Patents Assigned to General Dynamics
  • Patent number: 5114101
    Abstract: A modular distributed concentrating collector using a low loss power bus to route solar radiation collected from a plurality of concentrating and collecting dishes to a centralized converted for conversion into electricity in space. The power bus may utilize fiber optic bundles. The collector includes a plurality of adjustable solar collectors to provide optimum tracking of the sun. The arrangement can be folded for stowing in the payload bay of the Space Shuttle or other launch vehicle for transport to a location in space.
    Type: Grant
    Filed: January 22, 1991
    Date of Patent: May 19, 1992
    Assignee: General Dynamics Corporation/Space Systems Division
    Inventors: Theodore G. Stern, Mickey Cornwall
  • Patent number: 5112663
    Abstract: A method of making a composite structure, such as an aircraft wing, which has a foam core and at least one outer layer of fiber reinforced resin material. A shaped foam core is prepared by compressing a rigid, closed-cell foam to the desired shape in a closed mold under heat and pressure. A sheet of flexible open-cell foam is impregnated with a thermosetting resin. A sheet of dry fiber reinforcement material is placed on one or both sides of the impregnated foam sheet. The resulting sandwich is wrapped around the foam core and the assembly is placed in a corresponding tool cavity. The tool is heated to the curing temperature of the impregnating resin. As the temperature rises, the foam core expands, exerting pressure on the impregnated foam sheet, forcing resin into the fiber reinforcement, wetting all the fibers and forcing air out of the material. As the resin cures, void-free, strong skins are formed integral with the core foam.
    Type: Grant
    Filed: April 22, 1991
    Date of Patent: May 12, 1992
    Assignee: General Dynamics Corporation, Convair Division
    Inventors: Paul W. Morenz, Charles E. Knox
  • Patent number: 5113244
    Abstract: The fiber optic combiner/splitter is a positive and negative axicon combination which can convert a ring-shaped beam into a solid beam. The positive half of the axicon is effectively a plano-convex lens where the convex surface is generally a shallow cone. The flat surface of the lens abuts each end of an array of single mode fibers which are arranged in a ring configuration around a support member. The negative half of the axicon is effectively a plano-concave lens which is complementary to the positive lens. The focused beams from the positive half of the axicon are combined to form a single beam which is then directed into a single optical fiber. For conversions in the reverse direction, light is taken from a single multimode fiber and expanded into a ring-like pattern. The ring of light is picked up by the ring of single mode fibers. Each single mode fiber receives an equal amount of optical energy or power to provide good efficiency in splitting of the multiplexed beam.
    Type: Grant
    Filed: February 6, 1991
    Date of Patent: May 12, 1992
    Assignee: General Dynamics Corporation, Electronics Division
    Inventor: Mark E. Curran
  • Patent number: 5111525
    Abstract: An improved optical fiber suitable for use as a distributed sensor of variations in either hydrostatic pressure or temperature having two substantially hemi-cylindrical optical glass cores, the first said core having a first index of refraction and the second said core having a second index of refraction, separated by a layer of optical glass having a third index of refraction, and an outer optical glass sheath having a fourth index of refraction. The split-core optical fiber can be fabricated so that cross-talk between the two halves of the split-core is a function of hydrostatic pressure or of temperature variations.
    Type: Grant
    Filed: October 15, 1990
    Date of Patent: May 5, 1992
    Assignee: General Dynamics Corporation
    Inventor: Edward Hartouni
  • Patent number: 5108928
    Abstract: A method and equipment for making a chemical analysis of a sample enables multiple analyses to be conducted simultaneously. The system includes a number of injection valves connected in series to a sample inlet line. Each injection valve is connected in a parallel to a separate detection unit. Each injection valve is connected to a pressurized source such as a solvent pump. This equipment includes a sample preparation unit which injects the sample to flow through each of the valves. Each of the valves will retain a portion of the sample in a sample chamber. Each valve will rotate to an injecting position wherein the pressurized solvent pushes the sample into the separate detection units.
