Patents Assigned to General Dynamics Corporation, Air Defense Systems Division
  • Patent number: 5206450
    Abstract: An exhaust gas management system for missile launch arrangements which incorporates multiple launch cells exhausting into a common plenum. The system provides a flow passage configuration with a transition section that permits rocket exhaust flow gas to expand to fill the channel area downstream of the nozzle exit. Automatic aft closure members are included which serve to close off the flow passages to inactive cells while providing an open passage for exhaust gases from an active cell undergoing a missile firing. This arrangement prevents back flow or recirculation of exhaust gases into the volume in the cell which is upstream of the rocket nozzle exit.
    Type: Grant
    Filed: May 13, 1991
    Date of Patent: April 27, 1993
    Assignee: General Dynamics Corporation Air Defense Systems Division
    Inventor: Edward T. Piesik
  • Patent number: 5171693
    Abstract: A method is presented for the accurate quantitative determination of amounts of reactive (water and ethanol) and non-reactive N-methyl-2-pyrrolidone (NMP) volatiles in graphite-polyimide prepreg samples. The method is also applicable to other condensation-curing and/or solvent-impregnated prepreg systems, regardless of the type of reinforcement. Prepreg samples are heated in a containment chamber and the volatiles are subsequently flushed from the chamber with dry nitrogen gas. The volatiles are condensed, weighed, and analyzed via gas chromatography to determine the volatile composition. The method offers a means of purging the extremely tightly held, relatively non-volatile NMP solvent from the resin matrix by means of high temperatures applied to the sample chamber. The higher volatility reaction products are also captured by means of the specially designed very low temperature condenser. An internal check (collection efficiency) on the accuracy of the results is included in the test method.
    Type: Grant
    Filed: July 5, 1991
    Date of Patent: December 15, 1992
    Assignee: General Dynamics Corporation Air Defense Systems Division
    Inventors: Sean A. Johnson, Nancy K. Roberts
  • Patent number: 5159241
    Abstract: A relativistic magnetron device comprising an elongate cathode shank extending along the axis of the device and a cylindrical anode surrounding the cathode shank along at least part of its length to define an annular interaction area. The anode has an even number of resonator cavities facing the cathode, and microwave extraction devices are connected to alternate resonator cavities to extract power from the device. The cathode has a central, emission band extending from the center of the interaction area in opposite directions and terminating short of the ends of the anode, while the remainder of the cathode is non-emitting.
    Type: Grant
    Filed: October 25, 1990
    Date of Patent: October 27, 1992
    Assignee: General Dynamics Corporation Air Defense Systems Division
    Inventors: Keith G. Kato, James C. Weatherall
  • Patent number: 5136922
    Abstract: An exhaust gas management system for missile launch arrangements having multiple launch cells exhausting into a common plenum includes automatic aft closure members which serve to close off the flow passages to inactive cells while providing an open passage for exhaust gases from an active cell undergoing a missile firing. This arrangement prevents back flow or recirculation of exhaust gases into the volume in the cell which is upstream of the rocket nozzle exit.
    Type: Grant
    Filed: May 13, 1991
    Date of Patent: August 11, 1992
    Assignee: General Dynamics Corporation, Air Defense Systems Division
    Inventor: Edward T. Piesik
  • Patent number: 5114469
    Abstract: A process for producing high-strength, substantially nonporous alloys by means of a three-component mixture, including admixing a first component of one or more low-melting temperature metals or alloys thereof, a second component of one or more high-melting temperature metals or alloys thereof, and a substantially inert third component of one or more refractory compounds, subjecting the mixture to changes in temperature so as to form a mixture capable of being shaped at a temperature well below the melting or decomposition temperature of the highest melting metal and the inert refractory compound.
    Type: Grant
    Filed: December 10, 1987
    Date of Patent: May 19, 1992
    Assignee: General Dynamics Corporation Air Defense Systems Division
    Inventor: Sam M. Weiman
  • 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
  • Patent number: 5027062
    Abstract: A method for manufacturing a probe test structure for microcircuits utilizes a multiple coating method in conjunction with a novel double-cell electroplating apparatus having a relatively high-resistance ion path between the cells. Photoresist is applied to both sides of a copper foil, copper posts are electroformed onto selected areas of one side of the foil through image hole patterns, the remaining photoresist is stripped away, polyimide prepreg is laminated to the post side of the foil, the copper posts are exposed by sanding, photoresist is reapplied to both sides of the sanded remainder, additional copper is electroformed on each post through image hole patterns in the post side of the photoresist, the foil on the side opposite the posts is chemically milled to provide leads integral with each post using appropriate masking techniques and, finally, all of the remaining photoresist is removed to leave the desired test probe set.
    Type: Grant
    Filed: June 12, 1989
    Date of Patent: June 25, 1991
    Assignee: General Dynamics Corporation, Air Defense Systems Division
    Inventors: William P. Dugan, Marvin R. Johnson
  • Patent number: 4986186
    Abstract: A notched cartridge or casing is provided to mitigate the shock damage to a gun barrel or firing chamber when a cartridge with large amounts of explosive or propellant is fired. The cartridge or casing comprising a generally cylindrical shell with an open top end and a closed base is provided with an annular area near the base and a circular area on the base which have reduced wall thicknesses compared to the rest of the cartridge. The annular and circular areas have external surfaces which are inwardly displaced with respect to the outer surface of the remainder of the cartridge. Upon firing of the cartridge, the areas of reduced wall thickness expand outwardly and are plastically deformed without touching the barrel or firing chamber. Damage to the barrel and/or breech is prevented and the cartridge is easily removed for reloading of the gun system.
    Type: Grant
    Filed: November 1, 1988
    Date of Patent: January 22, 1991
    Assignee: General Dynamics Corporation Air Defense Systems Division, Pomona Facility
    Inventors: Edward W. LaRocca, Norman H. Andersson