Patents by Inventor Robert D. Blackshire

Robert D. Blackshire 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: 6106008
    Abstract: An improved hybrid airbag inflator comprises a container for storing a compressed gas having a rupturable wall defining an exit opening. A pyrotechnic gas generator has an output directed into the container for adding heat and mass flow to the compressed gas in the container. A single initiator ruptures the rupturable wall and initiates the gas generator, preferably via a pyrotechnic delay train which initiates combustion of the gas generator after a predetermined delay, to provide for delayed onset of the high pressure gas generator input. The initiator is preferably an electric detonator that produces a self forging fragment to rupture the rupturable wall and initiate the pyrotechnic delay. The pyrotechnic generator may also have a second output directed into a manifold leading from the container to the airbag and entering the manifold downstream from the inlet nozzles that restrict the flow of compressed gas into the manifold.
    Type: Grant
    Filed: July 23, 1996
    Date of Patent: August 22, 2000
    Assignee: Ad Astram Scientific LLC
    Inventors: Robert D. Blackshire, Milan L. Storch, Clyde L. Jones
  • Patent number: 5738371
    Abstract: An improved hybrid airbag inflator comprises a container for storing a compressed gas having a rupturable wall defining an exit opening. A pyrotechnic gas generator has an output directed into the container for adding heat and mass flow to the compressed gas in the container. The pyrotechnic generator may also have a second output directed into a manifold leading from the container to the airbag, the second output entering the manifold downstream from the inlet nozzles that restrict the flow of compressed gas into the manifold. Adding the second output directly to the manifold increases the energy content of the gas filling the airbag without physically changing the size of the inlet nozzles, thereby allowing a readily controllable staged flow of gases into the airbag. A single initiator ruptures the rupturable wall and initiates the gas generator, either directly or via a pyrotechnic delay train which initiates combustion of the gas generator after a predetermined delay.
    Type: Grant
    Filed: February 16, 1996
    Date of Patent: April 14, 1998
    Assignee: Ad Astam Scientific, L.L.C.
    Inventors: Robert D. Blackshire, Milan L. Storch, Clyde L. Jones
  • Patent number: 5538278
    Abstract: An improved hybrid airbag inflator comprises a container for storing a compressed gas having a rupturable wall defining an exit opening. A pyrotechnic gas generator has an output directed into the container for adding heat and mass flow to the compressed gas in the container. The pyrotechnic generator may also have a second output directed into a manifold leading from the container to the airbag, the second output entering the manifold downstream from the inlet nozzles that restrict the flow of compressed gas into the manifold. Adding the second output directly to the manifold increases the energy content of the gas filling the airbag without physically changing the size of the inlet nozzles, thereby allowing a readily controllable staged flow of gases into the airbag.
    Type: Grant
    Filed: June 14, 1994
    Date of Patent: July 23, 1996
    Assignee: Ad Astram Enterprises, Inc.
    Inventors: Robert D. Blackshire, Milan L. Storch, Clyde L. Jones
  • Patent number: 4706909
    Abstract: A catapult seat ejection system for ejecting a pilot and seat from an aircraft is disclosed in which the thrust of the catapult is controlled to prevent injury to the pilot due to acceleration forces. The catapult comprises a main catapult tube; a piston within the tube driven by gas pressure from the burning of two solid propellants cartridges; and four shuttle vent valves powered by gas from a plurality of electrically ignited squibs controlled by an electronic control system. The catapult is initially driven by only one of the two solid propellant cartridges and the electronic controller continuously monitors acceleration. If acceleration is too great the controller fires squibs with a control signal to open the shuttle vent valves to vent the gasses from the catapult and thereby reduce the pressure and acceleration of the seat. If the acceleration is too low and the vent valves are closed, and the sensor fires the second cartridge with a second control signal.
    Type: Grant
    Filed: June 19, 1986
    Date of Patent: November 17, 1987
    Assignee: The United States of America as represented by the Secretary of the Air Force
    Inventors: Jess A. Cuevas, Robert D. Blackshire