Rocket Fuel Core Patents (Class 425/DIG43)
  • Patent number: 5714081
    Abstract: A dismountable mechanical core (1) includes a counterform (2) attached to a central mandrel (3,8), the counterform components being able to be handled remotely and with complete safety. These components of the counterform are connected and attached to the central mandrel (3,8) by rod anchoring devices (6). The process of assembly and disassembly of the core is also described. This dismountable mechanical core is used for the molding of the cavity inside the charge of solid rocket fuel.
    Type: Grant
    Filed: June 25, 1996
    Date of Patent: February 3, 1998
    Assignee: Societe Nationale des Poudres et Explosifs
    Inventors: Jean-Francois Tillac, Jean-Pierre Hoguet, Alain Soulignac
  • Patent number: 5310159
    Abstract: Destructible cores useful particularly for shaping the internal channels of cast propellant blocks. The cores include at least one elongated element which is shaped, for example by winding, the cohesion of which is ensured by way of a joining material and a portion of which is accessible from the exterior of the component to be cast. In order to obtain quickly cores having a high rigidity, the shaped element is a band which includes interlaced wires having free spaces, the joining material filling the free spaces.
    Type: Grant
    Filed: July 26, 1991
    Date of Patent: May 10, 1994
    Assignee: Societe Nationale des Poudres et Explosifs
    Inventors: Andre Hiss, Jean-Michel Tauzia
  • Patent number: 4836961
    Abstract: A method of and apparatus for casting uncured solid propellant in solid propellant rocket motors includes a casting bayonet having annular slits formed in the exit end thereof that improve the fluidity and self-leveling behavior of the uncured propellant. Both of these effects eliminate or reduce the trapping of air in the cast propellant, thus providing a better product.
    Type: Grant
    Filed: January 2, 1987
    Date of Patent: June 6, 1989
    Assignee: Morton Thiokol, Inc.
    Inventors: Richard E. Morgan, Charles B. Dye
  • Patent number: 4380186
    Abstract: For the fabrication of pipeless explosive and/or propellant charges there is provided an insulation sleeve, whose radial thermal conductivity or heat transmission, at a random cross-section, essentially corresponds to the quantity of heat which radially flows out at such location and is released as a result of the solidification of the melt. By means of the insulation sleeve there is produced a pipeless casting without any subsequent supply of external or separate energy, e.g. electrical heating and so forth, even if the cast or molded article has very small pour openings. The required thermal conductivity or heat transmission in the insulation sleeve can be adapted to the thermal conditions of the cast article by employing insulating elements or parts and/or hollow spaces or chambers with heat carriers, e.g. melt. Corresponding casting methods are predicated upon a carefully directed preheating and stepwise cooling of the cast article and the insulation sleeve.
    Type: Grant
    Filed: August 31, 1981
    Date of Patent: April 19, 1983
    Assignee: Schweizerische Eidgenossenschaft, represented by Eidg. Munitionsfabrik Thun der Gruppe fur Rustungsdienste
    Inventor: Richard Buhrer
  • Patent number: 4106744
    Abstract: A process for producing mass filters for use in mass spectrometers. Several electrodes having precisely shaped surfaces must be held in precisely determined positions with respect to each other. Insulators are placed into position on the surface of a mandrel and a layer of metal is deposited over the mandrel and insulators to form a composite unitary structure, including the electrodes. The deposited metal overlying the insulators is then removed, electrically isolating the electrodes.
    Type: Grant
    Filed: February 14, 1977
    Date of Patent: August 15, 1978
    Assignee: Analog Technology Corporation
    Inventors: James L. Lawrence, Jr., Robert A. Holzl, Frederick P. Pickett