Patents by Inventor Cyro Stone

Cyro Stone 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: 7570177
    Abstract: Methods and systems are disclosed for preventing aircraft collisions with forward looking terrain avoidance (FLTA) functionality based on a terrain avoidance profile used to evaluate potential terrain threats based on the projected flight path of an aircraft in flight, and a clear terrain profile to determine whether the terrain threat has been cleared. If the terrain avoidance profile conflicts with terrain, a collision threat may exist whereby the pilot is notified and a terrain avoidance maneuver is executed. During the terrain avoidance maneuver the clear terrain profile extends in a direction substantially parallel with the horizon at or near the present altitude of the aircraft to check whether it is safe to return to the previous flight path angle or otherwise end the terrain-avoiding maneuver. When the clear terrain profile no longer conflicts with the terrain threat, a terrain clear indicator is then issued to the pilot.
    Type: Grant
    Filed: June 19, 2006
    Date of Patent: August 4, 2009
    Assignee: Aviation Communication & Surveillance Systems LLC
    Inventors: Zachary Reynolds, Richard Ridenour, Cyro Stone, Stacey Rowlan
  • Publication number: 20070080848
    Abstract: A delineated collision avoidance system may comprise a processor for executing one or more instructions that implement one or more functions of the collision avoidance system, a transceiver for transmitting information from and receiving information for the host aircraft, and memory for storing the one or more instructions for execution by the processor to implement the one or more functions of the collision avoidance system to: receive from the transceiver information from another aircraft, generate from the received information a track for the other aircraft, and determine whether the track will intersect within a predefined period of time a region of interest around the host aircraft. In a variation, the system may include a display and the memory may include instructions to: determine whether a predefined condition is satisfied and change an appearance of a symbol shown on the display to indicate that the predefined condition is satisfied.
    Type: Application
    Filed: June 12, 2006
    Publication date: April 12, 2007
    Inventors: Cyro Stone, Gregory Stayton, Charles Manberg
  • Publication number: 20070061055
    Abstract: An aircraft control system is delineated for a host aircraft, the system comprising a processor for executing one or more instructions that implement one or more functions of the aircraft control system, a transceiver for transmitting information from and receiving information for the host aircraft, and memory for storing the one or more instructions for execution by the processor to implement the one or more functions of the aircraft control system to: receive from the transceiver information from another aircraft, and generate from the received information a signal for use in the host aircraft to control separation between the host aircraft and the other aircraft while the aircraft are within a predefined range of a location where the aircraft plan to land.
    Type: Application
    Filed: June 13, 2006
    Publication date: March 15, 2007
    Inventors: Cyro Stone, Gregory Stayton, Charles Manberg
  • Publication number: 20070040658
    Abstract: A subsystem of an avionics system is operated in a first mode for receiving software via a port; and in a second mode in accordance with a circuit that includes a terminator coupled to the port. By using the terminator to convey information regarding a desired configuration for operation in the second mode, communication and wiring is avoided between subsystems of the avionics system for conveying such information. In one implementation, operation in the second mode includes performing a collision avoidance function (e.g., providing a TCAS advisory). Configuration information in accordance with the circuit may specify an arrangement of shared antennas between multiple transponders and/or mode changes related to using an antenna for a collision avoidance function in a hijack mode of operation.
    Type: Application
    Filed: August 28, 2006
    Publication date: February 22, 2007
    Inventors: Cyro Stone, Douglas Guetter, Desi Stelling
  • Publication number: 20060290531
    Abstract: Methods and systems are disclosed for preventing aircraft collisions with forward looking terrain avoidance (FLTA) functionality based on a terrain avoidance profile used to evaluate potential terrain threats based on the projected flight path of an aircraft in flight, and a clear terrain profile to determine whether the terrain threat has been cleared. If the terrain avoidance profile conflicts with terrain, a collision threat may exist whereby the pilot is notified and a terrain avoidance maneuver is executed. During the terrain avoidance maneuver the clear terrain profile extends in a direction substantially parallel with the horizon at or near the present altitude of the aircraft to check whether it is safe to return to the previous flight path angle or otherwise end the terrain-avoiding maneuver. When the clear terrain profile no longer conflicts with the terrain threat, a terrain clear indicator is then issued to the pilot.
    Type: Application
    Filed: June 19, 2006
    Publication date: December 28, 2006
    Inventors: Zachary Reynolds, Richard Ridenour, Cyro Stone, Stacey Rowlan
  • Patent number: 7064680
    Abstract: Methods and systems are disclosed for preventing aircraft collisions with forward looking terrain avoidance (FLTA) functionality based on a terrain avoidance profile used to evaluate potential terrain threats based on the projected flight path of an aircraft in flight, and a clear terrain profile to determine whether the terrain threat has been cleared. If the terrain avoidance profile conflicts with terrain, a collision threat may exist whereby the pilot is notified and a terrain avoidance maneuver is executed. During the terrain avoidance maneuver the clear terrain profile extends in a direction substantially parallel with the horizon at or near the present altitude of the aircraft to check whether it is safe to return to the previous flight path angle or otherwise end the terrain-avoiding maneuver. When the clear terrain profile no longer conflicts with the terrain threat, a terrain clear indicator is then issued to the pilot.
    Type: Grant
    Filed: December 20, 2002
    Date of Patent: June 20, 2006
    Assignee: Aviation Communications & Surveillance Systems LLC
    Inventors: Zachary Reynolds, Richard Ridenour, Cyro Stone, Stacey Rowlan
  • Publication number: 20060097895
    Abstract: Methods and systems are disclosed for preventing aircraft collisions with forward looking terrain avoidance (FLTA) functionality based on a terrain avoidance profile used to evaluate potential terrain threats based on the projected flight path of an aircraft in flight, and a clear terrain profile to determine whether the terrain threat has been cleared. If the terrain avoidance profile conflicts with terrain, a collision threat may exist whereby the pilot is notified and a terrain avoidance maneuver is executed. During the terrain avoidance maneuver the clear terrain profile extends in a direction substantially parallel with the horizon at or near the present altitude of the aircraft to check whether it is safe to return to the previous flight path angle or otherwise end the terrain-avoiding maneuver. When the clear terrain profile no longer conflicts with the terrain threat, a terrain clear indicator is then issued to the pilot.
    Type: Application
    Filed: December 20, 2002
    Publication date: May 11, 2006
    Inventors: Zachary Reynolds, Richard Ridenour, Cyro Stone, Stacey Rowlan