Patents by Inventor Gerald J. Block

Gerald J. Block has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • Publication number: 20120203997
    Abstract: Systems and methods are described here to provide a degree or level of certification to a resident application such as an operating system, e.g., Linux®. In a Linux® implementation, the operating system provides a robust environment including many seasoned communication stacks, e.g., TCP/IP, USB, and the like. However, Linux® is not certified to the level necessary to be a part of many avionics applications. To eliminate the need to certify all of such an operating system, such certification being highly costly, the avionics application itself may be protected so that the operating system cannot alter the application's operating environment, e.g., application code and data, once the application is loaded and running. In this case, only the application requires certification at the highest level, and not the operating system such as Linux®.
    Type: Application
    Filed: February 6, 2012
    Publication date: August 9, 2012
    Applicant: SANDEL AVIONICS, INC.
    Inventor: Gerald J. Block
  • Patent number: 8111920
    Abstract: Systems and methods for operating an avionics component to a level of certification. Steps include: receiving and sending data to a data monitor and an integrity monitor, the data monitor operating at a first level of certification and the integrity monitor operating at a second higher level; using the integrity monitor, determining where a feature of the data should appear on a display; checking if the feature properly appears, and if not, an error condition appears. The system includes: a sensor for sensing an aircraft condition; a data monitor for receiving and rendering data from the sensor, the data monitor certified to a first category level; an integrity monitor for receiving the data from the sensor and for calculating where a feature of the data should appear on a data display, the integrity monitor certified to a second higher level. If the feature does not properly appear, an error condition appears.
    Type: Grant
    Filed: October 15, 2007
    Date of Patent: February 7, 2012
    Assignee: Sandel Avionics, Inc.
    Inventors: Gerald J. Block, Delmar M. Fadden
  • Publication number: 20120004793
    Abstract: An aircraft hover system for enabling an aircraft to hover at a target spatial location represented by GPS location coordinates. The hover system includes a display screen rendering a display including live video feed of the terrain below the airborne aircraft, a first mark overlaying the video feed, the first mark representing the current position of the aircraft relative to the terrain, and a perimeter surrounding the first mark, the portion of the terrain within the perimeter being substantially magnified compared to that of the terrain outside of the perimeter. The hover system is configured such that, as the aircraft approaches the target spatial location, the distance between the first mark and a second mark on the display gradually decreases until and finally the first and second marks coincide; the second mark representing the target spatial location.
    Type: Application
    Filed: July 5, 2011
    Publication date: January 5, 2012
    Applicant: SANDEL AVIONICS, INC.
    Inventor: Gerald J. Block
  • Publication number: 20110276201
    Abstract: An aircraft terrain awareness warning system is disclosed that includes an interface for entering flight plan details of an aircraft including at least one waypoint. The terrain awareness warning system is configured such that potential-terrain-collision alerts are suppressed in the aircraft during landing operations performed at waypoints associated with landing zones.
    Type: Application
    Filed: April 8, 2011
    Publication date: November 10, 2011
    Applicant: SANDEL AVIONICS, INC.
    Inventor: Gerald J. Block
  • Patent number: 7187304
    Abstract: A display system for an airplane or other vehicle is disclosed. A rear projection LCD is used to allow for a maximum amount of screen area to be used in displaying operator pertinent data.
    Type: Grant
    Filed: December 5, 2005
    Date of Patent: March 6, 2007
    Assignee: Spendel Avionics LLC
    Inventor: Gerald J. Block
  • Patent number: 7057549
    Abstract: Embodiments of the invention provide a method and apparatus for indicating aircraft height relative to an obstruction in a terrain awareness warning system. The method includes receiving data indicative of geographic features of an obstruction, lateral distance of the geographic feature from an aircraft, height and flight path of the aircraft, calculating a projected height of the aircraft at the location of the obstruction using the data, generating a result signal, and displaying a colored indication on a display screen based on the result signal. The apparatus includes inputs for signals from instruments measuring height, flight path, and location of an aircraft, as well as an input for an instrument providing information about geographic features of terrain surrounding the aircraft. The apparatus includes a means for employing the signals to calculate an effective height of the aircraft relative to the terrain, and a screen display for graphically displaying the results of the calculation.
    Type: Grant
    Filed: March 9, 2005
    Date of Patent: June 6, 2006
    Assignee: Sandel Avionics, Inc.
