Patents Assigned to Advanced Aerospace Technologies, Inc.
  • Patent number: 9669946
    Abstract: A method of launching and retrieving a UAV (Unmanned Aerial Vehicle) (10). The preferred method of launch involves carrying the UAV (10) up to altitude using a parasail (8) similar to that used to carry tourists aloft. The UAV is dropped and picks up enough airspeed in the dive to perform a pull-up into level controlled flight. The preferred method of recovery is for the UAV to fly into and latch onto the parasail tow line (4) or cables hanging off the tow line and then be winched back down to the boat (2).
    Type: Grant
    Filed: October 20, 2014
    Date of Patent: June 6, 2017
    Assignee: Advanced Aerospace Technologies, Inc.
    Inventors: William R. McDonnell, Charles H. Baker
  • Patent number: 8864069
    Abstract: A method of launching and retrieving a UAV (Unmanned Aerial Vehicle) (10). The preferred method of launch involves carrying the UAV (10) up to altitude using a parasail (8) similar to that used to carry tourists aloft. The UAV is dropped and picks up enough airspeed in the dive to perform a pull-up into level controlled flight. The preferred method of recovery is for the UAV to fly into and latch onto the parasail tow line (4) or cables hanging off the tow line and then be winched back down to the boat (2).
    Type: Grant
    Filed: August 26, 2013
    Date of Patent: October 21, 2014
    Assignee: Advanced Aerospace Technologies, Inc.
    Inventor: William R. McDonnell
  • Publication number: 20140231585
    Abstract: A method of launching and retrieving a UAV (Unmanned Aerial Vehicle) (10). The preferred method of launch involves carrying the UAV (10) up to altitude using a parasail (8) similar to that used to carry tourists aloft. The UAV is dropped and picks up enough airspeed in the dive to perform a pull-up into level controlled flight. The preferred method of recovery is for the UAV to fly into and latch onto the parasail tow line (4) or cables hanging off the tow line and then be winched back down to the boat (2).
    Type: Application
    Filed: August 26, 2013
    Publication date: August 21, 2014
    Applicant: Advanced Aerospace Technologies, Inc.
    Inventor: William R. McDonnell
  • Patent number: 8567718
    Abstract: A method of launching and retrieving a UAV (Unmanned Aerial Vehicle) (10). The preferred method of launch involves carrying the UAV (10) up to altitude using a parasail (8) similar to that used to carry tourists aloft. The UAV is dropped and picks up enough airspeed in the dive to perform a pull-up into level controlled flight. The preferred method of recovery is for the UAV to fly into and latch onto the parasail tow line (4) or cables hanging off the tow line and then be winched back down to the boat (2).
    Type: Grant
    Filed: March 4, 2013
    Date of Patent: October 29, 2013
    Assignee: Advanced Aerospace Technologies, Inc.
    Inventor: William Randall McDonnell
  • Patent number: 8517306
    Abstract: A method of launching and retrieving a UAV (Unmanned Aerial Vehicle) (10). The preferred method of launch involves carrying the UAV (10) up to altitude using a parasail (8) similar to that used to carry tourists aloft. The UAV is dropped and picks up enough airspeed in the dive to perform a pull-up into level controlled flight. The preferred method of recovery is for the UAV to fly into and latch onto the parasail tow line (4) or cables hanging off the tow line and then be winched back down to the boat (2).
    Type: Grant
    Filed: August 28, 2006
    Date of Patent: August 27, 2013
    Assignee: Advanced Aerospace Technologies, Inc.
    Inventors: William R. McDonnell, Charles H. Baker
  • Patent number: 8167242
    Abstract: A method of launching and retrieving a UAV (Unmanned Aerial Vehicle) (10). The preferred method of launch involves carrying the UAV (10) up to altitude using a parasail (8) similar to that used to carry tourists aloft. The UAV is dropped and picks up enough airspeed in the dive to perform a pull-up into level controlled flight. The preferred method of recovery is for the UAV to fly into and latch onto the parasail tow line (4) or cables hanging off the tow line and then be winched back down to the boat (2).
    Type: Grant
    Filed: September 29, 2010
    Date of Patent: May 1, 2012
    Assignee: Advanced Aerospace Technologies, Inc.
