Rockwell Collins, Inc.

Kirschen A Seah

Sarah Barber

Felix B Turcios

Randy H Jacobson

Alan E Siniff

Jeffery A Finley

Matthew J Carrico

Scott F Bauler

Richard S Dove

Michael James Krenz

Patrick Dennis McCusker

Kevin Michael Kronfeld

William T Greenleaf

Pamela K Hahn

Christopher A Scherer

Hung-i B Tsai

Maureen A Lehman

Gregory D Murray

Lyndon L Dunbar

Alena L Benson

Steve L Oehlert

Deborah L Hardin

Michael J Beccario

Simon A Grosvenor

Christopher H Glass

Arnold Oldach

Eamon P Hegerty

Randy H Jacobsen

Travis S VanderKamp

Cockpit

Present novel and non-trivial methods for electronically recording a taxi route on a display unit are disclosed. In one method, a tax route entry window ('TREW') such as a taxi clearance entry window is used to present in smaller windows surfaces and next intersecting surfaces from which a pilot sequentially selects surfaces based upon surfaces stated in a taxi clearance. In another method, the TREW is comprised of an airport-specific keyboard or a traditional keyboard with visually-variable, interactive buttons, where an activation or deactivation of each button is dependent upon surfaces specified in the taxi clearance and potential intersecting surface. In another method, selections are made on the TREW and surfaces corresponding to the selections are highlighted in an image presenting a map of surfaces. Additionally, the image presenting a map of surfaces may be panned and zoom to the size of the highlighted surface.

Taxi route recording methods on an aircraft display unit

A plurality of present novel and non-trivial communication methods employed between the participants of a trajectory management operation is disclosed. A trajectory coordinator ('TC') generator may be configured to send data representative of a polling request to one or more of the participants, receive data responsive to the sending of the polling request, generate data representative of one or more proposed trajectories of the TC, and send data representative of each TC-proposed trajectory to an air navigation service provider ('ANSP') and/or a dispatch center (&#x201c;DC&#x201d;). When presented to a controller of the ANSP or a dispatcher of the DC, one or more of the trajectories may be sent to the aircraft system. In response, each ANSP-selected trajectory and each DC-selected trajectory may be presented to the pilot whom selects and approves one of the selected trajectories. In response, the pilot-selected trajectory may be sent to the ANSP and DC.

Communication methods employed by participants in a trajectory management operations

A present novel and non-trivial system, device, and method for presenting instrument approach procedure ('IAP') advisory information to a pilot of an aircraft are disclosed. An advisory generator ('AG') is programmed to retrieve or receive flight information representative of the current position of the aircraft, a designated airport, and at least one published IAP; weather minima data corresponding to each IAP; and one or more IAP suitability factors from a weather data source, a NOTAM data source, and/or an aircraft performance data source. The AG determines the suitability or availability of each published IAP, disables the pilot's selectability of each unsuitable or unavailable published IAP, and generates advisory data representative of information advising the pilot of the unsuitable or unavailable published IAP(s). Additionally, the AG is programmed to receive a pilot's override of an unsuitable or unavailable published IAP and enable the overridden unsuitable or unavailable IAP.

System, device, and method for presenting instrument approach procedure advisory information to a pilot on an aircraft

A head-up display system includes an aircraft, a predicted flight path generation component that calculates a predicted flight path over a period of time, and a graphic generation component configured to generate a graphical display and project it onto a combiner configured to combine the graphical display with a visual exterior view. A synthetic vision system includes an aircraft, a predicted flight path generation component that receives one or more state parameters and calculates a predicted flight path over a period of time, and a synthetic terrain generation component configured to generate a synthetic view which is displayed on a display. The graphical display and/or the synthetic view includes a three-dimensional depiction of the predicted flight path over the period of time generated utilizing one or more three-dimensional transforms, one or more graphical images based on flight data, and a three-dimensional graphical depiction of a flight plan.

Head-up display/synthetic vision system predicted flight path depiction

Present novel and non-trivial methods for presenting traffic information are disclosed. In a first method, data representative of ownship position, first traffic, and second traffic are received by a traffic symbology generator ('TSG'). The traffic is divided into zones and a correlation between the targets of the traffic is determined. A traffic symbology data set is generated by the TSG based upon the results of the correlation(s). In a second method, data representative of ownship position and first traffic, runway references, and a selectable display range are received by the TSG. The traffic is divided into zones, and a traffic symbology data set is generated by the TSG thereafter. In a third method, data representative of ownship position and first traffic are received by the TSG. The traffic is divided into zones, and a traffic symbology data set is generated by the TSG thereafter.

