Patents Assigned to General Dynamics
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Patent number: 6205187Abstract: A programmable signal decoder processes incoming signals using any one of several predefined decoding schemes. The signal decoder is programmed to perform the desired decoding operations by downloading configuration data representative of the decoding scheme from a data memory to programmable logic in the signal decoder. Programmable metric tables provide set mapping. A generic four-level decoder structure includes two levels that are programmable Viterbi decoders, one level that is a Wagner decoder and another level that provides free bit selection operations. The four levels are combined, as needed, to implement two-dimensional, four-dimensional, multi-level and other coded modulation formats.Type: GrantFiled: December 12, 1997Date of Patent: March 20, 2001Assignee: General Dynamics Government Systems CorporationInventor: Dan L. Westfall
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Patent number: 6202534Abstract: A handling system for brass shell casings in an ammunition handling system. A shaft has a first sprocket and first hub and a non-circular gear mounted thereto, and because of the non-circular gear, rotates at a variable speed when driven by a power source. A second hub, coaxial with the shaft and rotatable independently of the shaft, has a second sprocket and a circular gear mounted thereto, and because of the circular gear, rotates at a selected speed when driven by the power source. The speed of the first sprocket varies between being equal to the speed of the second sprocket to being less than the speed of the second sprocket so that one end of a shell casing mounted on the two sprockets first lags behind the other end of the shell casing, then catches up to the other end of the shell casing.Type: GrantFiled: January 13, 1999Date of Patent: March 20, 2001Assignee: General Dynamics Armament SystemsInventors: David R. Baxter, Edward A. Prouix, Bernard A. Derry
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Patent number: 6173824Abstract: A rolling-element clutch assembly including a first race member, a second race member and a plurality of rolling elements. The first race member defines a first race surface having a first ratchet surface portion. The second race member defines a second race surface having a second ratchet surface portion. The first race surface and the second race surface define a raceway therebetween. A plurality of rolling elements are disposed in the raceway. The rolling elements provide rolling support between the first race member and the second race member when the first race member moves in a first direction relative to the second race member. At least one of the plurality of rolling elements engages the first and second ratchet surface portions when the first race member moves in a second direction relative to the second race member.Type: GrantFiled: December 7, 1998Date of Patent: January 16, 2001Assignee: General Dynamics Government Systems CorporationInventor: John Edward Roberts
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Patent number: 6170380Abstract: A system and method for selectively transferring storable units, particularly artillery propellant charge units, between a storage space and a location outside of the storage space, the system including a storage magazine having a plurality of parallel, axially elongated chambers opening at an end of the storage magazine, a shuttle having a transfer mechanism tube movable relative to the storage magazine between positions of axial alignment with each of the plurality of elongated chambers and the location outside of the storage space, and a feed mechanism to move the units between the transfer tube and the elongated chambers.Type: GrantFiled: December 3, 1999Date of Patent: January 9, 2001Assignee: General Dynamics Armament Sys., Inc.Inventors: Joseph F. Bender-Zanoni, Anthony R. Steward, Ned S. Ashton, Derek A. Rodriguez, Glenn P. Livingston
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Patent number: 6167095Abstract: An improved digital bi-directional communications transceiver in which the upstream and downstream portions of the frequency spectrum are allocated different bandwidths and positioned at different locations on the frequency spectrum in response to transmission line conditions and impairments such as system provisioning, background noise, radio frequency interference (RFI), crosstalk and reflected signals. The movement of the upstream and downstream carrier frequencies are elastic in that they may be adjusted in near real-time involving methods for determining the signal quality parameter(SQP) of the received signal. The SQP is used to estimate the bit error rate (BER) margin on the received data and also takes into account the total signal to interference ratio (SIR), where the interference includes crosstalk, RFI, and residual echo from the neighboring upstream or downstream channel.Type: GrantFiled: December 24, 1997Date of Patent: December 26, 2000Assignee: General Dynamics Government Systems CorporationInventors: Neil E. Furukawa, Sheldon N. Salinger
