Patents by Inventor Bryce D. Brubaker

Bryce D. Brubaker 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: 7284487
    Abstract: Stereolithography is used to fabricate directly a single-piece, missile-usable, accurate, flightweight igniter without the use of intermediate, non-operational molds or prototypes in the fabrication process. The same prototype-less, direct stereolithography can be used to produce other missile-usable parts by designing each such part to be of a single-piece configuration and by using material that is suitable for both stereolithography and functional missile application.
    Type: Grant
    Filed: July 6, 2004
    Date of Patent: October 23, 2007
    Assignee: United States of America as represented by the Secretary of the Army
    Inventors: Robert W. Milton, Mark W. Kirkham, Robert S. Michaels, Jon A. Freeman, Bryce D. Brubaker
  • Patent number: 5062206
    Abstract: An igniter which is removably insertable in a rocket motor nozzle throat. The igniter includes a sleeve which has a body portion and a plurality of flexible and frangible tab members extending axially from one end of the body portion and spaced circumferentially thereabout and which have first portions which in combination define a diameter which is greater than the nozzle throat diameter. The frangible portions of the tab members in combination define an outer diameter which is substantially equal to the throat diameter. The body portion of the sleeve has a diameter which is greater than the throat diameter. The sleeve is insertable in the nozzle throat by flexing the tab members so that the first portions clear the throat and so that the frangible portions of the tab members are disposed in the throat. The tab members, in combination, have an inner diameter which is substantially equal to the inner diameter of the body portion of the sleeve.
    Type: Grant
    Filed: August 4, 1989
    Date of Patent: November 5, 1991
    Assignee: Thiokol Corporation
    Inventors: Robert I. Myers, Bryce D. Brubaker, Robert E. Overall
  • Patent number: 5007236
    Abstract: An igniter which is removably insertable in a rocket motor nozzle throat. The igniter includes a sleeve which has a body portion and a plurality of flexible and frangible tab members extending axially from one end of the body portion and spaced circumferentially thereabout and which have first portions which in combination define a diameter which is greater than the nozzle throat diameter. The frangible portions of the tab members in combination define an outer diameter which is substantially equal to the throat diameter. The body portion of the sleeve has a diameter which is greater than the throat diameter. The sleeve is insertable in the nozzle throat by flexing the tab members so that the first portions clear the throat and so that the frangible portions of the tab members are disposed in the throat. The tab members, in combination, have an inner diameter which is substantially equal to the inner diameter of the body portion of the sleeve.
    Type: Grant
    Filed: October 26, 1987
    Date of Patent: April 16, 1991
    Assignee: Morton Thiokol, Inc.
    Inventors: Robert I. Myers, Bryce D. Brubaker, Robert E. Overall