    Type: Grant
    Filed: November 13, 1989
    Date of Patent: April 28, 1992
    Assignee: General Dynamics Corporation
    Inventors: Kevin P. Menard, H. Randy O'Neal
  • Patent number: 5107129
    Abstract: In one embodiment a bundle of optic fibers of different lengths are inserted through the case wall of a solid fuel or a hybrid rocket motor and extends through the wall of the fuel grain to the edge of the bore in center thereof. As the grain burns in a normal manner, from the center toward the outer periphery of the case, the bright flame of ignition is seen at the end of the fiber optic fiber adjacent to the flame. The length of each fiber in the bundle is used to determine the burn rate and amount of grain left to ignite. In another embodiment different length fibers of a bundle are looped into the grain and back to the exterior of the case and light emitting diodes are positioned at one end of each fiber with a light-detecting means at the other end. The light through the diodes is monitored to detect a no-light condition which exists when a fiber is destroyed by the burn. In yet another embodiment a single optic fiber is used with a light source and a light reception means at one end.
    Type: Grant
    Filed: June 4, 1990
    Date of Patent: April 21, 1992
    Assignee: General Dynamics Corporation/Space Systems Division
    Inventor: Peter C. Lombrozo
  • Patent number: 5104061
    Abstract: A dual eccentric bearing system for precise adjustment of wing incidence and dihedral. The bearing system is utilized in the attachment of wings that vary the sweep by rotation about a pivot fixedly located on an aircraft fuselage through an interconnecting wing pivot pin. The top portion of the pivot pin is supported by the dual eccentric bearing system and the bottom by a non-eccentric bearing system. The eccentric bearing system has both an eccentric ball retaining ring free to rotate relative to its fuselage attachment and a ball contained within the ring which includes an eccentric pivot pin receiving aperture free to rotate within the ring containment. The bottom end of the pin is supported by a conventional non-eccentric bearing system with the ring fixedly held in position by its fuselage connection. The ball of the non-eccentric bearing has a similar pin receiving aperture with the ball free to rotate angularly relative to the ring.
    Type: Grant
    Filed: May 25, 1990
    Date of Patent: April 14, 1992
    Assignee: General Dynamics Corporation, Convair Division
    Inventor: William J. Doane
  • Patent number: 5102072
    Abstract: An adaptive gain and phase controller for an autopilot for a flight vehicle, such as a hypersonic glide vehicle, that includes applying a reference excitation signal to the control system of a flight vehicle, measuring the response of the vehicle to that excitation signal, namely the gain and phase losses through airframe, and making adjustments to the gain and phase inputs to the autopilot based on those measurements. A high gain narrow bandpass filter is incorporated so that the test signal can be extracted from the airframe of the flight vehicle.
    Type: Grant
    Filed: November 19, 1990
    Date of Patent: April 7, 1992
    Assignee: General Dynamics Corporation, Convair Division
    Inventors: Murray C. Egan, Frank D. Steketee
  • Patent number: 5099645
    Abstract: A liquid-solid propulsion system having a tank of liquid oxygen and a high pressure chamber loaded with solid grain fuel with a portion of the liquid oxygen being passed through a heat exchanger to convert the liquid oxygen to gaseous oxygen. The gaseous oxygen is directed to the chamber or solid grain fuel to induce a fuel rich gas burn that is directed to a thrust chamber which also receives liquid oxygen to increase the characteristic velocity of the exhaust and thereby provide the specific impulse of the propulsion system. The gaseous oxygen is also directed to the liquid oxygen tank to pressurize the flow of liquid oxygen from the tank. Valves are interposed to control the flow of liquid and gaseous oxygen to provide the required mixture ratio in the thrust chamber for optimum specific impulse or to terminate the thrust of the propulsion system. A method for providing the liquid-solid propulsion system is also disclosed.
