Runway Presentation Patents (Class 340/972)
  • Patent number: 7813845
    Abstract: A method and system for providing taxiway navigational information to a crewmember of an airplane taxiing at an airport. An airport taxiway navigation system (“ATNS”) that executes on an onboard computer system that displays a map of the taxiways of an airport, receives the name of each taxiway of the taxi route specified by the taxi clearance, and highlights the taxiways on a displayed map to provide a visual indication of the cleared taxi route for the crewmembers.
    Type: Grant
    Filed: February 19, 2003
    Date of Patent: October 12, 2010
    Assignee: The Boeing Company
    Inventors: Reagan Doose, Richard W. Ellerbrock, Glade L. Hulet, John M. Jaugilas, Matthew T. Majka
  • Patent number: 7796055
    Abstract: Systems and methods for runway status indication and related traffic information displays and filtering are disclosed. In one embodiment, the method for displaying runway status includes defining a monitored volume for each of one or more runways, determining a runway status for each of the one or more runways based on at least one of a state of at least one traffic vehicle and a monitoring vehicle state with respect to each monitored volume. The method continues with selecting at least one runway status for display based on the state of the monitoring vehicle. The method then presents the at least one runway status within the monitoring vehicle. In an additional embodiment, each monitored volume is based on a length of a corresponding runway, a width of the corresponding runway, and a predetermined altitude above the corresponding runway.
    Type: Grant
    Filed: November 2, 2006
    Date of Patent: September 14, 2010
    Assignee: The Boeing Company
    Inventors: Samuel T. Clark, Michael P. Snow, Roglenda R. Bowe, Howard F. Au
  • Patent number: 7765037
    Abstract: A method for displaying a runway incursion for an aircraft includes electronically gathering traffic information data from a traffic information system, employing a runway incursion algorithm to the traffic information data to detect a collision hazard, automatically calculating incursion data, and displaying the incursion data. A runway incursion detection system has a display unit, a computer and a software product that enables methodology herein.
    Type: Grant
    Filed: August 19, 2005
    Date of Patent: July 27, 2010
    Assignee: Rockwell Collins, Inc.
    Inventors: Charles J. Bagge, Donald J. Whalen
  • Patent number: 7756637
    Abstract: Methods and systems for a position indicating display system for an aircraft are provided. The system includes a map display unit configured to display a map representative of an area being traversed by the aircraft, and an overlay comprising an own ship depiction, said overlay displayed on the map for a period of time in response to an input from at least one of a user and an aircraft sensor.
    Type: Grant
    Filed: December 21, 2006
    Date of Patent: July 13, 2010
    Assignee: The Boeing Company
    Inventors: Patrick Ralf Wipplinger, Richard William Ellerbrock
  • Patent number: 7755516
    Abstract: A aircraft traffic display system, aircraft including the display system and a method of displaying aircraft and vehicle traffic in the display system. The system includes an ownship location finder determining ownship location and maps, including airport maps stored in map storage. A traffic information collector collecting information on airport and other traffic. A local display displays ownship on a moving map at a selected range and all airport traffic within range, or a filtered subset thereof. An off-scale traffic processor monitors off-scale traffic beyond the selected range and identifies of-interest off-scale traffic. The local display also provides an indication of any of interest off-scale traffic. The indication may visibly indicate status (e.g., air or ground) of respective said off-scale traffic and may include traffic specific information.
    Type: Grant
    Filed: August 20, 2007
    Date of Patent: July 13, 2010
    Assignee: The Boeing Company
    Inventors: Samuel T. Clark, Roglenda R. Bowe, Taji Shafaat, Michael P. Snow
  • Publication number: 20100127896
    Abstract: This invention involves the hardware and system for aiding a pilot in maintaining the desired approach path on VFR during the landing procedure. It is an on-board device comprised of analog parts. Approach path indicator lights or other clues from the ground or air are not necessary. The only requirement is that the pilot see the runway. He can choose and set his own aiming point. The landing by OPAL requires very little, if any, reference to the cockpit's instrument panel. The throttle and control surfaces should be functioning properly. Lights from the pilot's spectacle frame are reflected from a (clear, gravity oriented, pendular, magnetically stabilized) plastic plate to the pilot's eyes. These images are then mentally projected (superimposed) through said plate to the runway at a constant angle. OPAL maintains this angle (approach path) regardless of the attitude of the aircraft. The pilot, by flying, places the lights on the aiming point.
