Rockwell Collins, Inc.

Mark Wayne Volner

Dinesh Kumar Kushwaha

Bradley R Mickelson

Norm W Arons

Kirk A Kolek

Michael G Espenes

Brannen M Clark

A system and method for computing and displaying a fuel optimal idle deceleration start point which minimizes the overall auto throttle movement keeping the throttle at idle detent throughout the maneuver thus minimizing the fuel burn and stress on engine. The need for speed brakes deployment is also reduced because the deceleration distance length is accordingly adjusted based on current parameters. The accurate solution takes into account the current condition such as aircraft weight, altitude and speed and environmental parameters such as wind and temperature. The computed deceleration start point is displayed on map/navigation and vertical display for enhanced flight crew awareness.

Optimum idle descent start point display based on current conditions

A system includes a processing circuit onboard an aircraft and configured to determine an optimum cruise profile for the aircraft based on a flight plan, a characteristic of the aircraft, and an environmental characteristic. The processing circuit is also configured to determine an optimized cruise vertical path based on the optimum cruise profile and air traffic information of at least one other aircraft, and control an autopilot system of the aircraft to cause the aircraft to follow the optimized cruise vertical path.

Systems and methods for optimized cruise vertical path

A system, device, and method for a takeoff (T/O) of an aircraft are disclosed. The T/O automating system may include an autothrottle system configured with a plurality of thrust modes, an autopilot system configured with a plurality of vertical guidance modes; and a flight management computer (FMC). The FMC may be configured to perform the method of receiving of input data representative of inputs of a T/O profile selection, a first profile altitude, a second profile altitude, and/or a third altitude; generating output data representative of outputs which includes a command engaging a thrust mode and a command engaging a vertical guidance mode to provide pitch attitude guidance commensurate to a speed and/or vertical speed; and providing the output data to the autothrottle system and the autopilot system. In some embodiments, the T/O profile could be a profile designed for one or more noise abatement departure profiles.

Takeoff automating system, device, and method

Present novel and non-trivial system, device, and method for generating a vertical path profile are disclosed. The vertical path profile generating system is comprised of a source of navigation data, a source of performance factors data, a vertical path generator ('VPG') and a presentation system. The VPG may be configured to receive the navigation data representative of takeoff runway information; receive the performance data may be representative of aircraft performance factors; determine a first vertical path and/or second vertical path as a function of criteria employing the navigation data and the performance data; generate presentation data responsive to the determination; and provide the presentation data to one or more presentation devices comprised of, in part, a visual display unit configured to display a first takeoff path profile and/or a second takeoff path profile.

Vertical path profile generating system, device, and method

A present novel and non-trivial system, device, and method for presenting winds aloft symbology on an aircraft display unit are disclosed. Symbology image data representative of a plurality of sets of winds aloft symbologies may be generated as a function of flight plan data and weather data; flight plan data representative flight plan comprised of a plurality of waypoints may be received along with weather data representative of winds aloft data corresponding to each waypoint. Each set of winds aloft symbologies may be comprised of winds aloft symbology corresponding to each waypoint of the flight plan at a single altitude and symbolize winds aloft at that altitude. When provided to a display unit, each set of winds aloft symbologies represented in the symbology image data may be presented in a series of increasing or decreasing altitudes, where the series is presented sequentially or simultaneously.

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Marion, IA, United States of America

Mark Wayne Volner