    Type: Grant
    Filed: June 21, 1990
    Date of Patent: March 31, 1992
    Assignee: General Dynamics Corporation, Space Systems Division
    Inventors: Alan L. Schuler, Danny R. Wiley
  • Patent number: 5096880
    Abstract: A process is described for enhancing superconductor characteristics by application of strong magnetic and/or electric fields to the constituent component materials from which ceramic superconductors are being formed and during the time that these superconductors are being synthesized. This process has particular applicability to the production of superconducting oxide ceramics such as the cuprates. The required magnetic fields are on the order of 1-10 tesla and the required electric fields are on the order of 0.1-1 MV/cm. The fields act as ordering mechanisms and induce grain orientation. The magnetic field aligns the magnetic moment of the grains. The electric field induces electric polarization in the grains and then aligns them. The superconducting structure formation occurs during the sintering, cooling and annealing phases of the fabrication process. Superconductivity is strongly affected by the oxygen stoichiometry in the lattice elemental cell. Applied electric fields cause elongation of the unit cell.
    Type: Grant
    Filed: April 20, 1990
    Date of Patent: March 17, 1992
    Assignee: General Dynamics Corp./Electronics Division
    Inventor: Theodore W. Rybka
  • Patent number: 5093553
    Abstract: An optical input apparatus (10) for use with a weld evaluation monitor (14) to determine the concentration of hydrogen in a weld arc atmosphere (62) including weld arc plasma and shield gas is disclosed as including an optical fiber bundle (16) having a single optical input (18) and a plurality of optical outputs (22). The optical fiber bundle is disposed to receive, at its optical input, electromagnetic radiation emitted from the weld arc atmosphere and, because the optical fiber bundle has an individual optical fiber path distribution that is completely randomized, to communicate proportional amount of the radiation to each of its optical outputs independent of the angular disposition of the fiber bundle.
    Type: Grant
    Filed: June 4, 1991
    Date of Patent: March 3, 1992
    Assignee: General Dynamics Land Systems, Inc.
    Inventors: Dennis N. Harvey, Rosemarie Reilly
  • Patent number: 5092222
    Abstract: A "float-up" launching system for launching missiles from submerged submarines or other submerged launchers utilizing a lightweight rigid cylindrical tube telescoped over the missile while stored in the launcher so as to not take up additional volume. On launching, the tube is extended forward of the missile by a gas generator to form a floatation chamber which creates extra buoyance forward of the missile center of gravity, but still connected to the water surface, nose upwardly, where it is disconnected and the missile booster is ignited.
    Type: Grant
    Filed: August 26, 1981
    Date of Patent: March 3, 1992
    Assignee: General Dynamics Corporation, Convair Division
    Inventor: Robert A. Lynch
  • Patent number: 5080306
    Abstract: A multi-layer blanket insulation adapted of use in an aerobrake intended to assist in the return of a space vehicle from a higher earth orbit to a low earth orbit for recovery and possible reuse. Between two face sheets of a cloth material highly resistant to elevated temperatures are interposed a layer of a flexible insulative material and a layer of non-porous foil. The insulation is stitched together into a predetermined pattern. A backside stiffener may be secured to the back face by a layer of a suitable cloth material.
    Type: Grant
    Filed: October 10, 1989
    Date of Patent: January 14, 1992
    Assignee: General Dynamics Corporation, Space Systems Division
    Inventors: John W. Porter, Neal C. White, Jeffrey D. Holdridge
  • 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: 5073072
    Abstract: The threaded split-bushing fastener assembly has been designed for high temperature applications such as on hypersonic vehicles. The fastener assembly consists of a pin (with a standard countersunk head at one end and a tapered end at the other end), a tubular threaded split-bushing, a nut, and a washer. Installation is accomplished by inserting the pin in the parts to be fastened, then slipping the washer and split-bushing on the tapered end of the pin and finally screwing the nut onto the split-bushing. Tightening of the nut allows preloading of the fastener assembly.
    Type: Grant
    Filed: February 4, 1991
    Date of Patent: December 17, 1991
    Assignee: General Dynamics Corporation/Convair Division
    Inventors: Ebrahim Parekh, Jack E. Jensen, Jeffrey L. Summers
  • Patent number: 5073224
    Abstract: A barrier injection apparatus for injecting a barrier at a site characterized by a holder for holding the apparatus in place against the force of injection; at least one injector for injecting a medium for a barrier at the injections site when in place; respective conduit system extending from the storage unit, and including a pump for inducing pressure onto the medium, to the injection site for injecting the medium at the injection site under pressure; storage unit for storing the medium at atmospheric pressure and being connected with a suction side of a pump that will introduce pressure; a second conduit connected with the barrier injection apparatus and adapted to remove unused medium from the site, an adjusting mechanism for adjusting the injectors to a correct distance; and a gasket sealingly surrounding the injection site for constraining the medium to flow into the site under pressure and insulate the medium from a holding mechanism. Also disclosed are specific preferred embodiments.
