Patents Represented by Attorney Leo R. Carroll
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Patent number: 5420689Abstract: This invention is a high speed illumination apparatus and technique which highlights bond wires, ball bonds, bond wedges and microcircuit chips separately against a similar substrate background for manual or high speed automatic inspection of microelectronics assemblies. Preferred angles of illumination are provided which reflect off the different specular surfaces of the bond wires, wire bonds, and bond wedges, providing improved background contrast. Light projected on the flat surfaces of microchip bodies tends to be absorbed, producing a negative contrast shadow if the other elements are illuminated in parallel. Formation of the multiple light rings starts with light generated by a tungsten lamp, collimation by a condenser lens, then passage through a liquid crystal light valve having a plurality of circular active transmission areas.Type: GrantFiled: March 1, 1993Date of Patent: May 30, 1995Inventor: Bernard Siu
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Patent number: 5415058Abstract: A locking device is provided for a removable tailgate on a pickup truck which permits normal rotational use of the tailgate while the lock is installed. The device is comprised of two basic parts, a lock and a lockable clamp. The clamp is used to close the open portion of the receiving cup through which the shaft is passed when the tailgate is normally removed. The clamp consists of a "b" shaped clamp with bent apertured tabs at each end. The lock mechanism includes a short linear plunger shaft with a head on the end of the shaft outboard of the lock. The diameter of the head is larger than the apertures in the end tabs of the clamp, so that the clamp is held secure.Type: GrantFiled: February 1, 1993Date of Patent: May 16, 1995Inventors: William M. Young, Harold Peterson
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Patent number: 5347860Abstract: This invention provides a device and method for measurement of the actual on-bottom time of a sampling otter trawl used for benthic sampling. The device uses passive measurement of the actual on-bottom time without cables and wires connected to the ship, and is small enough to be mounted on a standard otter trawl door without affecting its net-towing function. The apparatus consists of a sealed bottom contacting and counting sensor which totalizes and displays the accumulated on-bottom time. Power is supplied from a self-contained battery which may be automatically recharged by a solar cell. In operation, a flexible trigger arm is mounted so as to extend below the runner on the bottom edge of the trawl door. When bottom contact is first made, the trigger arm bends and mechanically causes a magnet to move sufficiently close to actuate a magnetic switch inside a transparent electronic data module. An electronic counter inside the module will count minutes and seconds as long as the magnetic switch is closed.Type: GrantFiled: September 21, 1993Date of Patent: September 20, 1994Inventor: J. Patton Rimer
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Patent number: 5329918Abstract: This invention provides for the addition of a small electrical element within the confines of a conventional gas station on a cooktop for purposes of simmer cooking which requires control of temperatures below the minimum obtainable with the minimum gas flow rate control settings. Control of power to the electrical heating element is commenced by a first microswitch after control of the gas portion of the burner has been minimized, and reignition has been disabled by operation of a second microswitch. Electrical control means include on-off heater control, continuous power control with a rheostat, or by stepwise adjustment as in a conventional stove. The electrical system and control may be incorporated within a conventual gas burner during assembly with minimum modification.Type: GrantFiled: January 27, 1993Date of Patent: July 19, 1994Inventor: Gaetano Di Bari
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Patent number: 5302836Abstract: This invention is a high speed illumination apparatus and technique which isolates bond wires, ball bonds, bond wedges and microcircuit chips exclusively for manual or high speed automatic inspection of microelectronics assemblies. This system consists of multiple concentric rings of illumination, which are focused towards the center of the rings, but from different angles of incident. Light from these angles reflect off the different specular surfaces of the bond wires, wire bonds, and bond wedges, providing background contrast. Light projected on the flat surfaces of microchip bodies tends to be absorbed, producing a negative contrast shadow if the other elements are illuminated in parallel. Unique angles of incidence provide substantial illumination contrasts between the areas of interest and its neighboring surfaces. The reflections provide unique signatures which are easily distinguishable by an image processing system.Type: GrantFiled: July 16, 1992Date of Patent: April 12, 1994Inventor: Bernard Siu