    Type: Application
    Filed: November 21, 2008
    Publication date: May 27, 2010
    Inventor: Bland Hugh Schwarting
  • Publication number: 20100127895
    Abstract: A method of visually presenting aviation obstacles to an operator of an aircraft is disclosed. The method comprises receiving departure information associated with a runway having a departure end, parsing the departure information to determine a presence of an obstacle associated with the runway, determining a location of the obstacle relative to the departure end of the runway, and displaying a graphical representation of the runway and a graphical representation of the obstacle in the location relative to the departure end of the runway.
    Type: Application
    Filed: November 24, 2008
    Publication date: May 27, 2010
    Applicant: Honeywell International Inc.
    Inventors: Blake Wilson, Roger W. Burgin, Aaron Gannon, Dave Pepitone
  • Patent number: 7715955
    Abstract: An aircraft piloting system may include information sources that provide a position indication relating to the aircraft and information that characterizes a virtual approach axis. An information processing unit processes information emanating from the information sources and includes an assisted approach mode function and a landing aid multimode receiver that implements a precision approach. A user device uses the information provided by the landing aid multimode receiver to support the guidance of the aircraft up to its landing.
    Type: Grant
    Filed: March 18, 2004
    Date of Patent: May 11, 2010
    Assignee: Airbus France
    Inventors: Gilles Tatham, Eric Peyrucain
  • Publication number: 20100097241
    Abstract: An apparatus and method for displaying photo realistic features (230, 232, 234) on a display (116) of an aircraft (218) include storing (302) a plurality of photo realistic features (230, 232, 234), the photo realistic features including at least one of terrain (230) and obstacle (232) features. A priority factor is determined (304) that is based on one of, for example, aircraft type, speed, and altitude, and a plurality of display state is prioritized (304) for each of the plurality of photo realistic features (230. 232, 234) in accordance with the priority factor. One of the first and second display states is displayed (308) for each of the plurality of photo realistic features (230, 232, 234) as determined by the prioritizing step (306).
    Type: Application
    Filed: October 20, 2008
    Publication date: April 22, 2010
    Applicant: Honeywell International Inc.
    Inventor: John G. Suddreth
  • Patent number: 7689326
    Abstract: A method of providing heading awareness on a flight display is provided. The method comprises displaying a heading awareness symbology to indicate heading relative to track, and varying the prominence of the heading awareness symbology on a display element based on at least one sensed condition.
    Type: Grant
    Filed: February 2, 2006
    Date of Patent: March 30, 2010
    Assignee: Honeywell International Inc.
    Inventor: Gang He
  • Publication number: 20100039294
    Abstract: A system for detecting a landing area or runway for an aircraft includes a detection subsystem, a processor architecture, flight deck instrumentation, and a runway feature template database. The system is operated to perform an automated method for visually confirming the presence of a runway on approach. The method obtains sensor data indicative of an approach area of the aircraft, and extracts visually distinguishable features of the approach area from the sensor data. The method also accesses the runway feature template corresponding to the intended approach runway for the aircraft, fits the visually distinguishable features to the runway feature template, and provides flight crew feedback in response to the fitting step.
    Type: Application
    Filed: August 14, 2008
    Publication date: February 18, 2010
    Applicant: Honeywell International Inc.
    Inventors: Thea L. Feyereisen, Ivan S. Wyatt, Gang He
  • Publication number: 20100026525
    Abstract: An aircraft synthetic vision system (100) is provided for increasing data input to a pilot (109) during approach and landing flight operations, and includes a runway assistance landing system (114) and a plurality of databases (106, 108, 110, 112) which may include, for example, a terrain database (106), an obstacle database (112); and a validated runway database (110). The processor (104) detects the likelihood of an error in determining the altitude from at least one of the runway assistance landing system (114), the plurality of databases (106, 108, 110, 112), and identifies the error. The processor (104) further determines augmented coordinates, and a processor (104) generates symbology commands to a first display (116) for displaying a runway environment in response to data provided to the processor (104) from each of the runway assistance landing system (114), the plurality of databases (106, 108, 110, 112), and the processor (104).
    Type: Application
    Filed: July 31, 2008
    Publication date: February 4, 2010
    Applicant: Honeywell International Inc.