    Inventor: William R. McDonnell
  • Publication number: 20110127378
    Abstract: A method of launching and retrieving a UAV (Unmanned Aerial Vehicle) (10). The preferred method of launch involves carrying the UAV (10) up to altitude using a parasail (8) similar to that used to carry tourists aloft. The UAV is dropped and picks up enough airspeed in the dive to perform a pull-up into level controlled flight. The preferred method of recovery is for the UAV to fly into and latch onto the parasail tow line (4) or cables hanging off the tow line and then be winched back down to the boat (2).
    Type: Application
    Filed: February 4, 2011
    Publication date: June 2, 2011
    Applicant: ADVANCED AEROSPACE TECHNOLOGIES, INC.
    Inventor: William R. McDonnell
  • Publication number: 20110011974
    Abstract: A method of launching and retrieving a UAV (Unmanned Aerial Vehicle) (10). The preferred method of launch involves carrying the UAV (10) up to altitude using a parasail (8) similar to that used to carry tourists aloft. The UAV is dropped and picks up enough airspeed in the dive to perform a pull-up into level controlled flight. The preferred method of recovery is for the UAV to fly into and latch onto the parasail tow line (4) or cables hanging off the tow line and then be winched back down to the boat (2).
    Type: Application
    Filed: September 29, 2010
    Publication date: January 20, 2011
    Applicant: ADVANCED AEROSPACE TECHNOLOGIES, INC.
    Inventor: William R. McDonnell
  • Patent number: 7097137
    Abstract: A method of launching and retrieving a UAV (Unmanned Aerial Vehicle) (10). The preferred method of launch involves carrying the UAV (10) up to altitude using a parasail (8) similar to that used to carry tourists aloft. The UAV is dropped and picks up enough airspeed in the dive to perform a pull-up into level controlled flight. The preferred method of recovery is for the UAV to fly into and latch onto the parasail tow line (4) or cables hanging off the tow line and then be winched back down to the boat (2).
    Type: Grant
    Filed: January 9, 2004
    Date of Patent: August 29, 2006
    Assignee: Advanced Aerospace Technologies, Inc.
    Inventor: William R. McDonnell
  • Patent number: 6874729
    Abstract: A method of launching and retrieving a UAV (Unmanned Aerial Vehicle) (10). The preferred method of launch involves carrying the UAV (10) up to altitude using a parasail (8) similar to that used to carry tourists aloft. The UAV is dropped and picks up enough airspeed in the dive to perform a pull-up into level controlled flight. The preferred method of recovery is for the UAV to fly into and latch onto the parasail tow line (4) or cables hanging off the tow line and then be winched back down to the boat (2).
    Type: Grant
    Filed: July 24, 2000
    Date of Patent: April 5, 2005
    Assignee: Advanced Aerospace Technologies, Inc.
    Inventor: William R. McDonnell
  • Patent number: 6705573
    Abstract: A pod (34) containing sensors and/or targeting systems such as laser designators or range finders are hung on a cable (30) below an aircraft (12). The line (30) can be reeled in or out similar to towed decoys. This allows the aircraft (12) to operate above or in the cloud cover while the sensors/targeting equipment (34) are operating below the cloud cover to find the enemy forces.
    Type: Grant
    Filed: June 28, 2002
    Date of Patent: March 16, 2004
    Assignee: Advanced Aerospace Technologies, Inc.
    Inventor: William R. McDonnell
  • Patent number: 5799900
    Abstract: An aircraft adapted for flight in helicopter mode with its longitudinal axis oriented generally vertically and in airplane mode with its longitudinal axis oriented generally horizontally is provided with the capability of launching and landing with the tail end directed skyward. The invention also includes improvements to the controllability and efficiency of aircraft in helicopter mode provided by the stabilizer wings and relative rotation of the fuselage section about the aircraft's longitudinal axis. The aircraft has an elongate boom positioned between the rear fuselage and the stabilizer wings for engagement with a base structure. The base structure may be attached to a building, a trailer transporter, a ship or some other structure. The base may be a beam having latching arms that swing inward when pressure from the boom is applied, then trap the boom in a recess between the latching arm and beam, thereby suspending the aircraft.
    Type: Grant
    Filed: July 15, 1996
    Date of Patent: September 1, 1998
    Assignee: Advanced Aerospace Technologies, Inc.
    Inventor: William R. McDonnell