Patents Assigned to LTV Aerospace
  • Patent number: 4826275
    Abstract: 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: Grant
    Filed: December 14, 1987
    Date of Patent: May 2, 1989
    Assignee: LTV Aerospace and Defense Company
    Inventor: Homer W. Heinzman
  • Patent number: 4826380
    Abstract: 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: Grant
    Filed: January 19, 1988
    Date of Patent: May 2, 1989
    Assignee: LTV Aerospace & Defense Company
    Inventor: Winston L. Henry
  • Patent number: 4814994
    Abstract: 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: Grant
    Filed: November 7, 1986
    Date of Patent: March 21, 1989
    Assignee: LTV Aerospace and Defense Company
    Inventors: James R. Doane, Joan M. Sulecki
  • Patent number: 4808854
    Abstract: A trinary inverter for a digital logic circuit of the type having relatively positive, negative and zero signal voltage values is implemented with CMOS transistors and has the advantages of low power dissipation and low output impedance in the zero signal state. The inverter comprises first, second and third inverter branches, where each branch is formed of a pair of complementary MOS field effect transistors. The inverted output signals from each branch are used to produce a device output signal having the desired voltage transfer characteristics.
    Type: Grant
    Filed: March 5, 1987
    Date of Patent: February 28, 1989
    Assignee: LTV Aerospace & Defense Co.
    Inventor: Frederick G. Reinagel
  • Patent number: 4807184
    Abstract: A modular switching system for connecting a plurality of digital computers to a plurality of computer memories, employing interconnecting digital switching modules. Each module has the capability of recognizing an access request to a computer memory by recognizing a generated address within a range of addresses assigned to that computer memory. The digital switching modules are interconnected with a priority network which permits arbitration between simultaneous requests for access by several digital computers to the same computer memory.
    Type: Grant
    Filed: August 11, 1989
    Date of Patent: February 21, 1989
    Assignee: LTV Aerospace
    Inventor: Charles F. Shelor
  • Patent number: 4801923
    Abstract: 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: Grant
    Filed: July 20, 1984
    Date of Patent: January 31, 1989
    Assignee: LTV Aerospace & Defense Company
    Inventors: Robert J. Schwartz, Frederick G. Reinagel
  • Patent number: 4792904
    Abstract: 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: Grant
    Filed: January 6, 1988
    Date of Patent: December 20, 1988
    Assignee: LTV Aerospace and Defense Company
    Inventors: Frederick G. Reinagel, Allen B. Johnson
  • Patent number: 4791722
    Abstract: A printed circuit 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 circuit. 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 gounded. 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: Grant
    Filed: December 23, 1986
    Date of Patent: December 20, 1988
    Assignee: LTV Aerospace and Defense Co.
    Inventor: Grady A. Miller, Jr.
  • Patent number: 4778317
    Abstract: 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: Grant
    Filed: January 13, 1986
    Date of Patent: October 18, 1988
    Assignee: LTV Aerospace & Defense Company
    Inventors: George A. Earle, III, Michael J. Wheetley, Richard D. Button
  • Patent number: 4774702
    Abstract: 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: Grant
    Filed: July 17, 1987
    Date of Patent: September 27, 1988
    Assignee: LTV Aerospace and Defense Company
    Inventor: Jeffrey A. Giacomel
  • Patent number: 4761556
    Abstract: 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: Grant
    Filed: December 2, 1987
    Date of Patent: August 2, 1988
    Assignee: LTV Aerospace & Defense Company
    Inventors: Fynlon G. Simpson, Robert L. Fisher, James Kissell
  • Patent number: 4759109
    Abstract: 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: Grant
    Filed: November 13, 1986
    Date of Patent: July 26, 1988
    Assignee: LTV Aerospace & Defense Company
    Inventors: Jack W. Mason, Michael Blanc
  • Patent number: 4752160
    Abstract: 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: Grant
    Filed: January 20, 1987
    Date of Patent: June 21, 1988
    Assignee: LTV Aerospace & Defense Company
    Inventors: William J. Murray, George A. Earle, III
  • Patent number: 4745864
    Abstract: An explosive, fragmentation structure having means for selectively controlling fragment size and configuration. The structure includes an outer casing having an inner surface defining a chamber and further includes means for propagating shock waves across the inner surface from a selected one of two detonation points with the chamber. Means are provided for directing shock waves, propagated from the first detonation point, against the surface in a first pattern of segment-defining lines and for directing shock waves, propagated from the second detonation point, against the surface in a second pattern of lines which define segments larger than those of the first pattern.