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Patent number: 6145439Abstract: Apparatus mountable in a projectile for utilization with a rotor-type safing and arming mechanism for post-launch self-neutralization of a projectile having a fused warhead and a stab detonator, including a launch-activated battery, an electric detonator positioned sufficiently close to the stab detonator to initiate the stab detonator upon initiation of the electric detonator, and a time delay switch circuit operatively interconnecting the battery and the electric detonator after a predetermined delay time for delivering power sufficient to initiate the electric detonator. The time delay switch circuit includes an R-C delay circuit having a delay capacitor, and an SCR connected in series between the electric power source and the electric detonator, with the SCR gate operatively connected to the delay capacitor. The apparatus also includes a pre-launch shorting circuit electrically connected in parallel with the electric detonator, and a current amplifier interconnected with the SCR and a storage capacitor.Type: GrantFiled: June 16, 1998Date of Patent: November 14, 2000Assignee: General Dynamics Armament Systems, Inc.Inventor: Richard T. Ziemba
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Patent number: 6142080Abstract: Apparatus mountable in a projectile for utilization with a rotor-type safing and arming mechanism for post-launch self-neutralization of a spinning projectile having a fused warhead and a stab detonator, including a launch-activated battery, an electric detonator positioned sufficiently close to the stab detonator to initiate the stab detonator upon initiation of the electric detonator, and a spin decay switch circuit operatively interconnecting a charged storage capacitor and the electric detonator upon substantial cessation of projectile spin, for delivering power sufficient to initiate the electric detonator. The apparatus includes a storage capacitor charging circuit activated by launch-induced forces. The apparatus further includes a pre-launch shorting circuit electrically connected in parallel with the electric detonator and deactivated by launch forces, and a "bleed" circuit connected in parallel with the battery activated by launch-induced forces.Type: GrantFiled: June 16, 1998Date of Patent: November 7, 2000Assignee: General Dynamics Armament Systems, Inc.Inventor: Richard T. Ziemba
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Patent number: 6141770Abstract: A computer system uses redundant voting at the hardware clock level to detect and to correct single event upsets (SEU) and other random failures. In one preferred embodiment, the computer includes four or more commercial processing units (CPUs) operating in strict "lock-step" and whose outputs (33, 37) to system memory and system bus are voted by a gate array which may be implemented in a custom integrated circuit. A custom memory controller interfaces to the system memory and system bus. The data and address (35, 37) at each write to and read from memory within the computer are voted at each CPU clock cycle. A vote status and control circuit "reads" the status of the vote and controls the state of the CPUs using hardware and software. The majority voted signals are used by the agreeing CPUs 32 to continue processing operations without interruption.Type: GrantFiled: June 11, 1999Date of Patent: October 31, 2000Assignee: General Dynamics Information Systems, Inc.Inventors: Stephen Fuchs, Andrew J. Wardrop
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Patent number: 6116818Abstract: An ocean plow device and accompanying method which incorporate a passive plow blade and a jetter tool working in conjunction with one another to lower drawbar and increase cable deployment speeds. In order to avoid cavitation due to sand dilation, in one embodiment of the plow device, the jetter tool includes nozzles oriented in a downward and backward direction relative to the plow device which creates a flow pattern to turbulently remove surface soil in front of the jetter tool in a rapid manner. The jetter tool is pivotally suspended from a point in front of the passive plow blade, such that the jetter will be free to find its own equilibrium position. That is, the pivotal mounting enables the jetter tool to rotate upward in harder soils and become fully extended in softer soils in order to reach the equilibrium position. The passive plow blade behind the jetter tool provides a constant burial depth for the cable and also provides protection from side loads encountered during deployment.Type: GrantFiled: April 29, 1997Date of Patent: September 12, 2000Assignee: General Dynamics Advanced Technology SystemsInventors: James J. Bitetto, James Christopher Coyne, Frank Dominick Messina, Robert D. Smith, Gerald E. Tourgee