    Inventor: Gerald J. Block
  • Patent number: 6999023
    Abstract: Embodiments of the invention provide a method and apparatus for indicating aircraft height relative to an obstruction in a terrain awareness warning system. The method includes receiving data indicative of geographic features of an obstruction, lateral distance of the geographic feature from an aircraft, height and flight path of the aircraft, calculating a projected height of the aircraft at the location of the obstruction using the data, generating a result signal, and displaying a colored indication on a display screen based on the result signal. The apparatus includes inputs for signals from instruments measuring height, flight path, and location of an aircraft, as well as an input for an instrument providing information about geographic features of terrain surrounding the aircraft. The apparatus includes a means for employing the signals to calculate an effective height of the aircraft relative to the terrain, and a screen display for graphically displaying the results of the calculation.
    Type: Grant
    Filed: November 3, 2003
    Date of Patent: February 14, 2006
    Inventor: Gerald J. Block
  • Patent number: 6972695
    Abstract: A display system for an airplane or other vehicle is disclosed. A rear projection LCD is used to allow for a maximum amount of screen area to be used in displaying operator pertinent data.
    Type: Grant
    Filed: January 20, 2004
    Date of Patent: December 6, 2005
    Assignee: Sandel Avionics LLC
    Inventor: Gerald J. Block
  • Patent number: 6889124
    Abstract: A system for reducing nuisance alerts and warnings in a terrain awareness and warning system for an aircraft, including determining if the aircraft is within a predetermined geometric volume surrounding an airport. If the aircraft is within the geometric volume, then determining the aircraft's current projected flight path for a selected distance or time and comparing it with at least one approach volume extending from a runway at the airport towards an outer boundary of the geometric volume. If the aircraft's current projected flight path is such that the aircraft is expected to be within the approach volume and stay within the approach volume to the runway, then inhibiting selected alerts and warnings associated with non-threatening terrain.
    Type: Grant
    Filed: March 18, 2003
    Date of Patent: May 3, 2005
    Inventors: Gerald J. Block, Albert J. Bourdon
  • Patent number: 6750788
    Abstract: A display system for an airplane or other vehicle is disclosed. A rear projection LCD is used to allow for a maximum amount of screen area to be used in displaying operator pertinent data.
    Type: Grant
    Filed: May 22, 2001
    Date of Patent: June 15, 2004
    Assignee: Sandel Avionics, Inc.
    Inventor: Gerald J. Block
  • Publication number: 20040093131
    Abstract: A system for reducing nuisance alerts and warnings in a terrain awareness and warning system for an aircraft, including determining if the aircraft is within a predetermined geometric volume surrounding an airport. If the aircraft is within the geometric volume, then determining the aircraft's current projected flight path for a selected distance or time and comparing it with at least one approach volume extending from a runway at the airport towards an outer boundary of the geometric volume. If the aircraft's current projected flight path is such that the aircraft is expected to be within the approach volume and stay within the approach volume to the runway, then inhibiting selected alerts and warnings associated with non-threatening terrain.
    Type: Application
    Filed: March 18, 2003
    Publication date: May 13, 2004
    Inventors: Gerald J. Block, Albert J. Bourdon
  • Patent number: 6683556
    Abstract: Embodiments of the invention provide a method and apparatus for indicating aircraft height relative to an obstruction in a terrain awareness warning system. The method includes receiving data indicative of geographic features of an obstruction, lateral distance of the geographic feature from an aircraft, height and flight path of the aircraft, calculating a projected height of the aircraft at the location of the obstruction using the data, generating a result signal, and displaying a colored indication on a display screen based on the result signal. The apparatus includes inputs for signals from instruments measuring height, flight path, and location of an aircraft, as well as an input for an instrument providing information about geographic features of terrain surrounding the aircraft. The apparatus includes a means for employing the signals to calculate an effective height of the aircraft relative to the terrain, and a screen display for graphically displaying the results of the calculation.
    Type: Grant
    Filed: November 19, 2002
    Date of Patent: January 27, 2004
    Assignee: Sandel Avionics, Inc.
    Inventor: Gerald J. Block
  • Patent number: 6670892
    Abstract: A display system for an airplane or other vehicle is disclosed. A rear projection LCD is used to allow for a maximum amount of screen area to be used in displaying operator pertinent data.
    Type: Grant
    Filed: May 22, 2001
    Date of Patent: December 30, 2003
    Assignee: Sandel Avionics
    Inventor: Gerald J. Block
  • Publication number: 20030132876
    Abstract: Embodiments of the invention provide a method and apparatus for indicating aircraft height relative to an obstruction in a terrain awareness warning system. The method includes receiving data indicative of geographic features of an obstruction, lateral distance of the geographic feature from an aircraft, height and flight path of the aircraft, calculating a projected height of the aircraft at the location of the obstruction using the data, generating a result signal, and displaying a colored indication on a display screen based on the result signal. The apparatus includes inputs for signals from instruments measuring height, flight path, and location of an aircraft, as well as an input for an instrument providing information about geographic features of terrain surrounding the aircraft. The apparatus includes a means for employing the signals to calculate an effective height of the aircraft relative to the terrain, and a screen display for graphically displaying the results of the calculation.
