Patents by Inventor Robert W. Coburn

Robert W. Coburn 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: 5280889
    Abstract: "A vehicle and the ballistic shock isolator therefor including a turret, a sensor assembly and a shock isolator isolating the turret from the sensor switch and including upper and lower annular members, a plurality of leaves secured at opposing ends thereof to the annular members, each of the leaves having a corrugated bellows shaped portion in the form of an even number of similarly shaped portions, alternate ones of the similarly shaped portions having an open end in opposing directions, each of the leaves varying in thickness and width in a direction from the upper annular member to the lower annular member. The variation in width of the portion is alternately from wide to narrow and then from narrow to wide in a direction from the upper annular member to the lower annular member.
    Type: Grant
    Filed: April 8, 1991
    Date of Patent: January 25, 1994
    Assignee: Texas Instruments Incorporated
    Inventors: David L. Amil, William D. Bracken, Robert W. Coburn, Richard L. Knipe, Gregory G. Mooty, David D. Ratcliff, Daniel W. Stanley, Kenneth L. Taylor, Steven S. Stresau
  • Patent number: 5020436
    Abstract: A booster retarding apparatus for an airborne vehicle such as a missile having a separable booster at its rear end, comprises a series of flaps with hinge assemblies for securing the flaps to the aft end of the booster for movement between an inner position extending rearwardly from the booster and an extended position projecting outwardly from the booster. The flaps are biased towards the extended position, and normally retained in the inner position by retaining devices. The retaining devices are released on booster thrust termination, and include a release mechanism responsive to booster thrust termination for releasing the retaining devices. The release mechanism includes a biasing device having a biasing force less than the acceleration forces developed on launch which oppose operation of the release mechanism so that the flaps are held in during booster thrust and are released and urged outwardly on booster thrust termination to brake the booster and separate it from the remainder of the missile.
    Type: Grant
    Filed: July 24, 1989
    Date of Patent: June 4, 1991
    Assignee: General Dynamics Corp., Air Defense Systems Div.
    Inventor: Robert W. Coburn