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Patent number: 6109034Abstract: To control transmission ratio of a continuously variable hydrostatic transmission including an input shaft, an output shaft, a hydraulic pump unit driven by the input shaft, a grounded hydraulic motor unit, and a wedge-shaped swashplate drivingly, pivotally connected to the output shaft and positioned to accommodate pumped hydraulic fluid exchanges between the pump and motor units. A ratio controller is provided having a pair of hydraulically actuated, differentially sized pistons coupled by a linkage mechanism to pivot the swashplate in opposite transmission ratio-changing directions. The smaller piston is incorporated internally of the output shaft, while the larger piston, of an annular shape, coaxially surrounds the output shaft. The linkage mechanism has geometry effective to translate axial forces exerted by the pistons into amplified ratio-changing moments exerted on the swashplate.Type: GrantFiled: April 8, 1998Date of Patent: August 29, 2000Assignee: General Dynamics Land Systems, Inc.Inventor: Robert Francis Larkin
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Patent number: 6091787Abstract: A simplified symbol lock detector which uses T/2 spaced signal samples in conjunction with an interpolator to approximate the T/4 shifted signal samples used by conventional symbol lock detectors. The approximated T/4 shifted signal samples are processed by a phase detector prior to input to a threshold detector which indicates proper symbol lock if the lock signal exceeds a predetermined threshold.Type: GrantFiled: December 24, 1997Date of Patent: July 18, 2000Assignee: General Dynamics Government Systems CorporationInventor: Dan L. Westfall
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Patent number: 6075891Abstract: A processing system and method identifies materials present in a pixel of a multispectral or a hyperspectral image. Underlying data models representing spectral endmembers or materials of interest and model based relationships are used to identify the materials. The processing system and method provide a technique that detects, unmixes, and classifies spectral signatures for terrain categorization and object identification.Type: GrantFiled: July 6, 1998Date of Patent: June 13, 2000Assignee: General Dynamics Government Systems CorporationInventor: Jerome Allen Burman
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Patent number: 6073534Abstract: A transfer mechanism that can selectively transfer molded solid propellant charges or projectiles between a transport conveyor and respective storage magazines is described. The transfer mechanism has multiple transfer forks driven from a common drive shaft for engaging the munition(s) and selector gates driven by a gate crankshaft associated with each respective magazine for blocking or permitting the transfer controller to either transfer a projectile or one or more solid propellant charges. Each transfer fork and selector gate can be independently and selectively coupled to, or decoupled from, its respective shaft by respective coupling mechanisms under the command of a controller for coordinated transfer operation. The fork and gate coupling mechanisms, as well as a mechanism coupling the drive shaft to respective driven transfer crankshafts provide "uncoupled" positions with the respective fork or gate element or drive shaft restrained from rotary motion.Type: GrantFiled: August 31, 1998Date of Patent: June 13, 2000Assignee: General Dynamics Armament Systems, Inc.Inventor: Joseph A. L. N. Gagnon
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Patent number: 6065385Abstract: A linked bucket carrier for safely transporting molded, solid-propellant charges between a transport conveyor and respective storage magazines is described. The propellant charge carrier includes an elongated body having an arc-shaped cross section that defines an elongated slot which is divided into compartments by spacers so that the carrier is capable of holding at least two propellant charges. The carrier may further include clamping fingers extending from the body and arranged on the body in opposing pairs, and the fingers may be pre-formed so that they define an out-of-round cross section adapted to clamp the propellant charges when the propellant charges are positioned within the body.Type: GrantFiled: August 31, 1998Date of Patent: May 23, 2000Assignee: General Dynamics Armament Systems, Inc.Inventors: Anthony R. Steward, David L. Maher, Michael J. Laurin
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Patent number: 6062022Abstract: In a continuously variable hydrostatic transmission including a hydraulic pump unit driven by an input shaft, a grounded hydraulic motor unit, and an intermediate, wedge-shaped swashplate for developing torque on an output shaft in response to pumped exchanges of hydraulic fluid between the pump and motor units through swashplate ports, a ratio controller is provided to vary transmission ratio by changing the swashplate angular orientation and to engage a lock-up clutch directly mechanically coupling the input shaft to the output shaft when a 1:1 transmission ratio is set.Type: GrantFiled: April 20, 1998Date of Patent: May 16, 2000Assignee: General Dynamics Land Systems, Inc.Inventors: Lawrence Ray Folsom, Clive Tucker
