Patents Assigned to LTV Aerospace & Defense Company
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Patent number: 4868980Abstract: A printed circuit board for mounting and connecting a plurality of semiconductor devices is disclosed and includes a planar insulating substrate having multiple conductive layers disposed in overlying relationship within the planar substrate. A plurality of parallel rows of apertures for wire-wrap, quick-connect or stitch-wire contacts are provided for mounting integrated circuits. One side of the printed circuit board includes a plurality of power and ground connections disposed between each pair of parallel rows of apertures so that filter capacitors may be mounted under each integrated circuit, thereby conserving printed circuit board space. In a preferred mode of the present invention, alternate ones of the conductive layers are coupled to a source of electrical power while all remaining conductive layers are grounded. At least two adjacent conductive layers are then utilized to minimize parasitic capacitance by completely surrounding each aperture with a portion of conductive material.Type: GrantFiled: July 12, 1988Date of Patent: September 26, 1989Assignee: LTV Aerospace & Defense CompanyInventor: Grady A. Miller, Jr.
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Patent number: 4868533Abstract: Described is a transformer wherein the primary winding is formed from the same unitary piece of electrically conductive metal that comprises the housing of the transformer.Type: GrantFiled: February 16, 1989Date of Patent: September 19, 1989Assignee: LTV Aerospace & Defense CompanyInventors: Dan Ehrenhalt, George R. Giles
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Patent number: 4868532Abstract: Described is a transformer having a two-piece primary winding and housing wherein the second piece is mechanically received within the first piece and electrically coupled together.Type: GrantFiled: February 16, 1989Date of Patent: September 19, 1989Assignee: LTV Aerospace & Defense CompanyInventors: Dan Ehrenhalt, George R. Giles
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Patent number: 4862763Abstract: A composite, carbon-carbon rotor or rotor hub (20) for use in power translating devices, such as in a turbine engine or in fluid pumps, includes a plurality of carbon-carbon laminate plies (P1-P25) layered to form the thickness of the rotor. The plies include alternating plies of cloth and spiral plies of fibrous material having different diameters to provide a desired variation in the cross-sectional configuration of the rotor. The individual spiral plies may vary in thickness from near the center to the outer edge and may be either tapered or formed to other contours. The cloth plies are positioned at predetermined orientations such that the strand axes are not aligned. These plies consist of fibrous carbon or graphite filament tape preimpregnated with a thermosetting polymer material, such as phenolic resin.Type: GrantFiled: January 9, 1984Date of Patent: September 5, 1989Assignee: LTV Aerospace & Defense CompanyInventors: Earl L. Stone, III, James C. Foster, Stanley L. Whitcher
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Patent number: 4848042Abstract: A system for closely controlling the standoff distance of a nozzle in a remotely controlled fluid jet abrasive cutting system. The system comprises a head assembly having a support section and a nozzle body. Control means move the head assembly along a desired cutting path relative to the workpiece. A nozzle is mounted in the nozzle body and oriented to dispense cutting fluid along an axis directed against the workpiece. The nozzle body and the support section are interconnected by means which function to bias the nozzle body relative to the mounting section in a direction along the cutting axis of the nozzle. The nozzle body is provided with a standoff member which is adapted to ride on a portion of the workpiece and which projects beyond the nozzle tip by a distance sufficient to hold the nozzle off of the workpiece by the desired standoff distance.Type: GrantFiled: September 9, 1987Date of Patent: July 18, 1989Assignee: LTV Aerospace and Defense CompanyInventors: R. Craig Smith, John J. Allevato
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Patent number: 4842184Abstract: A method of applying solder to contacts of a connector, when the contacts are spaced apart according to a given arrangement. The method includes the steps of perforating a water-soluble adhesive material to form perforations in a pattern according to the given arrangement, applying solder preforms around the perforations, positioning the adhesive material to center the solder preforms around the contacts, washing off the adhesive material with water, and heating the contacts to the flow-point temperature of the solder.Type: GrantFiled: June 23, 1988Date of Patent: June 27, 1989Assignee: LTV Aerospace & Defense CompanyInventor: Grady A. Miller, Jr.
