc.

The Boeing Company

Bell Helicopter Textron Inc.

Robert Blyth

Robert L Fortenbaugh

Ronald Lorenz Kisor

Jose Manuel Rodriguez

Brady Garrett Atkins

Peter Carlton Mehl

Paul Raymond Wilkinson

Terrence Patrick Brehn

A method of determining a center of gravity of an aircraft in flight by comparing actual control surface actuator displacements to expected control surface actuator displacements. And a method of fuel/load management based on an offset of the center of gravity from a preferred center of gravity and a handling qualities factor.

Method of determining the center of gravity of an aircraft and a method of fuel/load management based thereon

A system includes a first mast torque transfer system, a second mast torque transfer system coupled to the first mast torque transfer system, and a torque limiting system. The torque limiting system includes a first sensor configured to determine a torque of the first mast torque transfer system, a second sensor configured to determine a torque of the second mast torque transfer system, and a processor configured to determine a differential torque between the torque of the first mast torque transfer system and the torque of the second mast torque transfer system and configured to control at least one of a torque input and a torque output to at least one of the first and second mast torque transfer systems as a function of the determined differential torque.

Tilt-rotor over-torque protection from asymmetric gust

A control system having a first loop configured to provide a longitudinal blowback value of a rotor blade during flight and a second loop associated with the first loop, the second loop being configured to provide a design maximum total flapping value and a lateral flapping value. A method includes calculating a flight control limit from the design maximum total flapping value and the lateral flapping value. An upper longitudinal cyclic control limit is calculated by adding the flight control limit to the longitudinal blowback value. A lower longitudinal cyclic control limit is calculated by subtracting the flight control limit from the longitudinal blowback value.

System and method for limiting cyclic control inputs

Growing community of inventors

Fort Worth, TX, United States of America

Robert Blyth