Patents Examined by John T. Niebling
  • Patent number: 5078843
    Abstract: A carbon composite tensile test specimen for high temperature testing and a method of fabricating the same are disclosed. A plurality of holes are drilled in first and second end sections of the specimen and then the end sections are electroplated with nickel. The nickel plating of the end sections prevents breakage of the ends in the jaws of a tensile testing apparatus. For high-temperature testing, a standard-sized specimen may be used with the jaws in the hot zone.
    Type: Grant
    Filed: June 13, 1989
    Date of Patent: January 7, 1992
    Assignee: General Dynamics Corporation Air Defense Systems Division
    Inventor: Wilson N. Pratt