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Patent number: 4840763Abstract: A process for the production of reinforced refractory composite structures which may be of high density and shaped in desired three dimensional configurations. The shaped composite structures are produced by forming a suspension of particulate materials including a colloidal refractory power, colloidal sintering aid, and refractory reinforcement whiskers in a carrier liquid. The colloidal suspension is conformed to a desired configuration and brought into contact with a semipermeable membrane. A pressure is imposed on the suspension in the desired configuration to expel liquid from the suspension through the membrane to arrive at a green composite having a density of at least 40% of theoretical density. After drying, the green composite is then sintered under conditions to form an intergranular liquid phase in the composite providing further densification. A specific composite is a silicon carbide reinforced silicon nitride composite.Type: GrantFiled: August 6, 1987Date of Patent: June 20, 1989Assignee: LTV Aerospace and Defense CompanyInventor: Douglas W. Freitag
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Patent number: 4830919Abstract: In accordance with the invention, a composition of matter is provided for forming a coating for protecting carbonaceous substrates from degradation at elevated temperatures. The composition of matter is a mixture of particulate silicon, silicon carbide and alumina. The mixture contains between about 40% and 50% silicon by weight of the total composition, between about 30% and 50% silicon carbide by weight of the total composition and between about 20% and 30% alumina by weight of the total composition. A method is provided for forming a primary protective coating on carbonaceous substrates utilizing the aforesaid mixture. An enhancement coating is provided for sealing the primary coating in applications where the substrate will be subjected to elevated temperatures and temperature cycling.Type: GrantFiled: April 15, 1986Date of Patent: May 16, 1989Assignee: LTV Aerospace & Defense CompanyInventor: David M. Shuford
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Patent number: 4830813Abstract: A lightweight, low energy neutron radiography inspection device (20) includes an inspection head (22) with a sealed tube neutron generator (44) using a deuterium target (110) for emitting relatively low energy neutrons. A moderating fluid (140) within the head is used to thermalize the neutrons emitted from the neutron source. A collimator (40) directs the thermalized neutrons to produce a thermal neutron radiograph. The relatively low energy neutrons produced by the neutron generator permit the reduction in volume of moderating fluid required and thus the use of a smaller, more maneuverable, inspection head.Type: GrantFiled: April 24, 1987Date of Patent: May 16, 1989Assignee: LTV Aerospace & Defense CompanyInventor: William E. Dance
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Patent number: 4827679Abstract: A system and process for fluid jet cutting of a workpiece providing for self orientation of a catcher vessel. This invention comprises a cutting head adapted to be connected to the robot arm of a robotically controlled cutting system. A nozzle is mounted in the cutting head and adapted to dispense a jet cutting fluid stream along a cutting axis to be directed against a workpiece. The system further comprises a catcher assembly including a bracket supporting a catcher vessel having a receiving aperture. The catcher vessel contains a sacrificial material for dissipation of kinetic energy of the spent jet cutting stream. The supporting bracket includes an arm which depends from the cutting head along a traverse which is laterally offset from the cutting axis.Type: GrantFiled: November 24, 1987Date of Patent: May 9, 1989Assignee: LTV Aerospace & Defense CompanyInventor: George A. Earle, III
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Patent number: 4826380Abstract: A pre-cast dome-like shell is loaded with a predetermined amount of curable sealant. The sealant and dome are similar in composition. The dome is pressed over the exposed end of a fastener. An elastic portion of the shell can expand, thereby increasing the internal volume of the shell to accommodate small variations in sealant amount. A close fit between the shell and fastener, combined with an adequate shell wall, insure proper shell orientation and barrier thickness.Type: GrantFiled: January 19, 1988Date of Patent: May 2, 1989Assignee: LTV Aerospace & Defense CompanyInventor: Winston L. Henry
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Patent number: 4826275Abstract: Optical communication system having repeater amplifiers cascaded with plurality of optical star couplers wherein each star coupler is coupled to an associated set of terminals. Each star coupler has two mixing sections serially disposed between its input and output terminal ports. Star couplers receive optical signals from their associated terminals, mix the received signals and retransmit the mixed signals to each terminal in its associated set and to each of the repeater amplifiers. Star couplers also receive amplified signals from the repeater amplifiers, mix the received amplified signal and retransmit the mixed optical signals only to their associated terminals. Star couplers, thus, enable optical signals transmitted by their associated terminals to be transmitted to each terminal in the system without permitting the same signal to be returned to the same star coupler, thereby avoiding the formation of continuous optical loops and hence avoiding the problem of optical lockup.Type: GrantFiled: December 14, 1987Date of Patent: May 2, 1989Assignee: LTV Aerospace and Defense CompanyInventor: Homer W. Heinzman
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Patent number: 4814994Abstract: A relative position navigation system and method installed in a first participant for computing the relative position, in range and azimuth, of at least one other participant in the system without using azimuth-sensing apparatus. The system includes ranging apparatus for determining the distance between the first participant and the other selected participant for at least three selected points in time. A processor determines the change in position of the first participant relative to the second participant during the time periods between the first and second, and second and third points in time, and computes the "synthetic" (rather than measured) azimuth coordinate of the selected other participant relative to the first participant at the third point in time as a function of the distance and change in relative position data obtained by the system.Type: GrantFiled: November 7, 1986Date of Patent: March 21, 1989Assignee: LTV Aerospace and Defense CompanyInventors: James R. Doane, Joan M. Sulecki
