Sikorsky Aircraft Corporation

Other

David L Adams

Kevin Ron Fimbers

Matthew T Luszcz

Mark R Alber

William P Fell

William C Fell, Jr

Mary Eileen Adams

Steven D Marzella

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

An airspeed indicator display for an aircraft having a main rotor system and a translational thrust system includes a first indicator operable to display an actual airspeed of the aircraft and a second indicator positioned adjacent the first indicator. The second indicator is operable to display an actual pitch angle of the translational thrust system.

Composite airspeed indicator display for compound aircrafts

A torque indicator for an aircraft having a main rotor system and a translational thrust system driven by at least one engine includes a first indicator operable to display an actual torque of an engine of the aircraft relative to an engine torque limit, a second indicator operable to display an actual torque of the translational thrust system of the aircraft relative to a translational thrust system torque limit, and a third indicator operable to display an actual torque of the main rotor system of the aircraft relative to a main rotor system torque limit.

Flight display screen or portion thereof with graphical user interface including a composite indicator

A flight control system for an aircraft includes a flight control computer operatively interconnected with a main rotor system and a translational thrust system of the aircraft. A selectively enabled integrated target and flight control system arranged in communication with the flight control computer. The integrated target flight and control system is configured to control pitch attitude and heading of the aircraft. When the integrated target and flight control system is enabled, at least partial operation of the aircraft is controlled in response to a pilot input via the flight control computer.

Attitude-coupled targeting system for rotary wing aircraft

A computer implemented method for displaying aircraft systems information on an aircraft display relating to and facilitating operation of an aircraft are disclosed herein. The method can include displaying a plurality of system indicators in a system indicator region of an aircraft display. At least two of the indicators of the plurality of system indicators in the system indicator region are disposed in a structurally approximated relationship relative to each other to increase system recognition and/or interpretation of status of a corresponding physical system indicated by each indicator.

Aircraft information systems

A well screen for preventing contaminants such as debris, pests, and insects from falling into the well water. The well screen includes a barrier having top and bottom faces with a plurality of apertures therethrough. A plurality of elongate hanging arms are upwardly extended from the top face of the barrier. The hanging arms each have an outwardly extending upper extent.

Growing community of inventors

Wallingford, CT, United States of America

David L Adams