Patents by Inventor Ron Brinkman

Ron Brinkman 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).

  • Patent number: 8849477
    Abstract: Embodiments of a method are provided that may be carried out by an avionics display system deployed on an aircraft and including a monitor. The avionics display system receives position data indicative of the aircraft's detected position from at least one data source. In one embodiment, the method includes the steps of: (i) attributing an error characteristic to the data source, (ii) identifying an airspace assigned to the aircraft at a given time, and (iii) establishing an error-compensated airspace as a function of the error characteristic and the assigned airspace. The aircraft's actual position remains within the assigned airspace provided that the aircraft's detected position resides within the error-compensated airspace. A visual representation of the outer boundaries of the error-compensated airspace is generated on the monitor.
    Type: Grant
    Filed: October 14, 2008
    Date of Patent: September 30, 2014
    Assignee: Honeywell International Inc.
    Inventor: Ron Brinkman
  • Patent number: 8362925
    Abstract: Embodiments of a process are provided suitable for implementation by an avionics display system deployed on a host aircraft and including a monitor. In one embodiment, the process includes the step of receiving air traffic data indicative of a first flight characteristic pertaining to a neighboring aircraft. The first flight characteristic is selected from the group consisting of: (i) the wake turbulence created by the neighboring aircraft, (ii) the current flight plan of the neighboring aircraft, and (iii) the airspace in which the neighboring aircraft's current detection position should reside to ensure that the neighboring aircraft's actual position resides within the an airspace currently assigned to the neighboring aircraft. A visual representation of the first flight characteristic is generated on the monitor.
    Type: Grant
    Filed: May 5, 2009
    Date of Patent: January 29, 2013
    Assignee: Honeywell International Inc.
    Inventors: Ron Brinkman, Pat Langdon
  • Patent number: 8185254
    Abstract: A method and system for updating navigation information are disclosed. The method includes the steps of connecting to a navigation information update system, determining if at least one navigation information update is available from the navigation information update system, if the at least one navigation information update is available from the navigation information update system, determining if an intended recipient of the at least one navigation information update is available or unavailable for an update.
    Type: Grant
    Filed: July 18, 2007
    Date of Patent: May 22, 2012
    Assignee: Honeywell International Inc.
    Inventor: Ron Brinkman
  • Publication number: 20100283635
    Abstract: Embodiments of a process are provided suitable for implementation by an avionics display system deployed on a host aircraft and including a monitor. In one embodiment, the process includes the step of receiving air traffic data indicative of a first flight characteristic pertaining to a neighboring aircraft. The first flight characteristic is selected from the group consisting of: (i) the wake turbulence created by the neighboring aircraft, (ii) the current flight plan of the neighboring aircraft, and (iii) the airspace in which the neighboring aircraft's current detection position should reside to ensure that the neighboring aircraft's actual position resides within the an airspace currently assigned to the neighboring aircraft. A visual representation of the first flight characteristic is generated on the monitor.
    Type: Application
    Filed: May 5, 2009
    Publication date: November 11, 2010
    Applicant: HONEYWELL INTERNATIONAL INC.
    Inventors: Ron Brinkman, Pat Langdon
  • Publication number: 20100094487
    Abstract: Embodiments of a method are provided that may be carried out by an avionics display system deployed on an aircraft and including a monitor. The avionics display system receives position data indicative of the aircraft's detected position from at least one data source. In one embodiment, the method includes the steps of: (i) attributing an error characteristic to the data source, (ii) identifying an airspace assigned to the aircraft at a given time, and (iii) establishing an error-compensated airspace as a function of the error characteristic and the assigned airspace. The aircraft's actual position remains within the assigned airspace provided that the aircraft's detected position resides within the error-compensated airspace. A visual representation of the outer boundaries of the error-compensated airspace is generated on the monitor.
    Type: Application
    Filed: October 14, 2008
    Publication date: April 15, 2010
    Applicant: Honeywell International Inc.
    Inventor: Ron Brinkman
  • Publication number: 20090024312
    Abstract: A method and system for updating navigation information are disclosed. The method includes the steps of connecting to a navigation information update system, determining if at least one navigation information update is available from the navigation information update system, if the at least one navigation information update is available from the navigation information update system, determining if an intended recipient of the at least one navigation information update is available or unavailable for an update.
    Type: Application
    Filed: July 18, 2007
    Publication date: January 22, 2009
    Applicant: HONEYWELL INTERNATIONAL INC.
    Inventor: Ron Brinkman