    Inventors: Thea L. Feyereisen, Ivan Sandy Wyatt, Gang He
  • Patent number: 7623044
    Abstract: According to an example embodiment, a method includes receiving data about an aircraft that is moving on a surface using at least a first wheel, the data descriptive of physical characteristics of the aircraft, calculating a first path of the first wheel along the surface using the data, and displaying the first path in relation to a boundary between a first area of the surface and a second area of the surface, the first area safe for the aircraft, the second area unsafe for the aircraft.
    Type: Grant
    Filed: November 30, 2006
    Date of Patent: November 24, 2009
    Assignee: Honeywell International Inc.
    Inventors: David Pepitone, Gang He
  • Publication number: 20090265090
    Abstract: A device, method and computer program product for locating aircraft with respect to airport runways and taxiways, determining if a conflict exists between an aircraft having operating the invention and another aircraft, and generating and annunciating conflict awareness advisories as a function of determining that a conflict exists.
    Type: Application
    Filed: June 25, 2009
    Publication date: October 22, 2009
    Applicant: Honeywell International Inc.
    Inventors: John J. Poe, Scott R. Gremmert, Kevin J. Conner
  • Patent number: 7605774
    Abstract: A head-up display (HUD) system for an aircraft is disclosed. The HUD comprises a computer receiving information representative of an aircraft flight path. The HUD also comprises a head-up display unit comprising a projector and a combiner. The combiner receives an image from the projector. An imaging sensor is coupled to the computer. The imaging sensor has a pointing direction and a field of view. A region of special processing is defined within the imaging sensor field of view. A program is running on the computer. The program determines an offset for the region of special processing. The offset is based on the aircraft flight path and the imaging sensor pointing direction. The offset is used in the computer to cause display region of special processing to be moved based on the direction of the aircraft flight path.
    Type: Grant
    Filed: July 2, 2004
    Date of Patent: October 20, 2009
    Assignee: Rockwell Collins, Inc.
    Inventors: Lawrence C. Brandt, Robert B. Wood
  • Patent number: 7605688
    Abstract: A vehicle location determination system including a radio frequency identification (RFID) interrogator system positioned on a vehicle; and, a plurality of passive RFID tags positioned in an environment proximate to an intended path of the vehicle. The RFID interrogator system provides the capability of having the vehicle determine its location in the proximate environment based on the interrogation of the passive RFID tags. The present invention is particularly adaptable for use in an airport environment. It is not reliant on any type of ground based interrogation system. Instead, the airport surface movement area (i.e. taxiways, runways, ramps and gates) is only required to have a system of passive RFID tags.
    Type: Grant
    Filed: May 19, 2006
    Date of Patent: October 20, 2009
    Assignee: Rockwell Collins, Inc.
    Inventor: Kirschen A. Seah
  • Patent number: 7589644
    Abstract: The invention relates to a method to help a person responsible for a vehicle on an airport to follow running procedures in the airport, the vehicle including a device for using the method, including: a database including: data modelling all or some of an airport environment; one or several acquisition devices for acquiring procedures applicable to the running operation on the airport; one or several devices configured to acquire and determine vehicle status information; calculation means using the database; graphic transcription means and warning means; means of generating sound and visual alarms; wherein the assistance method includes at least the following steps: determine applicable procedures; continuously calculate deviations between the behaviour of the vehicle and applicable procedures; graphic transcription of progress of the vehicle while running and deviations from applicable procedures; trigger visual and/or sound alerts when a predetermined deviation threshold is crossed.
    Type: Grant
    Filed: September 29, 2006
    Date of Patent: September 15, 2009
    Assignee: Thales
    Inventor: Hugues Meunier
  • Patent number: 7564372
    Abstract: A head-up display (HUD) is disclosed. The HUD is provided on board an aircraft. The HUD comprises a projector and a combiner. The combiner enables viewing of the world outside of the combiner and also allows viewing of information provided from the projector. A computer is coupled to the projector and provides airport runway and taxiway symbols conformally mapped onto the combiner. Also provided on the combiner is a mapping of hold lines onto the combiner.
    Type: Grant
    Filed: June 30, 2004
    Date of Patent: July 21, 2009
    Assignee: Rockwell Collins, Inc.