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Patent number: 6058816Abstract: Apparatus is disclosed for supporting a beam having a longitudinal axis. The apparatus includes a clamping assembly that surrounds and grips a portion of the beam. The clamping assembly is relatively compliant to deflections of the beam in at least one direction transverse to the axis, but relatively resistant to axial displacements of the beam and to torsional rotations of the beam about the axis. The apparatus further includes at least one actuator situated externally to the beam and arranged to urge the beam in the compliant direction or directions.Type: GrantFiled: February 28, 1997Date of Patent: May 9, 2000Assignee: General Dynamics Advanced Technology SystemsInventor: Igor Golioto
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Patent number: 6039347Abstract: An airbag inflator includes a pair of telescoping pistons slidingly mounted within a housing. Pressurization of a combustion chamber by a pyrotechnic initiator acts on one piston to pressurize a hydraulic fluid chamber, which, in turn, acts on the other piston to pressurize a liquid propellant reservoir. Liquid propellant can then be regeneratively pumped from the reservoir into the combustion chamber for combustion to generate an airbag inflation gas. A hydraulic fluid damping chamber is utilized to exert a controllable retarding force on the one piston, such as to control the rate of airbag inflation gas generation.Type: GrantFiled: December 19, 1997Date of Patent: March 21, 2000Assignee: General Dynamics Armament Systems, Inc.Inventor: Alfred Charles Maynard
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Patent number: 6036226Abstract: In an occupant restraint apparatus for installation in a vehicle, a smart airbag inflator is provided with a piston for regeneratively pumping liquid propellant from a reservoir into a combustion chamber for ignition and combustion to generate airbag inflation gases. To control the airbag inflation rate, the piston includes a piston head slidingly received in a damping chamber filled with a magneto-rheological fluid that is pumped through an orifice during the regenerative pumping stroke of the piston. An electromagnet is selectively energized to produce a varying magnetic field to adjust the viscosity of the magneto-rheological fluid flowing through the orifice and thus vary a damping force exerted on the piston stroke, thereby modulating the rate of liquid propellant combustion. Electromagnet current excitation is controlled in response to a particular accident scenario.Type: GrantFiled: December 19, 1997Date of Patent: March 14, 2000Assignee: General Dynamics Armament Systems, Inc.Inventors: Steven Joseph Brown, Larry Stefan Ingram, Neale Arthur Messina, Marek Tarczynski
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Patent number: 6036201Abstract: A suspension assembly for mounting a wheel assembly to any wheel position of a vehicle, the suspension assembly being pneumatically controlled to adjust both the ground clearance of the vehicle and its wheel-track width, the suspension assembly also being mountable at any wheel position whether the wheel at that position is to be steerable or nonsteerable. The suspension system includes upper and lower control arms connected between a frame attachable to the vehicle and a kingpin assembly to provide a parallelogram linkage. It also includes at least one pneumatically actuated linear actuator to control the angular disposition of the lower control arm with respect to the frame and thereby control the ground clearance and wheel-track width of the vehicle. The parallelogram geometry provides the upper and lower control arms with at least 120 degrees of angular travel.Type: GrantFiled: February 23, 1998Date of Patent: March 14, 2000Assignee: General Dynamics Land SystemsInventors: James E. Pond, Bruce B. McKinstry
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Patent number: 6000126Abstract: A method and apparatus is provided for connecting area grid array semiconductor chips to a printed wire board. A compliant lead matrix includes a carrier and a plurality of conductive leads arranged parallel to one another and secured relative to the carrier in the form of a matrix. The method includes orienting a first side of the lead matrix to be aligned with a reciprocal matrix of conductive surface pads on the area grid array semiconductor chip. First ends of the leads are electrically connected to the conductive surface pads of the area grid array chip. The second side of the lead matrix is oriented to be aligned with a reciprocal matrix of conductive surface pads on a printed wire board. Second ends of the leads of the lead matrix are electrically connected to the conductive surface pads of the printed wire board thereby establishing an electrical connection between the area grid array chip and the printed wire board.Type: GrantFiled: March 29, 1996Date of Patent: December 14, 1999Assignee: General Dynamics Information Systems, Inc.Inventor: Deepak Keshay Pai