Patents by Inventor Gary F. Hawkins

Gary F. Hawkins 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: 9220310
    Abstract: Force diversion apparatus, methods and devices including the same result in rotational motion being imparted to an impacting object. The apparatus, methods and devices may include, or may involve the use of, a force conversion portion, secured to the outer surface of a bumper, and a force spreading portion.
    Type: Grant
    Filed: April 8, 2010
    Date of Patent: December 29, 2015
    Assignee: The Aerospace Corporation
    Inventors: Gary F. Hawkins, Ching-Yao Tang
  • Patent number: 9194452
    Abstract: Vibration damping apparatus, systems, objects including such apparatus and systems, and vibration damping methods. The vibration damping involves amplifying a vibration-induced displacement and damping the amplified displacement.
    Type: Grant
    Filed: October 31, 2012
    Date of Patent: November 24, 2015
    Assignee: The Aerospace Corporation
    Inventors: Gary F. Hawkins, Ching-Yao Tang
  • Patent number: 8931606
    Abstract: Force diversion apparatus, methods and devices including the same result in rotational motion being imparted to an impacting object.
    Type: Grant
    Filed: November 29, 2008
    Date of Patent: January 13, 2015
    Assignee: The Aerospace Corporation
    Inventors: Gary F. Hawkins, Ching-Yao Tang
  • Publication number: 20140117600
    Abstract: Vibration damping apparatus, systems, objects including such apparatus and systems, and vibration damping methods. The vibration damping involves amplifying a vibration-induced displacement and damping the amplified displacement.
    Type: Application
    Filed: October 31, 2012
    Publication date: May 1, 2014
    Applicant: The Aerospace Corporation
    Inventors: Gary F. Hawkins, Ching-Yao Tang
  • Publication number: 20120139172
    Abstract: Force diversion apparatus, methods and devices including the same result in rotational motion being imparted to an impacting object.
    Type: Application
    Filed: November 29, 2008
    Publication date: June 7, 2012
    Inventors: Gary F. Hawkins, Ching-Yao Tang
  • Publication number: 20100313745
    Abstract: Force diversion apparatus, methods and devices including the same result in rotational motion being imparted to an impacting object.
    Type: Application
    Filed: April 8, 2010
    Publication date: December 16, 2010
    Inventors: Gary F. Hawkins, Ching-Yao Tang
  • Patent number: 7815146
    Abstract: A fixed sized bell rocket nozzle is lined with a layer of combustible material that is ignited during launch ignition and burns to outgas into the rocket exhaust for spatially variably confining the exhaust and perfecting an effective variably sized altitude compensating exhaust nozzle that maximizes lift during the launch of a spacecraft into orbit.
    Type: Grant
    Filed: August 29, 2001
    Date of Patent: October 19, 2010
    Assignee: The Aerospace Corporation
    Inventors: Gary F. Hawkins, John W. Murdock
  • Patent number: 7708653
    Abstract: A sports implement in accordance with at least one exemplary implementation includes a golf club head and a force diversion apparatus on the golf club head. The force diversion apparatus may include a force conversion portion configured to redirect at least a portion of a force associated with an object impacting the force diversion apparatus and a strike plate.
    Type: Grant
    Filed: March 4, 2008
    Date of Patent: May 4, 2010
    Assignee: The Aerospace Corporation
    Inventors: Gary F. Hawkins, Ching-Yao Tang
  • Publication number: 20100083915
    Abstract: An electromechanical actuator includes a cylinder and piston for driving a load and defining a chamber in which is disposed a buffer gas, such as nitrogen, and a solid or water-based electrolyte, and electrodes for generating hydrogen and oxygen by electrolysis that mixes with the buffer gas serving to control the combustion pressure profile, and into which chamber, above the electrolyte, is inserted an igniter for combusting the hydrogen and oxygen for creating high pressures in the chamber to move the piston and create efficient mechanical work.
    Type: Application
    Filed: October 8, 2008
    Publication date: April 8, 2010
    Inventors: Gary F. Hawkins, Thomas J. Curtiss, Eric W. Fournier, Michael J. O'Brien
  • Patent number: 7565950
    Abstract: A sound suppression method includes using a passive noise suppression technology to destructively interfere with a sound wave propagating through a structure at portions of the structure that are positioned apart less than half of a wavelength of the sound wave.
    Type: Grant
    Filed: January 26, 2005
    Date of Patent: July 28, 2009
    Assignee: The Aerospace Corporation
    Inventors: Gary F. Hawkins, Michael J. O'Brien
  • Publication number: 20090133405
    Abstract: A fixed sized bell rocket nozzle is lined with a layer of combustible material that is ignited during launch ignition and burns to outgas into the rocket exhaust for spatially variably confining the exhaust and perfecting an effective variably sized altitude compensating exhaust nozzle that maximizes lift during the launch of a spacecraft into orbit.
    Type: Application
    Filed: August 29, 2001
    Publication date: May 28, 2009
    Applicant: The Aerospace Corporation
    Inventors: Gary F. Hawkins, John W. Murdock
  • Patent number: 7461726
    Abstract: Force diversion apparatus, methods and devices including the same result in rotational motion being imparted to an impacting object.