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Patent number: 5211358Abstract: A deflated airbag is located on the outside of a missile or other vehicle beneath a folded, pivotally mounted airfoil member prior to launch, and a supply of pressurized gas is connected to the interior of the airbag via a suitable valve. After launch, or after lowering of a launch platform in the case of launch from an aircraft, an actuator such as an acceleration sensing device or timing device opens the valve, supplying gas to inflate the bag and simultaneously urge the airfoil into an extended, working position. After the airfoil is locked in its extended position, the airbag rapidly deflates and may be dropped off or retracted. Where more than one airfoil is to be deployed, separate airbags are located beneath each of the folded airfoils and a common gas supply is connected to all of the airbags.Type: GrantFiled: May 13, 1991Date of Patent: May 18, 1993Assignee: General Dynamics CorporationInventor: Cloy J. Bagley
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Patent number: 5211776Abstract: A process for manufacturing metal and ceramic matrix composite materials. The invention also encompasses various composite products made by the disclosed method. The resulting composite material comprises a reinforcement material in either continuous or discrete form embedded in a matrix material which is either a pure metal, a metal alloy, or a ceramic. The reinforcing material is optionally coated with a barrier coating material. An electric arc or plasma arc is used to spray a thin layer of matrix material over a preplaced layer of reinforcement material. Successive layers are built up until a desired object shape and thickness are achieved. There is an optional final step of high-temperature diffusion annealing or hot isostatic pressing.Type: GrantFiled: July 17, 1989Date of Patent: May 18, 1993Assignee: General Dynamics Corp., Air Defense Systems DivisionInventor: Sam M. Weiman
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Patent number: 5206450Abstract: 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: GrantFiled: May 13, 1991Date of Patent: April 27, 1993Assignee: General Dynamics Corporation Air Defense Systems DivisionInventor: Edward T. Piesik
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Patent number: 5183066Abstract: Apparatus for cleaning paint spray gun nozzles automatically includes a housing having separate cleaning and reservoir chambers separated by a dividing wall, and a cleaning spray head in the cleaning chamber for directing a spray of cleaning fluid at a nozzle in the chamber. A supply of cleaning fluid in the reservoir is connected to the cleaning spray head by a supply tube. The cleaning chamber has an entrance for receiving a spray gun nozzle, and a supply of gas under pressure is connected to the reservoir chamber automatically on detection of entry of a spray gun nozzle through the entrance, to urge cleaning fluid from the reservoir into the supply tube. A passageway is provided in the dividing wall for returning used cleaning fluid to the reservoir. The supply of gas to the reservoir is cut off automatically at the end of a cleaning cycle on removal of the cleaned nozzle from the chamber.Type: GrantFiled: April 2, 1991Date of Patent: February 2, 1993Assignee: General Dynamics Corp., Air Defense Systems DivisionInventor: Gary L. Hethcoat
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Patent number: 5171693Abstract: 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: GrantFiled: July 5, 1991Date of Patent: December 15, 1992Assignee: General Dynamics Corporation Air Defense Systems DivisionInventors: Sean A. Johnson, Nancy K. Roberts
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Patent number: 5165040Abstract: A pre-stressed cartridge of the invention generally comprises a cylindrical liner wrapped with a plurality of layers of wound fibers or high tensile wires. These high tension wrapped windings put the walls of the cartridge liner into compression, thus pre-stressing the cylindrical liner. A cartridge constructed in this fashion may develop an ultimate strength in the circumferential direction which approaches ten times the ultimate strength of a typical solid metal cylinder alone. Special reinforcing elements may also be provided, located at the points where the maximum stress is developed upon detonation. Various modifications of this structure include fabricating the liner out of ceramic instead of aluminum, incorporating a steel cup containing the explosive at the base of the internal space of the cartridge, and combining the composite windings with the steel cup to provide a cartridge consisting of a steel cup with the rest of the cartridge being composite fiber windings.Type: GrantFiled: December 23, 1991Date of Patent: November 17, 1992Assignee: General Dynamics Corp., Air Defense Systems DivisionInventors: Norman H. Andersson, S. D. Mack, Edward W. LaRocca, deceased
