Patents by Inventor Charles H. Gay, Jr.

Charles H. Gay, Jr. 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: 4526509
    Abstract: A seal structure between first and second relatively moveable members for preventing gas flow in the space between the members and transverse to their general direction of motion is disclosed. The seal structure includes a plurality of substantially parallel strips within 30.degree. of normal to the radial plane generally containing these first and second relatively moveable members. The strips are thin and closely spaced and arranged so that one strip edge is attached to the first member and another edge is free to resiliently deflect when in rubbing contact with the second member.
    Type: Grant
    Filed: August 26, 1983
    Date of Patent: July 2, 1985
    Assignee: General Electric Company
    Inventors: Charles H. Gay, Jr., Dean T. Lenahan
  • Patent number: 4411597
    Abstract: A replaceable tip cap for attachment to the end of a rotor blade. The tip cap includes a plurality of walls defining a compartment which, if desired, can be divided into a plurality of subcompartments. The tip cap can include inlet and outlet holes in walls thereof to permit fluid communication of a cooling fluid therethrough. Abrasive material can be attached with the radially outer wall of the tip cap.
    Type: Grant
    Filed: March 20, 1981
    Date of Patent: October 25, 1983
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: William K. Koffel, Eugene N. Tuley, Charles H. Gay, Jr., Raymond E. Troeger, Albert P. Sterman, deceased
  • Patent number: 4289447
    Abstract: A turbine shroud includes a ceramic sealing layer secured to a metal substrate. In one form, the metal substrate includes a plurality of pegs extending therefrom. Intermediate bonding layers are disposed on the peg-metal substrate structure. A ceramic sealing layer of zirconium oxide with about 20 weight percentage magnesium oxide is disposed, e.g., plasma sprayed, on the intermediate bonding layers. The ceramic sealing layer includes an ordered pattern of very fine cracks therein which reduce the thermal stress in the ceramic sealing layer. A method of constructing a turbine shroud structure is also disclosed.
    Type: Grant
    Filed: October 12, 1979
    Date of Patent: September 15, 1981
    Assignee: General Electric Company
    Inventors: Albert P. Sterman, Charles H. Gay, Jr., Frederick W. Tegarden, Dean T. Lenahan, Martin C. Hemsworth
  • Patent number: 4097194
    Abstract: A rotatable disc comprising a plurality of generally parallel plates tightly joined together for rotation about a hub. Each plate is provided with a plurality of angularly spaced lands projecting from a face thereof, the lands of each plate interposed in alternating relationship between the lands of the next adjacent plate. In this manner, circumferential displacement of adjacent sectors in any one plate is prevented in the event that a crack develops therein. Each plate is redundantly sized such that, in event of structural failure of one plate, the remaining plates can support a proportionate share of the load of the failed plate. In one embodiment, the plates are prevented from separating laterally through the inclusion of generally radially extending splines which are inserted to interlock cooperating, circumferentially adjacent lands.
    Type: Grant
    Filed: March 22, 1976
    Date of Patent: June 27, 1978
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: William N. Barack, Charles H. Gay, Jr., Stephen W. Beekman, Paul A. Domas