Patents by Inventor Edward J. Davert

Edward J. Davert 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: 4879875
    Abstract: A fastener driving tool for driving remotely located fasteners through preformed openings in a structure. The tool (10) comprises a housing (12) having a pneumatic-hydraulic intensifier (14) mounted thereon and a remotely located second hydraulic cylinder assembly (20) attached to the housing (12) by means of an extension tube (110). Pressurized air is provided to the tool (10) through a cartridge regulator (36) that is controlled by a trigger assembly (41). A pneumatic piston (72), connected to a first hydraulic piston (76) by a piston rod (80), moves from a first position located away from a nose portion (66) to a second position located toward a nose portion (66). The pressurizing valve (56) admits air to the pneumatic piston (72) to cause the first hydraulic piston (76) to move to the second position, thereby pressurizing hydraulic fluid (92) and causing the second hydraulic piston (102) to extend from the second cylinder housing (104).
    Type: Grant
    Filed: March 22, 1988
    Date of Patent: November 14, 1989
    Assignee: The Boeing Company
    Inventors: Edward J. Davert, Peter D. McCowin
  • Patent number: 4272890
    Abstract: A lattice template for locating aircraft structure and pilot holes behind flat or contoured surface panel structures. The lattice structure of template strips positioned by bridge structures or flexible cables enables adjustment of template strips within the lattice template thereby enabling coordination with its respective structural element to accommodate tolerances of assembly.
    Type: Grant
    Filed: November 30, 1979
    Date of Patent: June 16, 1981
    Assignee: The Boeing Company
    Inventor: Edward J. Davert
  • Patent number: 4272215
    Abstract: A surface of a wedge acts as a stop to limit travel of a spindle on an automatic riveting machine. A drive mechanism moves the wedge back and forth to vary the heighth of the wedge, and the same mechanism simultaneously moves a rod back and forth to act on a transducer, and transmit an electrical signal to give a digital readout of the change in heighth of the wedge.
    Type: Grant
    Filed: April 2, 1979
    Date of Patent: June 9, 1981
    Assignee: The Boeing Company
    Inventors: Edward J. Davert, Wilbur L. Gants