    Inventors: Gary C. Bailey, Kenneth A. Zimmerman, Louis J. Bailey, Robert A. Armstrong, John G. Wilson
  • Patent number: 7522977
    Abstract: A method for landing an aircraft includes determining the aircraft's deviation from its approach path so as to define a first point of the aircraft's heading. A first straight line passing through the first point and through a second point defining the ground orientation of the approach path is displayed, by a head-up display, on a horizon line with a heading scale. The first straight line represents a ground plot of the approach path. A first assistance gate is displayed such that the first straight line passes through the first assistance gate when the aircraft is aligned on the approach path. A second straight line, parallel with the horizon line and passing through the first point, is displayed and represents a plot on the ground of the origin of the approach path. A second assistance gate is displayed under the horizon line and represents the slope of the approach path.
    Type: Grant
    Filed: March 31, 2006
    Date of Patent: April 21, 2009
    Assignee: AIRBUS France
    Inventors: Vincent Foucart, Eric Albert, Patrice Gonzalez
  • Patent number: 7508322
    Abstract: A current path display indicator for a display device of a vehicle. The current path display indicator includes a flight path indicator (FPI) and a visual cue associated with the FPI to indicate relative direction from the vehicle's current path to a desired path. The visual cue may be embodied in possibly a number of different ways. For example, it may be embodied as an arrow extending from a circular portion of the FPI; a highlighted segment superimposed on the circular portion of the FPI; a triangle extending from the circular portion; or, a pie-shaped marker contained within the circular portion.
    Type: Grant
    Filed: March 3, 2006
    Date of Patent: March 24, 2009
    Assignee: Rockwell Collins, Inc.
    Inventors: Michael J. Krenz, Arlen E. Breiholz, Matthew J. Carrico, Kenneth W. Mc Elreath
  • Patent number: 7499795
    Abstract: Method and device for assisting in the navigation of an airplane on the ground at an airport. The device (1) comprises means (14) for transmitting an alarm signal, at least if an airplane position is not on a routing zone of the airport or if the orientation bearing-wise of the airplane on this routing zone does not correspond to a particular traffic direction.
    Type: Grant
    Filed: June 6, 2007
    Date of Patent: March 3, 2009
    Assignee: AIRBUS France
    Inventors: Fabien Fetzmann, Pierre Coldefy, Stéphane Collins
  • Publication number: 20090045982
    Abstract: The general field of the invention is that of systems for aiding the guidance of an aircraft on an airport. The system according to the invention comprises means for determining at least one element of the topology of the airport in relation to the position of the aircraft for selecting. Selecting means are provided by the pilot of the aircraft for the element. Generating means are provided to generate at least one guidance or safety set-point using the topological element. Presenting means are provided for the element or the associated set-point on a man-machine interface to the pilot of the aircraft.
    Type: Application
    Filed: June 6, 2008
    Publication date: February 19, 2009
    Applicant: THALES
    Inventors: Christophe Caillaud, Guy Deker, Nicolas Marty
  • Patent number: 7493196
    Abstract: This onboard flight management system displays on the navigation screen the plots of the flight plan parts corresponding to the navigation procedures whose names are displayed on the MCD console during the introduction by the crew of the aircraft, by means of the MCD console, of the elements allowing the FMS flight management computer to plot a flight plan. This facilitates the task of the crew when choosing navigation procedure since the plot of the flight plan part corresponding to a navigation procedure is much more expressive than the name of the procedure.
    Type: Grant
    Filed: February 20, 2004
    Date of Patent: February 17, 2009
    Assignee: Thales
    Inventors: Christophe Caillaud, Vincent Jacquier
  • Publication number: 20080234882
    Abstract: Method and device to assist in the piloting of an aircraft in a landing phase. The device (1) comprises means (12) for applying a maximum braking of the aircraft if there is a risk of longitudinal departure from a runway, on a landing.
    Type: Application
    Filed: March 19, 2008
    Publication date: September 25, 2008
    Applicants: AIRBUS France, AIRBUS
    Inventors: Fabrice VILLAUME, Armand Jacob, Robert Lignee
  • Publication number: 20080211692
    Abstract: The invention concerns a system (1) comprising means (2) for determining the current position of the aircraft, a display device (4) displaying, on a viewing screen (7) an airport map, wherewith is associated a symbol illustrating the current position of the aircraft, an interface means (8) enabling the display of the display device (4) to be operated by an operator, storage means (10) storing a plurality of airport maps, means (12) for determining a reference point for each airport, whereof the map is stored in the storage means (10), and a selecting device (13) which selects an airport map stored in the storage means (8) so as to transmit same to the display device (4) so that it can be displayed, and which comprises means (14) enabling an airport map to be automatically selected, based on the current position of the aircraft and as airport reference point.
