Patents by Inventor William C. Brodegard

William C. Brodegard 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: 7085630
    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: Grant
    Filed: July 29, 2005
    Date of Patent: August 1, 2006
    Assignee: Avidyne Corporation
    Inventors: Dean E. Ryan, William C. Brodegard
  • Patent number: 6978205
    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: Grant
    Filed: October 26, 2004
    Date of Patent: December 20, 2005
    Assignee: Ryan International Corporation
    Inventors: Dean E. Ryan, William C. Brodegard
  • 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: 5388047
    Abstract: A proximity warning device for aircraft responds solely to transmissions from transponders. The host aircraft has a host transponder and a signal is generated therein and coupled to the device to indicate transmission of a host reply. Selective suppression is implemented based on presence of an SSR beam which is indicated by the signal. Suppression pulses have a fixed duration but randomly selected intervening durations. Data collection proceeds without regard for suppression or the presence of host replies. The shaping of data collection intervals free of interference from suppression provides for improved efficiency for later data decoding and processing. The signal is used to specially mark collected data generated by a host reply. The ability to discriminate between host and other replies allows completely new performance monitoring functions. In one case, the health of the receiver is deduced from the amplitude of host replies.
    Type: Grant
    Filed: March 18, 1992
    Date of Patent: February 7, 1995
    Assignee: Ryan International Corp.
    Inventors: Dean E. Ryan, Paul A. Ryan, William C. Brodegard
  • Patent number: 5157615
    Abstract: A passive aircraft Traffic alert and Collision Avoidance Device (TCAD) is based on sensing and responding to transponder replies of other aircraft to SSR interrogations. In order to avoid masking other aircraft replies by the host transponder TCAD repeatedly and randomly suppresses the host transponder and simultaneoulsly listens for other aircraft replies. Suppression on each occasion is effective for an equal and predetermined duration which is much longer than a typical replay, in a preferred embodiment the suppression/listen duration is 725 .mu.s. In this embodiment the time between successive suppression/listen occasions is random between 725 .mu.s. and 5.025 ms. with an average value of about 2.9 ms. Digital signal processing is used to detect and discard garbled or overlapping replies. Each valid reply, exhibiting a minimum pulse amplitude, is decoded and correlated with a calibrated range parameter and given a time tag.
    Type: Grant
    Filed: December 31, 1991
    Date of Patent: October 20, 1992
    Assignee: Ryan International Corporation
    Inventors: William C. Brodegard, Dean E. Ryan, Paul A. Ryan
  • Patent number: 5077673
    Abstract: A passive aircraft Traffic alert and Collision Avoidance device (TCAD) is based on sensing and responding to transponder replies of other aircraft to SSR interrogations. In order to avoid masking other aircraft replies by the host transponder TCAD repeatedly and randomly suppresses the host transponder and simultaneously listens for other aircraft replies. Suppression on each occasion is effective for an equal and predetermined duration which is much longer than a typical reply, in a preferred embodiment the suppression/listen duration is 725 .mu.s. In this embodiment the time between successive suppression/listen occasions is random between 725 .mu.s. and 5.025 ms. with an average value of about 2.9 ms. Digital signal processing is used to detect and discard garbled or overlapping replies. Each valid reply, exhibiting a minimum pulse amplitude, is decoded and correlated with a calibrated range parameter and given a time tag.
    Type: Grant
    Filed: January 9, 1990
    Date of Patent: December 31, 1991
    Assignee: Ryan International Corp.
    Inventors: William C. Brodegard, Dean E. Ryan, Paul A. Ryan