    Type: Grant
    Filed: February 25, 2005
    Date of Patent: December 9, 2008
    Assignee: The Aerospace Corporation
    Inventors: Gary F. Hawkins, Ching-Yao Tang
  • Publication number: 20080268978
    Abstract: Force diversion apparatus, methods and devices including the same result in rotational motion being imparted to an impacting object.
    Type: Application
    Filed: March 4, 2008
    Publication date: October 30, 2008
    Inventors: Gary F. Hawkins, Ching-Yao Tang
  • Patent number: 7367898
    Abstract: Force diversion apparatus, methods and devices including the same result in rotational motion being imparted to an impacting object.
    Type: Grant
    Filed: February 25, 2005
    Date of Patent: May 6, 2008
    Assignee: The Aerospace Corporation
    Inventors: Gary F. Hawkins, Ching-Yao Tang
  • Patent number: 6946180
    Abstract: A composite material is provided that includes a matrix material, and a plurality of deflectable elements or “machines” disposed in the matrix material, the machines acting to modify one or more physical properties of the composite material in response to forces acting upon the composite material. Preferably, the machines have an elongate shape defining a longitudinal axis, which are disposed within the matrix material in a predetermined array. The elongate members have an asymmetrical cross-section which is deflectable between first and second shapes, and consequently the composite material exhibits different physical properties because the elongate members deflect between the first and second shapes. The machines may include a variety of asymmetrical cross-sections, such as a generally “Z” shape, an hourglass shape, a cantilever shape or a leaf spring shape.
    Type: Grant
    Filed: June 18, 2002
    Date of Patent: September 20, 2005
    Assignee: The Aerospace Corporation
    Inventor: Gary F. Hawkins
  • Patent number: 6830793
    Abstract: A composite material is provided that includes an array of machine elements disposed within a matrix material. Each machine element includes a cross-section defining an internal space that is filled with a viscous fluid. Preferably, the machine elements are provided in complementary pairs of tubular members, with the internal spaces of the tubular members communicating with one another. When subjected to a predetermined force, the cross-sections of the tubular members change shape, changing the volume of the internal spaces, and causing fluid to flow into or out of the internal spaces. Preferably, under the predetermined force, one tubular member increases in volume and the other tubular member simultaneously decreases in volume, thereby causing fluid to flow between the tubular elements to dissipate energy from the predetermined force.
    Type: Grant
    Filed: March 20, 2002
    Date of Patent: December 14, 2004
    Assignee: The Aerospace Corporation
    Inventors: Gary F Hawkins, John W. Murdock
  • Patent number: 6588969
    Abstract: A micromachine is embedded into an adhesive film for increasing the shear strength of the adhesive used to form a bonding joint. The micromachine has an irregular shaped cross section, such as a trapezoid, so that when the micromachine tends to rotate between two bonded adherents, a surface portion of the micromachine tends to penetrate into and compress the adhesive towards a bonding interface with the constrained adherent for increasing the shear strength of the bonding joint.
    Type: Grant
    Filed: August 13, 2001
    Date of Patent: July 8, 2003
    Assignee: The Aerospace Corporation
    Inventor: Gary F. Hawkins
  • Publication number: 20030031507
    Abstract: A micromachine is embedded into an adhesive film for increasing the shear strength of the adhesive used to form a bonding joint. The micromachine has an irregular shaped cross section, such as a trapezoid, so that when the micromachine tends to rotate between two bonded adherents, a surface portion of the micromachine tends to penetrate into and compress the adhesive towards a bonding interface with the constrained adherent for increasing the shear strength of the bonding joint.
    Type: Application
    Filed: August 13, 2001
    Publication date: February 13, 2003
    Applicant: The Aerospace Corporation
    Inventor: Gary F. Hawkins
  • Publication number: 20020196834
    Abstract: A glass transition temperature Tg measurement system includes a probe point penetrating into a sample under test that has been heated by a heater to a temperature where the sample undergoes a phase change from a solid to a semisolid. A thermocouple is used to measure the temperature while a motion transducer is used to measure the amount of penetration. The penetration amount sharply increases at the glass transition temperature. A portable unit can be used in the field to test the Tg properties of various composite materials used, for example, in structures including buildings and bridges.
    Type: Application
    Filed: June 22, 2001
    Publication date: December 26, 2002
    Inventors: Rafael J. Zaldivar, James P. Nokes, Gary F. Hawkins
  • Publication number: 20020172783
    Abstract: A composite material is provided that includes an array of machine elements disposed within a matrix material. Each machine element includes a cross-section defining an internal space that is filled with a viscous fluid. Preferably, the machine elements are provided in complementary pairs of tubular members, with the internal spaces of the tubular members communicating with one another. When subjected to a predetermined force, the cross-sections of the tubular members change shape, changing the volume of the internal spaces, and causing fluid to flow into or out of the internal spaces. Preferably, under the predetermined force, one tubular member increases in volume and the other tubular member simultaneously decreases in volume, thereby causing fluid to flow between the tubular elements to dissipate energy from the predetermined force.
    Type: Application
    Filed: March 20, 2002
    Publication date: November 21, 2002
    Applicant: The Aerospace Corporation
    Inventors: Gary F. Hawkins, John W. Murdock