Lockheed Martin Corporation

Sikorsky Aircraft Corporation

William C Fell, Jr

Jason E Browning

Matthew T Luszcz

Kathryn P Guy

Stacey Ann Sanchez

Matthew A White

David L Adams

Kevin L Bredenbeck

Steven D Marzella

A power display of an aircraft having a main rotor system and a translational thrust includes a reference member, a first indicator arranged adjacent the reference member and operable to display a power being used by the main rotor system, and a second indicator arranged adjacent the reference member and operable to display a power being used by the translational thrust system.

Power display for compound aircraft using shared engine torque

Flight display screen or portion thereof including a power indicator icon

A method of automating entry of an aircraft into autorotation includes detecting a loss of engine power, analyzing a sensed height and sensed airspeed of the aircraft, determining an adjusted position of one or more control surfaces of the aircraft in response to the sensed height and sensed airspeed, and automatically moving the one or more control surfaces to the adjusted position.

Automated autorotation and pilot aiding system

According to an aspect, a collaborative aircraft display system includes an aircraft, a first display unit in a first position of the aircraft and in operable communication with a buffer unit, a second aircraft display in a second position and in operable communication with the buffer unit, where the first display unit operable to transmit a distinct copy of first data to the second display unit via a haptic stimulus, and where the buffer unit operable to filter a second data from being transmitted to the second display unit.

Advanced multi-touch capabilities

An aircraft is provided including at least one pilot input and a flight control system n communication with the at least one pilot input. The flight control system is operable in a manual mode and a pointing mode. In the manual mode, a velocity, position, and attitude of the aircraft are controlled manually, and in the pointing mode, at least one of the velocity and position of the aircraft is controlled by the flight control system and at least one of the attitude and heading of the aircraft is controlled manually.

Precision pointing mode of an aircraft

Growing community of inventors

Stuart, FL, United States of America

William C Fell, Jr