Patents by Inventor Gregg H. Wilson

Gregg H. Wilson 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).

  • Publication number: 20240051019
    Abstract: A green body part comprises a first green portion, a second green portion, an interfacial joint between the first green portion and the second green portion, and a joint material disposed within the interfacial joint. The joint material comprises a powder having a particle size distribution than or equal to 1 ?m and less than or equal to 50 ?m. A method of manufacturing a joined part includes applying a joint material on a face of the first green portion and contacting the second green portion to the joint material on the face of the first green portion to form a joined green body part.
    Type: Application
    Filed: July 17, 2023
    Publication date: February 15, 2024
    Applicant: General Electric Company
    Inventors: Arunkumar Natarajan, Kwok Pong Chan, William C. Alberts, Sivaruban Shivanathan, Elliot C. Dilger, Gregg H. Wilson
  • Patent number: 6367240
    Abstract: Air collecting manifold for a gas turbine engine including a plurality of arcuate pipe segments surrounding a compressor casing receives air from a system of feed tubes incorporating spherical ball joints to allow for differential thermal growth and limit transmission of vibration from one component of the manifold structure to another.
    Type: Grant
    Filed: December 16, 1998
    Date of Patent: April 9, 2002
    Assignee: General Electric Company
    Inventors: James C. Hoyer, Gregg H. Wilson, Ronald C. Beatty
  • Patent number: 5320307
    Abstract: An aircraft engine thrust mount includes a pair of spaced apart thrust links pivotally joined at one end to an engine first frame and at opposite ends to a lever. A platform is fixedly joined to an aircraft pylon and includes first and second spaced apart clevises and a center clevis therebetween. The center clevis is pivotally joined to a center of the lever for carrying thrust force from the first frame through both thrust links and to the platform and pylon during normal operation. A pair of pins pivotally join the thrust links to the lever and extend through apertures in the platform first and second clevises to define predetermined gaps therebetween for allowing the lever to rotate relative to the platform center clevis up to a predetermined angular rotation. In a failure mode of operation the pins contact the platform first and second clevises for transmitting thereto either tension or compression thrust loads for providing an alternate failsafe loadpath.
    Type: Grant
    Filed: March 25, 1992
    Date of Patent: June 14, 1994
    Assignee: General Electric Company
    Inventors: Hahn M. Spofford, Thomas G. Wakeman, Donald L. Bellia, Thomas P. Joseph, Gregg H. Wilson, James E. Cencula, Frederick W. Tegarden, Michael H. Schneider