    Type: Application
    Filed: November 19, 2002
    Publication date: July 17, 2003
    Applicant: Sandel Avionics, Inc.
    Inventor: Gerald J. Block
  • Patent number: 6591170
    Abstract: A system for reducing nuisance alerts and warnings in a terrain awareness and warning system for an aircraft, including determining if the aircraft is within a predetermined geometric volume surrounding an airport. If the aircraft is within the geometric volume, then determining the aircraft's current projected flight path for a selected distance or time and comparing it with at least one approach volume extending from a runway at the airport towards an outer boundary of the geometric volume. If the aircraft's current projected flight path is such that the aircraft is expected to be within the approach volume and stay within the approach volume to the runway, then inhibiting selected alerts and warnings associated with non-threatening terrain.
    Type: Grant
    Filed: October 11, 2001
    Date of Patent: July 8, 2003
    Assignee: Sandel Avionics, Inc.
    Inventors: Gerald J. Block, Albert J. Bourdon
  • Patent number: 6507288
    Abstract: A display system for an airplane or other vehicle is disclosed. A rear projection LCD is used to allow for a maximum amount of screen area to be used in displaying operator pertinent data.
    Type: Grant
    Filed: May 22, 2001
    Date of Patent: January 14, 2003
    Assignee: Sandel Avionics, Inc.
    Inventor: Gerald J. Block
  • Patent number: 6489916
    Abstract: Embodiments of the invention provide a method and apparatus for indicating aircraft height relative to an obstruction in a terrain awareness warning system. The method includes receiving data indicative of geographic features of an obstruction, lateral distance of the geographic feature from an aircraft, height and flight path of the aircraft, calculating a projected height of the aircraft at the location of the obstruction using the data, generating a result signal, and displaying a colored indication on a display screen based on the result signal. The apparatus includes inputs for signals from instruments measuring height, flight path, and location of an aircraft, as well as an input for an instrument providing information about geographic features of terrain surrounding the aircraft. The apparatus includes a means for employing the signals to calculate an effective height of the aircraft relative to the terrain, and a screen display for graphically displaying the results of the calculation.
    Type: Grant
    Filed: October 11, 2001
    Date of Patent: December 3, 2002
    Assignee: Sandel Avionics, Inc.
    Inventor: Gerald J. Block
  • Publication number: 20020126040
    Abstract: Embodiments of the invention provide a method and apparatus for indicating aircraft height relative to an obstruction in a terrain awareness warning system. The method includes receiving data indicative of geographic features of an obstruction, lateral distance of the geographic feature from an aircraft, height and flight path of the aircraft, calculating a projected height of the aircraft at the location of the obstruction using the data, generating a result signal, and displaying a colored indication on a display screen based on the result signal. The apparatus includes inputs for signals from instruments measuring height, flight path, and location of an aircraft, as well as an input for an instrument providing information about geographic features of terrain surrounding the aircraft. The apparatus includes a means for employing the signals to calculate an effective height of the aircraft relative to the terrain, and a screen display for graphically displaying the results of the calculation.
    Type: Application
    Filed: October 11, 2001
    Publication date: September 12, 2002
    Inventor: Gerald J. Block
  • Publication number: 20020116097
    Abstract: A system for reducing nuisance alerts and warnings in a terrain awareness and warning system for an aircraft, including determining if the aircraft is within a predetermined geometric volume surrounding an airport. If the aircraft is within the geometric volume, then determining the aircraft's current projected flight path for a selected distance or time and comparing it with at least one approach volume extending from a runway at the airport towards an outer boundary of the geometric volume. If the aircraft's current projected flight path is such that the aircraft is expected to be within the approach volume and stay within the approach volume to the runway, then inhibiting selected alerts and warnings associated with non-threatening terrain.
    Type: Application
    Filed: October 11, 2001
    Publication date: August 22, 2002
    Inventors: Gerald J. Block, Albert J. Bourdon
  • Publication number: 20010035832
    Abstract: A display system for an airplane or other vehicle is disclosed. A rear projection LCD is used to allow for a maximum amount of screen area to be used in displaying operator pertinent data.
    Type: Application
    Filed: May 22, 2001
    Publication date: November 1, 2001
    Applicant: Sandel Avionics
    Inventor: Gerald J. Block