The Boeing Company

Jason William Clark

Samantha Ann Schwartz

Cindy Dorfmann

Jeffrey Lee Williams

Matthew Bonbright Hendrian

Susan Anne Foster

Katie M Reid

Aaron Daniel Pilcher

Willard Kyle Otto

Andre Lutz

Andres Chapiro Fermon

Andreas Sindlinger

Thorsten Wiesemann

Patrick Ralf Wipplinger

Brian A Azcuenaga

Jakub Dziecielski

Jonasz Rudnik

Alexander V Korolev

Aleksander Rydzewski

Jeffrey L Williams

Markus Florian Peukert

Michal Ruminski

Matthew Robert Price

Milan Guenther

Jonas Hatzenbuehler

Piotr Marian Mazuz

Mitchell G Woolever

Joshua T Glazer

Diana Marie Baca

The present disclosure provides for informed de-icing by identifying a travel time range for an aircraft from a de-icing station to a runway; identifying a holdover window based on predicted weather conditions during the travel time range; estimating a takeoff time for the aircraft based on a takeoff queue for the runway and the travel time range; and in response to the holdover window expiring before the estimated takeoff time, delaying the aircraft from de-icing. In some aspects, informed de-icing includes, in response to identifying an aircraft scheduled for de-icing within a caution threshold of a scheduled takeoff time and to determining that a push time cannot be delayed: evaluating an effect of repeating a de-icing operation for the aircraft on flight operations; and in response to the effect exceeding an impact threshold: rescheduling the de-icing operation for the aircraft based on a new takeoff time.

Informed de-icing procedures for aircraft flight preparations

A system and a method include at least one control unit that determines a de-icing time for an aircraft within a de-icing area of an airport, predicts a de-icing time for an aircraft within a de-icing area of an airport, schedules de-icing times for a plurality of aircraft within a de-icing area of an airport, and/or predicts demand for future de-icing operations of aircraft within a de-icing area of an airport.

Aircraft de-icing determination systems and methods

A runway exiting system is configured to determine a suitable exit off of a runway for an aircraft. The runway exiting system includes a housing, and one or more processors within the housing that are configured to determine a current position of the aircraft on the runway, determine a current rate of deceleration of the aircraft on the runway, and determine the suitable exit off of the runway for the aircraft based, at least in part, on the current position of the aircraft on the runway and the current rate of deceleration of the aircraft on the runway.

Runway exiting systems and methods for aircraft

A system and method is disclosed for providing dynamic tactile feedback. A tactile feedback generator is mounted in each vehicle in a group of vehicles and is coupled to provide a controllable tactile feedback signal to an operator of each vehicle in the group of vehicles upon receipt of an activation signal. A tactile feedback control device is mounted in each vehicle in the group of vehicles and is coupled to the tactile feedback generator for selectively providing an activation signal and a tactile feedback characteristic signal thereto. An accelerometer is positioned within each vehicle in the group of vehicles. A turbulence processing unit is coupled to receive accelerometer data from each accelerometer. The turbulence processing unit processes the accelerometer data to identify characteristics of a current level of turbulence-induced vibration, and, based thereon, selects and provides updated tactile feedback characteristics to each tactile feedback control device.

System and method for providing dynamic tactile feedback to a vehicle operator

A wearable electronic display system detects aircraft flight related conditions, compares the detected flight related conditions with rules or procedures, retrieves flight condition information relating to phase of flight, and displays small amounts of contextually relevant flight condition information on a display screen.

Wearable electronic display and method for displaying information to a pilot

A flight range-restricting system is configured to control a flight range of an unmanned aerial vehicle (UAV). The flight range-restricting system includes a database including a UAV capabilities storage area that stores UAV capabilities data indicative of technical specifications of the UAV, and a restricted airspace storage area that stores restricted airspace data indicative of a restricted airspace. A range-restricting control unit is communicatively coupled to the database. The range-restricting control unit controls the flight range of the UAV based on a current location of the UAV, the UAV capabilities data, and the restricted airspace data.

Flight range-restricting systems and methods for unmanned aerial vehicles

An instrument panel is identified based on a captured image such as a photograph. A target configuration of the instrument panel is compared with a current configuration of the instrument panel based on the image data. An indication of differences between the target configuration and the current configuration is provided.

Virtual instrument verification tool

Systems and methods for use in identifying at least one alternate airport for an aircraft. One example method includes identifying a plurality of airports based on static data associated with the plurality of airports, and identifying, at a processing device, at least one preferred airport from the plurality of airports based on dynamic data associated with at least the at least one preferred airport, wherein the static data and/or the dynamic data is associated with at least one weight that enables at least one of the plurality of airports to be identified based on a relative importance of the static data and/or the dynamic data.

Systems and methods for use in identifying at least one alternate airport

A method for providing a minimum safe altitude indication on an aircraft display is described. The method includes utilizing current aircraft heading and position data to generate a location and orientation for an own-ship depiction with respect to an aircraft display, utilizing the current position data, along with terrain data, to generate minimum safe altitude data for an area surrounding the aircraft, and displaying on the aircraft display, about the location for own-ship depiction, the minimum safe altitudes surrounding the aircraft.

Methods and systems for depicting a data driven minimum safe altitude

The different advantageous embodiments provide a system comprising a computer, first program code stored on the computer, and second program code stored on the computer. The computer is configured to run the first program code to retrieve flight status information during a flight and generate four dimensional flight information. The four dimensional flight information includes a comparison of the flight status information to a flight plan for the flight. The computer is configured to run the second program code to depict the four dimensional flight information in a textual format.

Four dimensional trajectory based operation flight plans

A method and apparatus for managing a touch screen system. Data generated by an acceleration detector about acceleration of the touch screen system is received. The acceleration detector is located within the touch screen system. An action is initiated by an input manager when the acceleration of the touch screen system reduces usability of the touch screen system.

Turbulence mitigation for touch screen systems

A method and apparatus for managing a map of an airport. The map of the airport is displayed on a display device. A movement of a number of fingers with respect to a number of aeronautical objects on the map of the airport is detected. Information generated by an operation based on the number of aeronautical objects on the map of the airport is displayed in response to detecting the movement of the number of fingers with respect to the number of aeronautical objects on the map of the airport.

Aircraft charting system with multi-touch interaction gestures for managing a map of an airport

A method, computer system, and computer program product for displaying flight information. A number of elements for a number of phases of flight for a route of an aircraft are identified. The number of elements in association with the number of phases of flight is displayed on a strip on a display. The number of elements is displayed on the strip in a sequence in which the number of elements is encountered by the aircraft on the route during the number of phases of flight.

Data driven route strip

Systems and methods for use in identifying at least one alternate airport for an aircraft. One example method includes identifying a plurality of alternate airports based on static data associated with the plurality of alternate airports, identifying, at a processing device, at least one preferred alternate airport from the plurality of alternate airports based on dynamic data associated with the plurality of alternate airports, and storing the at least one preferred alternate airport. The dynamic data includes at least one of visibility information and traffic density information.

Growing community of inventors

Evergreen, CO, United States of America

Jason William Clark