Patents by Inventor Clayton C. Gnagy

Clayton C. Gnagy 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: 5119535
    Abstract: A fluid such as a fluidized bed or a molten bath, is heated to a temperature sufficiently high to soften a substantially rigid body of material and sufficiently low to avoid damage to the material. While maintaining the fluid at this temperature, the body is immersed in the fluid to heat the body uniformly. Pressure is applied to the heated body to form it into a desired three-dimensional configuration. The heated body is removed from the fluid either before, after, and/or while the pressure is applied. The body is allowed to cool and harden into its desired configuration. The body is preferably formed between a flexible member and a mold surface. The method may be used to form various types of material, including honeycomb core, laminated sheets of plastic, plastic tubing, and titanium. The body may be precut and indexed and secured to a mold which is immersed in the fluid with the body.
    Type: Grant
    Filed: September 18, 1989
    Date of Patent: June 9, 1992
    Assignee: The Boeing Company
    Inventors: Clayton C. Gnagy, William L. Rodman, Ralph R. Welsh
  • Patent number: 4495764
    Abstract: An integrated three-component insulation wall assembly which can be used by itself as an insulation wall assembly, or which can be incorporated into a solid rocket motor case that is made of material fabricated using conventional layup construction methods, or which can provide the contour stability necessary to allow its functioning as a mandrel for filament-winding a solid rocket motor case, and which can be spliced and reinforced across the splice. The insulation wall assembly comprises, in an integrated condition, an inner wall component (i.e., a flame side wall component) which is laminated from woven reinforcements in an ablative matrix, a middle wall component of non-metallic honeycomb core material, and an outer wall (i.e., a pressure side wall component). The inner wall component provides a fire barrier; the middle wall component provides thermal insulation; and the outer wall component provides structural stability.
    Type: Grant
    Filed: May 26, 1983
    Date of Patent: January 29, 1985
    Assignee: The United States of America as represented by the Secretary of the Air Force
    Inventor: Clayton C. Gnagy