Patents by Inventor William J. Arbegast

William J. Arbegast 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: 6986452
    Abstract: The present invention provides an improved method and apparatus for joining aluminum allow panels (eg. 2090-T83 aluminum lithium alloy). The method preliminarily positions two panels and skin panels next to each other so that a stringer panel overlaps a skin panel. A friction stir weld pin tool penetrates through one panel and at least partially into another panel. The panel material around the pin tool is frictionally heated, plasticized and joined until the faying surface is substantially consumed. In another embodiment, a tee-shaped structure is formed using friction stir welding to join three panels together. A projecting part of one panel (center, vertical) provides material that becomes a contoured corner panel below two side, horizontal panels after friction stir welding is completed (FIGS.
    Type: Grant
    Filed: May 15, 2003
    Date of Patent: January 17, 2006
    Assignee: Lockheed Martin Corporation
    Inventors: Brian J. Dracup, William J. Arbegast
  • Patent number: 6779707
    Abstract: The present invention provides an improved method and apparatus for joining aluminum allow panels (eg. 2090-T83 aluminum lithium alloy). The method preliminarily positions two panels and skin panels next to each other so that a stringer panel overlaps a skin panel. A friction stir weld pin tool penetrates through one panel and at least partially into another panel. The panel material around the pin tool is frictionally heated.
    Type: Grant
    Filed: August 12, 2002
    Date of Patent: August 24, 2004
    Assignee: Lockheed Martin Corporation
    Inventors: Brian J. Dracup, William J. Arbegast
  • Publication number: 20040050907
    Abstract: The present invention provides an improved method and apparatus for joining aluminum allow panels (eg. 2090-T83 aluminum lithium alloy). The method preliminarily positions two panels and skin panels next to each other so that a stringer panel overlaps a skin panel. A friction stir weld pin tool penetrates through one panel and at least partially into another panel. The panel material around the pin tool is frictionally heated, plasticized and joined until the faying surface is substantially consumed. In another embodiment, a tee-shaped structure is formed using friction stir welding to join three panels together.
    Type: Application
    Filed: May 15, 2003
    Publication date: March 18, 2004
    Inventors: Brian J. Dracup, William J. Arbegast
  • Publication number: 20030116609
    Abstract: The present invention provides an improved method and apparatus for joining aluminum allow panels (eg. 2090-T83 aluminum lithium alloy). The method preliminarily positions two panels and skin panels next to each other so that a stringer panel overlaps a skin panel. A friction stir weld pin tool penetrates through one panel and at least partially into another panel. The panel material around the pin tool is frictionally heated.
    Type: Application
    Filed: August 12, 2002
    Publication date: June 26, 2003
    Inventors: Brian J. Dracup, William J. Arbegast
  • Patent number: 6543671
    Abstract: A friction stir welding tool includes a body having an upper surface defining an entrance opening and a lower surface, and a pin having a lower surface defining an exit opening, wherein the pin extends from the lower surface of the body. The friction stir welding tool further includes a passageway defined by the body and the pin from the entrance opening to the exit opening and is capable of allowing a filler material to pass therethrough. A friction stir welding method includes applying a frictional heating source to a workpiece to plasticize a volume of the workpiece and applying the frictional heating source to a filler material to plasticize the filler material. The method further includes introducing the filler material into the volume of the workpiece and incorporating the filler material into the volume of the workpiece.
    Type: Grant
    Filed: September 5, 2001
    Date of Patent: April 8, 2003
    Assignee: Lockheed Martin Corporation
    Inventors: Timothy E. Hatten, William J. Arbegast
  • Publication number: 20030042292
    Abstract: A friction stir welding tool includes a body having an upper surface defining an entrance opening and a lower surface, and a pin having a lower surface defining an exit opening, wherein the pin extends from the lower surface of the body. The friction stir welding tool further includes a passageway defined by the body and the pin from the entrance opening to the exit opening and is capable of allowing a filler material to pass therethrough. A friction stir welding method includes applying a frictional heating source to a workpiece to plasticize a volume of the workpiece and applying the frictional heating source to to a filler material to plasticize the filler material. The method further includes introducing the filler material into the volume of the workpiece and incorporating the filler material into the volume of the workpiece.
    Type: Application
    Filed: September 5, 2001
    Publication date: March 6, 2003
    Inventors: Timothy E. Hatten, William J. Arbegast
  • Patent number: 6230957
    Abstract: A method of using friction stir welding to repair weld defects and to help avoid weld defects in intersecting welds and crack-sensitive material, such as 2195 Al—Cu—Li. Intersecting fusion welds in 2195 Al—Cu—Li have shown a propensity to crack both during welding and during proof testing. These cracks have generally been associated with a particular metallurgical structure present in the fusion zone ofVPPA/SPA weldments. HYBRID Friction Stir Overwelding of the initial VPPA/SPA weld from the penetration side is shown to convert the cast microstructure of these VPPA/SPA weldments into a fine grained, dynamically recrystallized microstructure showing higher strength, ductility, toughness, and resistance to intersection weld cracking.
    Type: Grant
    Filed: March 5, 1999
    Date of Patent: May 15, 2001
    Assignee: Lockheed Martin Corporation
    Inventors: William J. Arbegast, Paula J. Hartley
  • Patent number: 5120175
    Abstract: A fastener having an elongated shank formed of a shape memory alloy, a head at the upper end of the shank, and an annular segment at the lower end of said shank having a deformed cross-sectional shape suitable for insertion into an opening extending through adjacent workpieces. The annular segment has a frusto-conical trained shape that is larger than this opening. The annular segment radially flares from the deformed shape to an approximation of the trained shape when heated above a critical transformation temperature, thereby securing the fastener in place with respect to the workpieces. Alternatively, a sleeve made of a different material (e.g. aluminum) extending over a portion or the entire length of the fastener can be added for improved deformational characteristics, by providing the same frusto-conical shape through axial contraction of the shank.
    Type: Grant
    Filed: July 15, 1991
    Date of Patent: June 9, 1992
    Inventors: William J. Arbegast, Joseph H. Armstrong, Brian J. Maclean