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Patent number: 4801923Abstract: A method and apparatus are disclosed for converting a digital TACAN output into an analog potentiometer input suitable for an analog navigation computer. The apparatus includes an input register for temporarily storing a digital TACAN output signal. A nines complement generation circuit is utilized to generate the nines complement of the digital TACAN output signal and the nines complement is temporarily stored in a second register. The data in each register is then utilized to control one of two identical resistive circuits which are coupled to a common output node so that the total resistance in both circuits is always equal to a selected total resistance. In a preferred embodiment of the present invention, a plurality of optically coupled solid state relays are utilized to control the resistive circuits.Type: GrantFiled: July 20, 1984Date of Patent: January 31, 1989Assignee: LTV Aerospace & Defense CompanyInventors: Robert J. Schwartz, Frederick G. Reinagel
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Patent number: 4792904Abstract: A computerized flight inspection system is disclosed. The system of the present invention may be utilized to generate an accurate reference location with respect to an airport runway for an aircraft having an inertial navigation system. A selected geometric pattern having a highly unambiguous autocorrelation function is placed on at least one end of the runway. A video line scanning camera mounted to the aircraft is then utilized to scan the geometric pattern in a line generally perpendicular to the line of flight. The output of the video line scanning camera is then correlated with a stored reference pattern to generate a signal indicative of the detection of the geometric pattern on the runway. A laser altimeter is mounted to the aircraft and utilized to generate an accurate signal indicative of the aircraft altitude with respect to the runway pattern. The outputs of the correlation circuit and the laser altimeter are then utilized to correct data from the inertial navigation system.Type: GrantFiled: January 6, 1988Date of Patent: December 20, 1988Assignee: LTV Aerospace and Defense CompanyInventors: Frederick G. Reinagel, Allen B. Johnson
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Patent number: 4778317Abstract: A tactile sensing tool positioning system for positioning a tool normal to the surface of a curved workpiece is disclosed. The tool positioning system of the present invention includes a steel frame for rigidly supporting a cutting tool having a longitudinal cutting implement, such as a drill bit or countersink bit. The steel frame includes a steel collar which is normal to the axis of the cutting implement and which supports a deformable ring of polyurethane or other resilient material. A plurality of aluminum cylinder positioning sensors are imbedded into the steel collar and surrounded by the deformable ring with one end of each aluminum cylinder positioning sensor contiguous with the exposed surface of the deformable ring. The axial loading experienced by each aluminum cylinder positioning sensor is measured by an associated strain gauge, and a quadrature circuit is then utilized to balance the forces on the aluminum cylinder positioning sensors and normalize the longitudinal cutting implement.Type: GrantFiled: January 13, 1986Date of Patent: October 18, 1988Assignee: LTV Aerospace & Defense CompanyInventors: George A. Earle, III, Michael J. Wheetley, Richard D. Button
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Patent number: 4774702Abstract: A portion of a chalcogenide transformation film in a less reflective phase responds to a low energy laser beam writing pulse by transforming to a crystalline phase. A marmem alloy, secured to the bottom side of the film, responds to a longer erasing pulse of a lower energy laser beam at the same portion by physically stressing the film only at that same portion. The film portion responds to the physical stress by transforming back to a less reflective phase. An optical reader interprets the crystalline phase as a digital logic "1", and the less reflective phase as a digital logic "0".Type: GrantFiled: July 17, 1987Date of Patent: September 27, 1988Assignee: LTV Aerospace and Defense CompanyInventor: Jeffrey A. Giacomel
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Patent number: 4761556Abstract: An infrared receiver for detecting a communications signal during a fixed reception period in a high noise environment that includes a sensor having a cooled detector mounted upon a substrate upon the end of a cold well tube that further includes a cooling gas tube having a fixed orifice to emit a cooling gas upon the interior surface of the substrate. The receiver further includes a signal processor that receives the detector signals and determines if the detector signals include prdetermined signal characteristics of the communications signal.Type: GrantFiled: December 2, 1987Date of Patent: August 2, 1988Assignee: LTV Aerospace & Defense CompanyInventors: Fynlon G. Simpson, Robert L. Fisher, James Kissell
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Patent number: 4759109Abstract: A riveting apparatus includes a body pivotable about a horizontal axis and having first and second arms extending therefrom. Riveting structure is provided on the arms for cooperating to install and fasten rivets through a workpiece positioned between the riveting structure. The body may be rotated between a substantially horizontal to a substantially vertical position to accommodate riveting a workpiece having varying contours. The apparatus allows riveting operations to be performed at any point on the workpiece while permitting the operator to position himself immediately adjacent the point of riveting to assure proper alignment of the workpiece and proper riveting thereof.Type: GrantFiled: November 13, 1986Date of Patent: July 26, 1988Assignee: LTV Aerospace & Defense CompanyInventors: Jack W. Mason, Michael Blanc
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Patent number: 4752160Abstract: An automated tool positining system is disclosed. The system includes a plurality of work stations, each having a set of guide rails disposed along the length thereof. A single control device is provided and includes a set of guide rails adapted to be temporarily aligned with the guide rails of each work station. The control device is thus movable from work station to work station and operates with a novel tool support member which may be selectively positioned along any guide rail to support a cutting tool at a selected position on a particular work station. The tool support member includes arcuate bearing surfaces which permit the cutting tool to be rotated through a conical section having its vertex at the cutting point of the tool in reponse to the output of a workpiece surface detection circuit. In this manner, the cutting tool may be automatically and accurately positioned normal to the contoured surface of the workpiece.Type: GrantFiled: January 20, 1987Date of Patent: June 21, 1988Assignee: LTV Aerospace & Defense CompanyInventors: William J. Murray, George A. Earle, III