Patents by Inventor Gerald W. Tyree

Gerald W. Tyree 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: 4979281
    Abstract: The invention is a flush head fastener for joining two or more structural elements together. The structural elements have a fasterner hole therein with one of the structural elements being countersunk to accommodate the head of the fastener. The fastener includes head and shank portions and a layer of material joined to the top of the head of the fastener which can readily be deformed to fill any gaps between the head and the countersink. Thereafter, the excess material can be removed leaving an aerodynamically smooth surface. The surface also will have no electrical discontinuities. The procedure for installing the fastener includes the steps of (1) providing two or more structural elements having a countersunk fastener hole therein (2) thereafter the fastener is installed in the hole (3) the layer of material is deformed so as to fill any gaps between the head of the fastener and the countersink, and (4) thereafter, excess material is removed leaving a smooth external surface.
    Type: Grant
    Filed: February 8, 1989
    Date of Patent: December 25, 1990
    Assignee: Lockheed Corporation
    Inventors: Charles R. Smith, Anthony E. Brindisi, Gerald W. Tyree
  • Patent number: 4958743
    Abstract: The invention is a close out fitting for installing in a structural element, the structural element having a port extending from a first surface to a second surface thereof, the port countersunk at both ends, and a method of installing the closeout fitting. In detail, the fitting comprises a hollow, tubular sleeve having a flared first end, a flarable second end and internal threads therebetween. The fitting further comprises a plug having a head portion and a shank portion attached to the head portion with the shank portion having external threads.
    Type: Grant
    Filed: May 18, 1989
    Date of Patent: September 25, 1990
    Inventors: Randall C. Hatton, Gerald W. Tyree
  • Patent number: 4884929
    Abstract: The invention is a flush head fastener for joining two or more structural elements together. The structural elements have a fastener hole therein with one of the structural elements being countersunk to accommodate the head of the fastener. The fastener includes head and shank portions and a layer of material joined to the top of the head of the fastener which can readily be deformed to fill any gaps between the head and the countersink. Thereafter, the excess material can be removed leaving an aerodynamically smooth surface. The surface also will have no electrical discontinuities. The procedure for installing the fastener includes the steps of (1) providing two or more structural elements having a countersunk fastener hole therein (2) thereafter the fastener is installed in the hole (3) the layer of material is deformed so as to fill any gaps between the head of the fastener and the countersink, and (4) thereafter, excess material is removed leaving a smooth external surface.
    Type: Grant
    Filed: December 21, 1987
    Date of Patent: December 5, 1989
    Assignee: Lockheed Corporation
    Inventors: Charles R. Smith, Anthony E. Brindisi, Gerald W. Tyree
  • Patent number: 4088053
    Abstract: An assemblage of a rivet for securing at least a pair of sheets or other members, wherein the rivet is formed with a cavity in its upset end of predetermined dimensions with respect to the sheets and the remainder of the rivet. The cavity preferably terminates in the thickness of the bottom sheet, thus facilitating rivet upset while providing maximum strength.
    Type: Grant
    Filed: February 26, 1975
    Date of Patent: May 9, 1978
    Assignee: Lockheed Aircraft Corporation
    Inventor: Gerald W. Tyree
  • Patent number: 4007540
    Abstract: An assemblage of a rivet for securing at least a pair of sheets or other members, wherein the rivet is formed with a cavity in its upset end of predetermined dimensions with respect to the sheets and the remainder of the rivet. The cavity preferably terminates in the thickness of the bottom sheet, thus facilitating rivet upset while providing maximum strength.
    Type: Grant
    Filed: March 3, 1975
    Date of Patent: February 15, 1977
    Assignee: Lockheed Aircraft Corporation
    Inventor: Gerald W. Tyree