Methods for presenting traffic information on an aircraft display unit

A method of managing an aircraft in flight may include electronically monitoring for a presence of a threat object along a flight path of the aircraft and at a destination airport of the aircraft, and electronically generating an alert when the presence of the threat object is detected. The alert may include information enabling air traffic control (ATC), flight dispatch, and a pilot of the aircraft to make a collaborative flight path correction decision that may prevent the aircraft from being affected by the threat object.

Automated datalink alert and alternate advisory system

A system for providing the capability for a vehicle to avoid regions of signal interference from high energy (HE) electromagnetic (EM) radiation emitters. The system includes a processing module. A database is operatively connected to the processing module. The database comprises a plurality of geographical areas affected by HE EM radiation emitters and data associated with the geographical areas. The data includes location, lateral and vertical extents, and signal attenuation for selected geographical areas affected by HE EM radiation emitters. The data preferably also includes affected frequency spectrum for the selected geographical areas. A display system is operatively connected to the processing module. The processing module functions to receive information regarding the position of the vehicle and query the database to retrieve relevant HE EM radiation emitters which are a threat to the vehicle's ability to properly navigate or communicate. The relevant HE EM radiation emitters are displayed on the display system. The present invention provides enhanced situational awareness to the pilot and permits decision support systems to refine their trajectory through hazards.

Mapping, storage, retrieval and display of high energy electromagnetic radiation emitters

A system may include a sensor for coupling with a vehicle configured for atmospheric flight. The sensor may be configured for detecting a turbulence event, where the turbulence event is at least one of experienced by the vehicle or occurs proximal to the vehicle during atmospheric flight. The system may also include a transmitter coupled with the sensor. The transmitter may be configured for automatically remotely transmitting data regarding the turbulence event to a ground based entity.

Sensing, display, and dissemination of detected turbulence

A vehicle system for determining an object threat level, includes a display and electronics configured to receive mission context data indicating an operational state of the vehicle. The electronics determines a threat level of the object in response to the mission context data. The electronics determines at least one recommended action in response to the threat level. The electronics provides an indication of the threat level and at least one recommended action to the display.

System and method for determining an object threat level

A runway identification system and method utilizes a set of (reflectors or sources). The reflectors or sources can be located in proximity to the end of runway. The method receives electromagnetic energy from the reflectors or sources. A runway identification is determined from the electromagnetic energy. The runway identification can be displayed on a display in the aircraft. The reflectors can be corner reflectors, laser reflectors or other reflective optics.

Runway identification system and method

A present novel and non-trivial system, module, and method for presenting surface symbology on an aircraft display unit are disclosed. Symbology image data representative of an image depicting a runway highlighter adjacent to the assigned runway is generated by a symbology generator based upon assigned runway information and airport surface information provided by a flight management data source and the navigation reference data source, respectively. Such runway highlighter comprises a plurality of runway edge highlighters and a plurality of chevrons pointing in the direction of the assigned runway. The image could include one or more directional runway identifiers. Additionally, the generated image could include the depiction of township location, a line-up distance docking indicator, and/or a groundspeed indicator based upon information provided by a navigation data source. Additionally, the generated image could include the depiction of a wind barb based upon information provided by a weather data source.

System, module, and method for presenting surface symbology on an aircraft display unit

The present example a vertical profile display system with enhanced temporal depiction of navigation information. Such a display, or user interface, may advantageously display information relating to the terrain an aircraft is traveling through based on time ahead of the aircraft to a terrain feature or event, rather than distance to the feature or event. Time to a particular feature may typically be displayed with altitude of the aircraft displayed on the Y-axis. However in alternative examples other types of displays, such as three dimensional displays and the like may be substituted for a two dimensional Cartesian display.

Vertical profile display with enhanced temporal depiction of navigation information

In one aspect, the flight display system comprises a navigation map that includes a time window for a required time of arrival (RTA) waypoint. The time window has a proximal end indicating the aircraft's position at the RTA using a defined lowest speed and a distal end indicating the aircraft's position at the RTA using a defined highest speed. In another aspect, a pop-up time map displays flight plan waypoints mapped out along a time line adjacent to a plurality of time markers. The waypoint scrolls along the time line during flight. In another aspect, the flight display system includes a full format time map for displaying at least one flight plan waypoint mapped out along a time line adjacent to a plurality of time markers. In another broad aspect, a time/bearing map includes a plurality of concentric 'range' rings corresponding to selected times in the future; a plurality of radially spaced bearing ticks positioned at selected locations about the concentric rings; and, a relative time ring presentable about a central axis of, and internal to, the concentric rings. The relative time ring represents a fixed increment in time. Selected waypoints are presentable at their relative bearing to the airplane and at their range (in time) from the airplane.

Growing community of inventors

Cedar Rapids, IA, United States of America

Kirschen A Seah