    Type: Application
    Filed: July 13, 2006
    Publication date: September 4, 2008
    Applicant: AIRBUS France
    Inventors: Fabien Fetzmann, Pierre Coldefy, Thierry Malaval
  • Publication number: 20080186207
    Abstract: The invention relates to a device (1) comprising a set (2) of information sources for determining the active values of a plurality of parameter of an aeroplane, calculating means (3) for determining, by means of said active values, a first position corresponding to a position which is extrapolated from the nose of the aeroplane following a particular time interval from the current instant. The inventive device also comprises a database (5) provided with at least one pre-determined unauthorized zone of the airport, comparison means (6) for comparing said first position to said pre-determined unauthorized zone of the airport, and warning means (9) for emitting at least one warning signal if the first position is located in the unauthorized zone.
    Type: Application
    Filed: March 29, 2006
    Publication date: August 7, 2008
    Applicant: AIRBUS GRANCE
    Inventors: Fabien Fetzmann, Pierre Coldefy, Stephane Collins
  • Patent number: 7382284
    Abstract: The present invention is a method and system of aircraft surface operations guidance on a head up display. An aircraft surface operations guidance method includes the following steps. At time t1, a taxi guidance cue and a trend vector are displayed on a head up display of an aircraft. The taxi guidance cue represents a desired position of an aircraft control point of the aircraft at time t2. The trend vector represents a predicted path of the aircraft control point from time t1 to time t2 based on a state of the aircraft at time t1. The trend vector includes a tip representing a predicted position of the aircraft control point at time t2. The tip is maintained within the taxi guidance cue so that the aircraft control point may reach the desired position at time t2.
    Type: Grant
    Filed: September 29, 2004
    Date of Patent: June 3, 2008
    Assignee: Rockwell Collins, Inc.
    Inventors: Robert A. Armstrong, John G. Wilson, Kenneth A. Zimmerman, Gary C. Bailey, Louis J. Bailey
  • Patent number: 7382287
    Abstract: A destination runway selection method, system and apparatus for use with a Terrain Awareness and Warning System (“TAWS”). The method involves determining upon which of a number of candidate runways an aircraft is most likely to land so that appropriate Required Terrain Clearance (“RTC”) values and other alert thresholds may be referenced. According to a first aspect of the method, a destination airport is initially selected from among candidate airports. According to a second aspect of the method, a destination runway is selected from among the candidate runways at the destination airport. In one particular embodiment of the invention, the candidate runway is selected solely on the basis of distance calculations between the runway and the aircraft.
    Type: Grant
    Filed: June 3, 2003
    Date of Patent: June 3, 2008
    Assignee: Garmin International, Inc
    Inventors: Susan S. Chen, Clayton E. Barber
  • Patent number: 7382288
    Abstract: A head-up display (HUD) is disclosed. The HUD is provided on board an aircraft. The HUD comprises a projector and a combiner. The combiner enables viewing of the world outside of the combiner and also allows viewing of information provided from the projector. A computer is coupled to the projector and provides airport runway and taxiway symbols conformally mapped onto the combiner. Also provided on the combiner is a mapping of virtual airport signs onto the combiner.
    Type: Grant
    Filed: June 30, 2004
    Date of Patent: June 3, 2008
    Assignee: Rockwell Collins, Inc.
    Inventors: John G. Wilson, Kenneth A. Zimmerman, Gary C. Bailey, Robert A. Armstrong, Louis J. Bailey
  • Publication number: 20080106438
    Abstract: Systems and methods for runway status indication and related traffic information displays and filtering are disclosed. In one embodiment, the method for displaying runway status includes defining a monitored volume for each of one or more runways, determining a runway status for each of the one or more runways based on at least one of a state of at least one traffic vehicle and a monitoring vehicle state with respect to each monitored volume. The method continues with selecting at least one runway status for display based on the state of the monitoring vehicle. The method then presents the at least one runway status within the monitoring vehicle. In an additional embodiment, each monitored volume is based on a length of a corresponding runway, a width of the corresponding runway, and a predetermined altitude above the corresponding runway.
    Type: Application
    Filed: November 2, 2006
    Publication date: May 8, 2008
    Applicant: THE BOEING COMPANY
    Inventors: Samuel T. Clark, Michael P. Snow, Roglenda R. Bowe, Howard F. Au
  • Patent number: 7342514
    Abstract: A head-up display (HUD) is disclosed. The HUD is provided on board an aircraft. The HUD comprises a projector and a combiner. The combiner enables viewing of the world outside of the combiner and also allows viewing of information provided from the projector. A computer is coupled to the projector and provides airport runway and taxiway symbols conformally mapped onto the combiner. Also provided on the combiner is a mapping of automatic dependent surveillance broadcast advisory information and traffic onto the combiner.
