The Boeing Company

Joseph Adam Sikora

Thomas A Campbell

Phuong H Nguyen

Michael Edwin Foster

John Wiedemann

Samuel T Clark

Kent Edmund Karnofski

Matthew August Lassen

Adam Marshall Thoreen

Joshua Jay Baer

Roglenda R Bowe

Mark Ivan Nikolic

Jean Marie Crane

Andrew William Houck

Michael B McAvoy

Jennifer L Gertley

Bryan P Kesterson

Phuoc D Nguyen

Timothy Patrick Gallagher, Jr

Justin Eugene Hale

Norman F Kirby

George H Hamasaki

Robert J Crane

Thanh-Ha N Herter

Gregory P Owens

Timothy P Gallagher

William Lawrence Hunt

Jr Gallagher Timothy Patrick

Farhad R Shroff

Joshua J Baer

Matthew A Lassen

Michael E Foster

A method and apparatus for a wingtip control system. The wingtip control system comprises a switch system for a flight deck of an aircraft and a controller. The switch system is configured to be placed into an armed state and generate an armed signal. The controller is in communication with the switch system. The controller is configured to receive the armed signal from the switch system, visually indicate a desired position for a wingtip of the aircraft in the switch system in response to an event occurring during operation of the aircraft, and generate a movement command to move the wingtip.

Wingtip control system

A system and method for braking an aircraft. A processor unit identifies an operating condition of the aircraft. The processor unit displays available modes indications on a display device on the aircraft. The available modes indications indicate modes of operating an automatic braking system on the aircraft that are available for selection by an operator based on the operating condition of the aircraft. The processor unit receives a mode selection from an operator interface. The mode selection indicates a selected mode of operating the automatic braking system that is selected by the operator from the available modes. The processor unit displays on the display device a selected mode indication indicating the selected mode.

Display-based flight deck autobrake selection

Systems and methods for operating aircraft power systems are disclosed. A power system in accordance with one embodiment of the invention includes an aircraft auxiliary power unit and a controller coupled to the aircraft auxiliary power unit, with the controller being configured to automatically stop the auxiliary power unit while the auxiliary power unit is functioning normally. The controller can also be configured to automatically start the auxiliary power unit in-flight when power supplied or expected to be supplied to a subsystem of the aircraft has a non-zero value at or below a threshold value. The controller may also be configured to start the auxiliary power unit when a load or expected load on the subsystem meets or exceeds a threshold value.

Automatic control systems for aircraft auxiliary power units, and associated methods

A method and a system for indicating a target idle running speed, a predicted core speed, a predicted time to running, current engine state or automation modes of an operating aircraft engine, and indicating that the current core speed of the aircraft engine is less than a target idle running speed or is abnormally decreasing towards a target idle running speed. The indicators may be visual or aural. The visual indicators may include graphical or numeric symbols indicating the target idle running speed, the direction of core speed change, the predicted core speed at some future time, or current engine state or automation mode.

Method and apparatus for indicating operational state of aircraft engine

Systems and methods for presenting information corresponding to circuit breakers and for controlling such circuit breakers are disclosed. In one embodiment, the system can include a menu-driven, pointer-accessible graphical user interface via which an operator can receive information corresponding to circuit breakers, and can automatically change the states of the circuit breakers. Menus of circuit breaker information can be organized by the state of the circuit breaker, the location of the circuit breaker, the bus to which the circuit breaker is coupled, the electrical system to which the circuit breaker belongs, and/or the system or subsystem of which the circuit breaker is a part. In further embodiments, the circuit breaker information can be organized according to custom-made arrangements.

Systems and methods for monitoring and controlling circuit breakers

A method and system for displaying aircraft engine information. In one embodiment, the method includes directing the display of an icon that represents an overall operational state of an aircraft engine, with the overall operational state including one of a started state and an unstarted state. The method can further include directing a change in a displayed characteristic of the icon when the overall operational state of the aircraft engine changes from the one of the started state and the unstarted state to the other of the started state and the unstarted state. In a further embodiment, the method can further include repeatedly directing changes in the display of the icon as the aircraft changes from the unstarted state to the started state.

Methods and systems for displaying aircraft engine characteristics

A method and system for displaying aircraft engine information. In one embodiment, the method includes directing the display of an icon that represents a qualitative, overall operational state of an aircraft engine, with the overall operational state being determined from a plurality of engine operating parameters. The method can further include directing a change in the display of the icon when the overall operational state of the aircraft engine changes from a first overall operational state to a second operational state. In a further aspect of this embodiment, the change in the characteristic of the icon can include a change in the color or other visual characteristic of the icon, and the color or other visual characteristic of the icon can correspond directly to instructions to the pilot for actions suggested or required as a result of the current engine operational state.

Method and apparatus for displaying aircraft engine characteristics

Growing community of inventors

Seattle, WA, United States of America

Joseph Adam Sikora