Patents by Inventor Robert Gilchrist, III

Robert Gilchrist, III 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: 10843817
    Abstract: Systems and methods for recovering unmanned aircraft and controlling post-recovery motion of the aircraft are disclosed herein. An aircraft recovery system for handling an unmanned aircraft in accordance with one embodiment of the disclosure includes a base portion and an elongated aircraft capture member having a first end movably coupled to the base portion and a second, free end opposite the first end. The aircraft capture member includes a first portion and a second portion at a distal end of the first portion and positioned to intercept an unmanned aircraft in flight. The first and/or second portions are generally flexible. The system further includes an energy capture and dissipation assembly operably coupled to the aircraft capture member and positioned to receive at least a portion of the landing forces from the aircraft.
    Type: Grant
    Filed: March 12, 2018
    Date of Patent: November 24, 2020
    Assignee: Insitu, Inc.
    Inventors: Robert Gilchrist, III, John Stafford, Brian D. Dennis, Allen Smith, Jaime Mack, Steven M. Sliwa, Bradley Louis Schrick, Robert Hughes
  • Publication number: 20180273204
    Abstract: Systems and methods for recovering unmanned aircraft and controlling post-recovery motion of the aircraft are disclosed herein. An aircraft recovery system for handling an unmanned aircraft in accordance with one embodiment of the disclosure includes a base portion and an elongated aircraft capture member having a first end movably coupled to the base portion and a second, free end opposite the first end. The aircraft capture member includes a first portion and a second portion at a distal end of the first portion and positioned to intercept an unmanned aircraft in flight. The first and/or second portions are generally flexible. The system further includes an energy capture and dissipation assembly operably coupled to the aircraft capture member and positioned to receive at least a portion of the landing forces from the aircraft.
    Type: Application
    Filed: March 12, 2018
    Publication date: September 27, 2018
    Inventors: Robert Gilchrist, III, John Stafford, Brian D. Dennis, Allen Smith, Jaime Mack, Steven M. Sliwa, Bradley Louis Schrick, Robert Hughes
  • Patent number: 9944408
    Abstract: Systems and methods for recovering unmanned aircraft and controlling post-recovery motion of the aircraft are disclosed herein. An aircraft recovery system for handling an unmanned aircraft in accordance with one embodiment of the disclosure includes a base portion and an elongated aircraft capture member having a first end movably coupled to the base portion and a second, free end opposite the first end. The aircraft capture member includes a first portion and a second portion at a distal end of the first portion and positioned to intercept an unmanned aircraft in flight. The first and/or second portions are generally flexible. The system further includes an energy capture and dissipation assembly operably coupled to the aircraft capture member and positioned to receive at least a portion of the landing forces from the aircraft.
    Type: Grant
    Filed: October 21, 2011
    Date of Patent: April 17, 2018
    Assignee: Insitu, Inc.
    Inventors: Robert Gilchrist, III, John Stafford, Brian D. Dennis, Allen Smith, Jaime Mack, Steven M. Sliwa, Bradley Schrick, Robert Hughes
  • Publication number: 20120223182
    Abstract: Systems and methods for recovering unmanned aircraft and controlling post-recovery motion of the aircraft are disclosed herein. An aircraft recovery system for handling an unmanned aircraft in accordance with one embodiment of the disclosure includes a base portion and an elongated aircraft capture member having a first end movably coupled to the base portion and a second, free end opposite the first end. The aircraft capture member includes a first portion and a second portion at a distal end of the first portion and positioned to intercept an unmanned aircraft in flight. The first and/or second portions are generally flexible. The system further includes an energy capture and dissipation assembly operably coupled to the aircraft capture member and positioned to receive at least a portion of the landing forces from the aircraft.
    Type: Application
    Filed: October 21, 2011
    Publication date: September 6, 2012
    Applicant: Insitu, Inc.
    Inventors: Robert Gilchrist, III, John Stafford, Brian D. Dennis, Allen Smith, Jaime Mack, Steven M. Sliwa, Bradley Schrick, Robert Hughes