    Type: Grant
    Filed: June 30, 2004
    Date of Patent: March 11, 2008
    Assignee: Rockwell Collins, Inc.
    Inventors: Louis J. Bailey, John G. Wilson, Gary C. Bailey, Kenneth A. Zimmerman, Robert A. Armstrong
  • Patent number: 7253748
    Abstract: A system for detection of foreign objects on airport travel surfaces including a plurality of foreign object detector modules mounted on a corresponding plurality of existing aircraft travel surface lighting supports, the plurality of foreign object detector modules providing a corresponding plurality of detection outputs and a high speed detection output analyzer operative to receive at least one of the plurality of detection outputs and to provide a high speed output indication of foreign object presence.
    Type: Grant
    Filed: June 6, 2005
    Date of Patent: August 7, 2007
    Assignee: Xsight Systems Ltd
    Inventors: Alon Nitzan, Aviv Goner, Aviram Golan, Moshe Fisher
  • Patent number: 7222017
    Abstract: A system and method are provided for the efficient entry and display of ground taxi routes on an electronic airport map display. The system may include a touchscreen entry device, a display device, a computer, a map database, a vehicle position sensor and a transmitter/receiver. The system may be configured to check the ground taxi entries to ensure that each successive segment is contiguous with the last or next segment, and any gaps or discontinuities in the displayed taxi instructions may be annunciated. An intelligent display of next possible segments may be incorporated into the system.
    Type: Grant
    Filed: June 17, 2004
    Date of Patent: May 22, 2007
    Assignee: The Boeing Company
    Inventors: Samuel T. Clark, Wayne R. Jones, Michael P. Snow, Eddie J. Trujillo
  • Patent number: 7216069
    Abstract: An apparatus and method for simulating airport lighting aids by providing a generator having a processor structured to receive a plurality of navigation signals representative of position and altitude of a host aircraft; a signal generator operated by the processor, the generator being structured to retrieve airport information from a database as a function of the position signal, compare the position and altitude signals with a glide path, and output a signal representative of a degree of coincidence with the glide path as a function of the position and altitude signals; and a plurality of indicators structured to receive the signal output by the signal generator and responsively output a visual indication of the degree of coincidence with the glide path.
    Type: Grant
    Filed: January 17, 2002
    Date of Patent: May 8, 2007
    Assignee: Honeywell International, Inc.
    Inventor: Charles L. Hett
  • Patent number: 7209053
    Abstract: An improved system and method are disclosed for indicating the validity of airport runway visual approach slope indicators on an aircraft display. An aircraft display system is provided, which includes a database for storing data about the specific visual approach slope lighting indicator system being used by each airport of a plurality of airports and any special distance and/or usage limitations associated with each such visual approach slope indicator system, a processing unit, a position determination unit, and a visual display. As an aircraft approaches an airport, the processing unit receives the aircraft's current position from the position determination unit, and compares the aircraft's current position data with the distance and/or usage limitation data stored in the database for the approach slope indicator system being used by that airport.
    Type: Grant
    Filed: April 6, 2005
    Date of Patent: April 24, 2007
    Assignee: Honeywell International Inc.
    Inventor: Aaron J. Gannon
  • Patent number: 7161501
    Abstract: Method and system for analyzing and displaying one or more present flight parameter values FP(t) of an aircraft in motion at a measurement time tn, and for comparing the present flight parameter value with a selected percentage band, containing historical flight parameter data for similar conditions.
    Type: Grant
    Filed: February 22, 2005
    Date of Patent: January 9, 2007
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Robert E. Lynch, Robert E. Lawrence, Thomas R. Chidester, Brett G. Amidan, Gary L. Prothero, Timothy P. Romanowski
  • Patent number: 7132960
    Abstract: A system, method, and computer program product are provided for monitoring for high energy landing approaches and advising a flight crew of an aircraft. Specific aircraft energy is predicted at a touchdown zone of a runway. The predicted specific energy is compared with predetermined threshold specific energy. An alert is generated when the predicted specific energy is at least the predetermined threshold specific energy. The present invention improves flight crew awareness of an impending problem with a landing approach, such as a high energy approach, provides an advisory when probability of an unsuccessful approach is significant, and allows a margin from stable approach criteria while avoiding increased aural and visual clutter in the flight deck.