    Type: Grant
    Filed: October 26, 1989
    Date of Patent: December 17, 1991
    Assignee: General Dynamics Corporation
    Inventors: Mark K. Addison, William F. Campbell, Ralph J. Panno
  • Patent number: 5069510
    Abstract: An endless track (52) for a track laying vehicle has a construction that facilitates replacement and repair of track components as well as providing an extended lifetime of use as compared to conventional vehicle tracks. The components of the track which facilitate its construction and maintenance include a track shoe (60), a replaceable road pad (62) for the track shoe (60), a pin assembly (64) for connecting laterally aligned pairs of the track shoes (60), a hollow pin (66) of the pin assembly (64), a center guide (68) that guides the track on the associated vehicle roadwheels, an end connector (72) that connects ends of the pins (66) associated with adjacent shoe assemblies (70), and a center connector (74) that cooperates with the end connectors (72) in connecting the shoe assemblies (70).
    Type: Grant
    Filed: April 7, 1987
    Date of Patent: December 3, 1991
    Assignee: General Dynamics Land Systems, Inc.
    Inventor: Robert M. Cory
  • Patent number: 5067908
    Abstract: A self-aligning connector that is used with electrical plug-in-module connectors. The self-aligning connector has an elongated connector body with a cutout portion extending from its top surface to its bottom surface to form a walled structure that would surround an electrical contact area. A foot portion extends from each end of the connector body. Each foot portion has an inclined front surface that mates with the inclined bottom wedge surface of a wedge block. Elongated slots in the respective wedge blocks algin with vertically oriented bore holes in the foot portions and mounting screws are passed downwardly through the respective openings. As the mounting screws are tightened the wedge blocks and foot portions have relative translation along their inclined surfaces, thus aligning the connector in the cutout portion.
    Type: Grant
    Filed: November 19, 1990
    Date of Patent: November 26, 1991
    Assignee: General Dynamics Corporation, Convair Division
    Inventor: Lloyd A. Guth
  • Patent number: 5066921
    Abstract: A radome diagnostic system comprises a rotatably mounted turntable having support memebers for supporting a radome in a radome support area on the turntable, and a scanning assembly on the turntable for supporting a probe antenna in the radome support area and for translating the probe antenna in perpendicular x and y directions to cover a predetermined planar scanning area. A reference antenna is mounted on the turntable to provide a reference signal, and both the reference antenna and the probe antenna are connected to a suitable receiver for receiving signals from them and for suitably analyzing the collected data. A transmitter is located at a position remote from the turntable to direct radiation towards a radome mounted on the turntable. The probe antenna will detect radiation as degraded or modified by the effect of the presence of the radome in the radiation path. The reference antenna receives unperturbed radiation.
    Type: Grant
    Filed: August 1, 1990
    Date of Patent: November 19, 1991
    Assignee: General Dynamics, Electronics Division
    Inventors: Eugene L. Rope, Dary R. Stewart, Gus P. Tricoles, Gary L. Vance, Jonathan Roussos, Roy S. Luoma
  • Patent number: 5060365
    Abstract: A tool for installation of pin connector assemblies into a computer path board, the pin assembly being of a type that permits a locking bushing to be slid over the pin into a recess within the body of the assembly and thereby cause a tight interference fit of the assembly within a receiving orifice in the patch board. The tool includes a retainer to engage a guide groove formed on the upper portion of the pin assembly and a tubular driver that is mechanically coupled to the retainer for driving the locking bushing into position. The retainer and the tubular driver are preferably connected to opposing handles of a biased plier arrangement. The plier arrangement may be hand or machine operated.
    Type: Grant
    Filed: October 10, 1990
    Date of Patent: October 29, 1991
    Assignee: General Dynamics Corporation, Convair Division
    Inventor: Robert F. Lanzo