Patents by Inventor Jeremiah E. Halley

Jeremiah E. Halley 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: 6910616
    Abstract: A method of constructing a preform for use in forming a machined structural assembly is provided. The method includes determining the dimensions of the machined structural assembly. First and second structural members are selected based on the predetermined dimensions of the machined structural assembly. The first structural member is positioned adjacent the second structural member so as to define at least two contact surfaces. The contact surfaces of the first and second structural members are friction welded to construct the preform such that the preform has dimensions approximating the dimensions of the machined structural assembly to thereby reduce material waste when forming the machined structural assembly. A machined structural assembly having predetermined dimensions is formed from the preform by machining away excess material.
    Type: Grant
    Filed: March 7, 2002
    Date of Patent: June 28, 2005
    Assignee: The Boeing Company
    Inventors: Jeremiah E. Halley, Kevin T. Slattery
  • Publication number: 20040094604
    Abstract: A method of constructing a preform for use in forming a machined structural assembly is provided. The method includes determining the dimensions of the machined structural assembly. First and second structural members are selected based on the predetermined dimensions of the machined structural assembly. The first structural member is positioned adjacent the second structural member so as to define at least two contact surfaces. The contact surfaces of the first and second structural members are friction welded to construct the preform such that the preform has dimensions approximating the dimensions of the machined structural assembly to thereby reduce material waste when forming the machined structural assembly. A machined structural assembly having predetermined dimensions is formed from the preform by machining away excess material.
    Type: Application
    Filed: July 2, 2003
    Publication date: May 20, 2004
    Applicant: The Boeing Company
    Inventors: Jeremiah E. Halley, Kevin T. Slattery
  • Publication number: 20040004108
    Abstract: A method of constructing a preform for use in forming a machined structural assembly is provided. The method includes determining the dimensions of the machined structural assembly. First and second structural members are selected based on the predetermined dimensions of the machined structural assembly. The first structural member is positioned adjacent the second structural member so as to define at least two contact surfaces. The contact surfaces of the first and second structural members are friction welded to construct the preform such that the preform has dimensions approximating the dimensions of the machined structural assembly to thereby reduce material waste when forming the machined structural assembly. A machined structural assembly having predetermined dimensions is formed from the preform by machining away excess material.
    Type: Application
    Filed: July 2, 2003
    Publication date: January 8, 2004
    Applicant: The Boeing Company
    Inventors: Jeremiah E. Halley, Kevin T. Slattery
  • Publication number: 20030168494
    Abstract: A method of constructing a preform for use in forming a machined structural assembly is provided. The method includes determining the dimensions of the machined structural assembly. First and second structural members are selected based on the predetermined dimensions of the machined structural assembly. The first structural member is positioned adjacent the second structural member so as to define at least two contact surfaces. The contact surfaces of the first and second structural members are friction welded to construct the preform such that the preform has dimensions approximating the dimensions of the machined structural assembly to thereby reduce material waste when forming the machined structural assembly. A machined structural assembly having predetermined dimensions is formed from the preform by machining away excess material.
    Type: Application
    Filed: March 7, 2002
    Publication date: September 11, 2003
    Applicant: The Boeing Company
    Inventors: Jeremiah E. Halley, Kevin T. Slattery
  • Patent number: 6379090
    Abstract: A force balanced irregular pitch reamer is provided that is particularly well suited for precision operations requiring small tolerances. More specifically, a reamer is provided having a shank, a body portion, and a plurality of cutting teeth extending outwardly therefrom. The teeth are spaced at non-uniform intervals around the body portion, wherein each tooth includes a cutting surface and rake face, and defines a rake angle between the rake face and an imaginary line extending from the central or longitudinal axis of the reamer to the cutting surface. In operation, the reamer is rotated about its central axis and is plunged into a formed hole sized slightly smaller than the reamer such that the reamer engages the workpiece and produces a smooth finished hole. Each tooth generates a cutting force with determinable magnitude and direction to define cutting force vectors.
    Type: Grant
    Filed: June 30, 2000
    Date of Patent: April 30, 2002
    Assignees: The Boeing Company, Washington University
    Inventors: Jeremiah E. Halley, Jeffery J. Luner, Keith Young, Philip V. Bayly