    Type: Grant
    Filed: October 7, 2003
    Date of Patent: November 7, 2006
    Assignee: Honeywell International Inc.
    Inventor: John H. Glover
  • Patent number: 7109889
    Abstract: A method for enhancing ground situational awareness to an aircraft operating at an airport is described. The method includes displaying, within the aircraft, runways and taxiways for the airport and displaying a position of the aircraft with respect to the runways and taxiway. A resolution of at least one of a runway, a taxiway, and an aircraft position is based on at least one of a selected resolution, a position and heading of the aircraft, a taxi speed, and a ground speed of the aircraft.
    Type: Grant
    Filed: March 1, 2004
    Date of Patent: September 19, 2006
    Assignee: Honeywell International Inc.
    Inventor: Gang He
  • Patent number: 7084785
    Abstract: The method provides for determining an approach mode which has been selected by the pilot of the aircraft from among a plurality of predetermined approach modes, for selecting a characteristic segment (6) of an arrival path which relates to the selected approach mode thus determined, for determining the orientation of the projection on the ground of the said characteristic segment (6) with respect to the center line of the said runway (5) and, depending on this orientation, for determining an anchoring point of the said final approach path, the orientation (?) in a horizontal plane of the said final approach path and the slope (?) of the said final approach path.
    Type: Grant
    Filed: February 11, 2004
    Date of Patent: August 1, 2006
    Assignee: Airbus France
    Inventors: Patrice Rouquette, Olivier Coussat
  • Patent number: 7079951
    Abstract: A method and system for locating aircraft with respect to airport runways selecting as a function of aircraft state parameters one of a plurality of candidate runways that the aircraft on which it is installed is most likely to encounter, whether taxiing, preparing for take-off, or approaching to land.
    Type: Grant
    Filed: December 10, 2004
    Date of Patent: July 18, 2006
    Assignee: Honeywell International Inc.
    Inventors: Kevin J. Conner, Scott R. Gremmert, Yasuo Ishihara, Ratan Khatwa, John J. Poe, James J. Corcoran, III
  • Patent number: 6983206
    Abstract: A method for locating aircraft with respect to airport runways and taxiways, generating and annunciating situational awareness advisories as a function of aircraft state parameters relative to a determination of the aircraft location.
    Type: Grant
    Filed: May 15, 2003
    Date of Patent: January 3, 2006
    Assignee: Honeywell International, Inc.
    Inventors: Kevin J Conner, Scott R. Gremmert, Yasuo Ishihara, Ratan Khatwa, John J. Poe, James J. Corcoran, III
  • Patent number: 6972696
    Abstract: A programmable symbology is provided that defines a series of geometric forms in the visual field of a pilot. The symbology includes a virtual representation of a predicted flight path of the aircraft and a virtual representation of a projected contact point with an external object, including the ground. The symbology also provides a virtual representation of a predicted flight path of the aircraft that is projected onto the ground below the projected flight path as a ground path predictor. The symbology further provides a critical slowing air speed indicator.
    Type: Grant
    Filed: March 22, 2003
    Date of Patent: December 6, 2005
    Inventors: Steven P. Rogers, Charles N. Asbury
  • Patent number: 6927701
    Abstract: Techniques are described for monitoring runway occupancy and providing an indication of occupancy of a runway to an airplane on final approach the runway. A system, for example, defines and monitors one or more zones on the runway to determine whether the runway is occupied. Such a system includes sensors, such as inductive loop sensors, that may be located proximate to or on the runway, and the system may monitor ingress and egress of objects, such as airplanes or other vehicles on the ground, into and out of the zone in order to determine whether the zone is activated. The sensors may be located at points of entry and exit for the zone. The zones may be located at take-off hold areas of the runway and intersections of the runway with taxiways. A ground-based approach light array of the system may provide the indication of runway occupancy to the airplane.
    Type: Grant
    Filed: January 29, 2003
    Date of Patent: August 9, 2005
    Assignee: Architecture Technology Corporation
    Inventors: Noel E Schmidt, Kirk J Swanson, Eric R Chartier
  • Patent number: 6917309
    Abstract: A system for detection of foreign objects on airport travel surfaces including a plurality of foreign object detector modules mounted on a corresponding plurality of existing aircraft travel surface lighting supports, the plurality of foreign object detector modules providing a corresponding plurality of detection outputs and a high speed detection output analyzer operative to receive at least one of the plurality of detection outputs and to provide a high speed output indication of foreign object presence.
