Patents by Inventor Everette M. Pierce

Everette M. Pierce 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: 4216039
    Abstract: The propellant compositions of this invention are crosslinked with from at 0.1 to about 1.0 weight percent of nitrocellulose which improves the physical properties and the thermal stabilities of these propellants thereby permitting their storing and testing up to 165.degree. F.
    Type: Grant
    Filed: November 20, 1978
    Date of Patent: August 5, 1980
    Assignee: The United States of America as represented by the Secretary of the Army
    Inventor: Everette M. Pierce
  • Patent number: 4209351
    Abstract: A liner composition is employed as a liner/inhibitor for a solid propellant rain while functioning as a liner-binder between the propellant grain and insulation or the motor case. The liner and inhibitor composition is prepared from the conventional binder systems (e.g., hydroxy terminated polybutadiene (HTPB), polysulfide, polyurethane, and polyester). The composition employs a cool burning oxidizer selected from oxamide and nitroguanidine. The type of solid propellant grain, particularly the crosslinking or reaction mechanism to form a chemical bond between the binder of the liner composition and the binder of the propellant, dictates the type formulation of the liner/inhibitor composition. A representative liner/inhibitor for a HTPB propellant grain contains from about 10 to about 70 weight percent oxidizer, from about 0.1 to about 1.
    Type: Grant
    Filed: June 5, 1978
    Date of Patent: June 24, 1980
    Assignee: The United States of America as represented by the Secretary of the Army
    Inventors: Everette M. Pierce, Henry C. Allen
  • Patent number: 4154633
    Abstract: An oxidizer that is soluble in a polar solvent selected from ethanol, diel ether, and acetone is used in a propellant composition mixing procedure to effect an improved dispersion of the oxidizer. The soluble oxidizer is selected from the reaction products formed by reacting together an equivalent amount of a first reactant selected from triethanol amine or diethanol amine with an equivalent amount of a second reactant perchloric acid when the soluble perchlorate salt is desired for use. The soluble oxidizer is selected from the reaction products formed by reacting together an equivalent amount of a first reactant selected from triethanol amine or diethanol amine with an equivalent amount of a second reactant nitric acid when the soluble nitrate salt is desired for use. The dissolved oxidizer is added to the binder portion of the propellant during mixing. After being widely dispersed, the soluble oxidizer and binder portion are mixed under low vacuum and mild heat (e.g., 110.degree. F. to 120.degree. F.
    Type: Grant
    Filed: April 14, 1978
    Date of Patent: May 15, 1979
    Assignee: The United States of America as represented by the Secretary of the Army
    Inventor: Everette M. Pierce