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Patent number: 5162605Abstract: A structural arrangement is provided in conjunction with the upper closure of a missile cell which, upon launch of the missile, generates a rarefaction wave which assists in closing the bottom closure of the missile cell. As a result, reverse flow of exhaust gases back up into the missile chamber from an associated plenum chamber is prevented or minimized.Type: GrantFiled: January 16, 1992Date of Patent: November 10, 1992Assignee: General Dynamics CorporationInventor: Edward T. Piesik
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Patent number: 5162698Abstract: A cascaded magnetron device has an elongate cathode shank extending along its axis and a series of tubular anode elements placed end to end in a linear cascade surrounding the cathode shank along at least part of its length. Each adjacent pair of anode elements is separated by a conductive, annular pin down disc, and the cathode shank has a series of spaced bands of field emitting material separated by non-emitting regions, each band being located within a respective one of the anode elements and spaced inwardly from the ends of that element. Suitable power inputs and magnetic field generators are provided for generating electron emission and oscillation in the interaction zone between each emitting band and the anode element surrounding that band, and suitable extraction devices are provided for extracting power from each of the interaction zones, the arrangement producing phase-locking of the cascaded magnetron bodies.Type: GrantFiled: December 21, 1990Date of Patent: November 10, 1992Assignee: General Dynamics Corporation Air Defense Systems Div.Inventors: Keith Kato, James Weatherall
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Patent number: 5159241Abstract: 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: GrantFiled: October 25, 1990Date of Patent: October 27, 1992Assignee: General Dynamics Corporation Air Defense Systems DivisionInventors: Keith G. Kato, James C. Weatherall
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Patent number: 5136922Abstract: 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: GrantFiled: May 13, 1991Date of Patent: August 11, 1992Assignee: General Dynamics Corporation, Air Defense Systems DivisionInventor: Edward T. Piesik
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Patent number: 5129604Abstract: A lateral thrust assembly for missile maneuvering comprises an annular array of outwardly directed nozzles, each nozzle having a releasable plug normally blocking flow of propellant gases out of the nozzle. A plug release mechanism associated with each plug allows that plug to be released to open the respective nozzle. A combustion chamber containing propellant is connected to the inner ends of all the nozzles. The propellant is ignited when one or more selected plugs are released to allow opening of the associated nozzle or nozzles, controlling the direction of the lateral thrust applied to the vehicle.Type: GrantFiled: July 17, 1989Date of Patent: July 14, 1992Assignee: General Dynamics Corporation, Pomona Div.Inventor: Cloy J. Bagley
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Patent number: 5111525Abstract: 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: GrantFiled: October 15, 1990Date of Patent: May 5, 1992Assignee: General Dynamics CorporationInventor: Edward Hartouni
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Patent number: 5078843Abstract: 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: GrantFiled: June 13, 1989Date of Patent: January 7, 1992Assignee: General Dynamics Corporation Air Defense Systems DivisionInventor: Wilson N. Pratt
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Patent number: 5062149Abstract: A millimeter wave device having a dielectric substrate with a pair of substantially parallel planar surfaces with at least one predetermined millimeter wave circuit pattern formed in a conductive layer located on at least one of the substrate surfaces. A substantially planar conductive channel plate is mounted adjacent the conductive layer on one substrate surface with the channel plate having an aperture overlying each circuit pattern formed in the conductive layer. A substantially planar conductive cover plate is mounted adjacent one of the channel plates so as to form a first cavity in the region defined by the substrate surface, the channel plate aperture and the cover plate. The device may further include a second substantially planar conductive channel plate mounted adjacent the other one of the substrate surfaces with the second channel plate having an aperture corresponding to and aligned with the first channel plate aperture.Type: GrantFiled: October 23, 1987Date of Patent: October 29, 1991Assignee: General Dynamics CorporationInventors: Garry N. Hulderman, Eugene Phillips, Richard J. Swanson
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Patent number: D337004Type: GrantFiled: March 5, 1990Date of Patent: July 6, 1993Inventors: Steven M. O'Day, Edie M. Boudreau