    Type: Grant
    Filed: October 28, 2002
    Date of Patent: July 12, 2005
    Assignee: Integritech System Engineering Ltd.
    Inventors: Alon Nitzan, Aviv Goner, Aviram Golan, Moshe Fisher
  • Patent number: 6862519
    Abstract: An airport map display system for an aircraft displays the airport paved surfaces and structures to a pilot or crew member. The system displays runways, taxiways, connectors, ramps, gates, and buildings. Hold and yield points may also be displayed. A compact set of specific data points and associated pavement width values is used to store unique data for each airport.
    Type: Grant
    Filed: February 20, 2002
    Date of Patent: March 1, 2005
    Assignee: Smiths Aerospace, Inc.
    Inventor: Randy L. Walter
  • Publication number: 20040183698
    Abstract: The method provides for determining an approach mode which has been selected by the pilot of the aircraft from among a plurality of predetermined approach modes, for selecting a characteristic segment (6) of an arrival path which relates to the selected approach mode thus determined, for determining the orientation of the projection on the ground of the said characteristic segment (6) with respect to the center line of the said runway (5) and, depending on this orientation, for determining an anchoring point of the said final approach path, the orientation (&agr;) in a horizontal plane of the said final approach path and the slope (&bgr;) of the said final approach path.
    Type: Application
    Filed: February 11, 2004
    Publication date: September 23, 2004
    Applicant: Airbus France
    Inventors: Patrice Rouquette, Olivier Coussat
  • Publication number: 20040167685
    Abstract: A critical point on a runway indicates a point at which an aircraft may experience a runway overrun if landing beyond the critical point. A path projection is extended from the aircraft at a descent slope angle to determine whether the aircraft will land beyond the critical point at the current descent slope. Timely alerts may be provided by accounting for the time required to announce a distance value, and the distance traveled during the announcement.
    Type: Application
    Filed: May 21, 2003
    Publication date: August 26, 2004
    Inventors: Dean E. Ryan, William C. Brodegard
  • Patent number: 6751545
    Abstract: A taxi planning system for aircraft provides an intuitive user interface for entering and selecting taxi plans quickly and easily. The system includes predefined reduced selection menus that prompt the pilot with feasible taxi choices. Predefined standard routes allow the pilot to select a taxi route with a minimum of keystrokes and in a minimum of time. A display screen communicates the selection menus and standard routes to the pilot who makes a selection with as little as one keystroke. A database comprising a linked list structure facilitates a flexible system that is able to represent a wide variety of airport runways, taxiways, gates, ramps, and other airport structures. The selected taxi route is communicated to other aircraft systems such as head-down displays, head-up displays, flight management computers, communication systems, and the like.
    Type: Grant
    Filed: February 20, 2002
    Date of Patent: June 15, 2004
    Assignee: Smiths Aerospace, Inc.
    Inventor: Randy L. Walter
  • Patent number: 6731226
    Abstract: An airport feature display system for aircraft provides visual guidance cues and awareness to track the specified taxi path on a HUD. The guidance cues include symbology representative of the position of selected airport features such as runway and taxiway edges, taxi routes, and airport signage. Data representative of the airport features is communicated between aircraft systems using a data interchange method that facilitates efficient throughput of the large quantities of data required to represent the airport features.
    Type: Grant
    Filed: February 20, 2002
    Date of Patent: May 4, 2004
    Assignee: Smiths Aerospace, Inc.
    Inventor: Randy L. Walter
  • Patent number: RE41396
    Abstract: A system and method are provided for the efficient entry and display of ground taxi routes on an electronic airport map display. The system may include a touchscreen entry device, a display device, a computer, a map database, a vehicle position sensor and a transmitter/receiver. The system may be configured to check the ground taxi entries to ensure that each successive segment is contiguous with the last or next segment, and any gaps or discontinuities in the displayed taxi instructions may be annunciated. An intelligent display of next possible segments may be incorporated into the system.
    Type: Grant
    Filed: June 13, 2008
    Date of Patent: June 22, 2010
    Assignee: The Boeing Company
    Inventors: Samuel T. Clark, Wayne R. Jones, Michael P. Snow, Eddie J. Trujillo