    Type: Grant
    Filed: December 21, 1970
    Date of Patent: May 24, 1988
    Assignee: LTV Aerospace & Defense Company
    Inventor: Gerald G. Craddock
  • Patent number: 4745557
    Abstract: A machine tool setting device and control system are provided. The machine tool setting device sets the machine tool tip at a predetermined distance above a work piece by detecting when the machine tool tip intercepts an optical beam. The control system allows for the drilling of multi-ply work pieces wherein the multi-plies comprise different thicknesses and hardnesses. The drill bit translational velocity and rotational velocity are continuously controlled for optimization depending upon the type of material and thickness as a hole is drilled through the work piece.
    Type: Grant
    Filed: February 13, 1986
    Date of Patent: May 17, 1988
    Assignee: LTV Aerospace & Defense Company
    Inventors: Gary W. Pekar, Billy R. Sewell, Michael Blanc
  • Patent number: 4703922
    Abstract: A mechanism for raising, rotating and lowering a workpiece from a first secured position to a second secured position with only a rotational input, wherein work operations may be performed on said workpiece in the first and second secured positions, includes dual cam followers extending from the first end of the workpiece for engaging dual camming races to allow the workpiece to first be raised, then rotated and then lowered to a second position. A ball bushing is mounted on the opposite end of the workpiece and pivots in a bushing support to permit the workpiece to rotate about its elongate axis. In an alternative embodiment, two sets of cam followers are provided, one set being mounted at the first end of the workpiece and other set mounted at the opposite end. Both sets of cam followers engage separate dual camming races to rotate the workpiece from a first secured position to a second secured position while remaining in a horizontal position.
    Type: Grant
    Filed: December 12, 1986
    Date of Patent: November 3, 1987
    Assignee: LTV Aerospace and Defense Company
    Inventor: Gene P. Schell
  • Patent number: 4659624
    Abstract: Novel carbon-carbon laminate composite materials capable of significantly increased strengths in at least one predetermined direction of load are disclosed. The composites can comprise plies of resin impregnated woven carbon or graphite cloth material in combination with resin impregnated carbon or graphite filament unidirectional tape or can be fabricated from the unidirectional tape alone. Generally the unidirectional reinforcement of the tape plies provides higher strengths and moduli in specific directions which can be controlled during lay up of parts. The processes for obtaining the beneficial increase strength of unidirectional tape ply materials while avoiding fabrication problems resulting therefrom are also disclosed.
    Type: Grant
    Filed: November 25, 1983
    Date of Patent: April 21, 1987
    Assignee: LTV Aerospace & Defense Company
    Inventors: Robert E. Yeager, Isaac E. Harder, Earl L. Stone, III
  • Patent number: 4655679
    Abstract: An apparatus for translating motive energy includes a rotor structure, having mutually spaced rotor members, adapted to react with fluids within the housing. In one embodiment, the rotor structure is rotationally driven by an external power plant for pumping fluids through a tangentially oriented outlet duct. In a second embodiment, the apparatus is driven by fluid under pressure which is conducted toward the rotor structure through an inlet aligned with peripheral portions of the rotor members, for rotationally driving the rotor structure. A variable geometry inlet control system is provided for controlling fluid flow in response to varying flow conditions and for directioning fluid flow to a portion of the rotor structure. The apparatus incorporates a structural configuration which permits its construction of carbonized composite materials, for operation at elevated temperatures.
    Type: Grant
    Filed: May 25, 1983
    Date of Patent: April 7, 1987
    Assignee: LTV Aerospace and Defense Company
    Inventor: Jeffrey A. Giacomel
  • Patent number: 4645394
    Abstract: A fastening apparatus is adapted to be inserted and removed from one side of a work piece having an opposite side which is substantially inaccessible to a worker. A first, externally threaded member is threadingly engaged with a receiving structure, and a second member is inserted within corresponding seats or grooves for interlocking the two members. In the preferred embodiment diverting seats are provided for forming the second member into locking engagement between the receiving structure and the first member. In one embodiment, seat structures are provided for engaging frangible panels or the like for high temperature applications.
    Type: Grant
    Filed: September 9, 1983
    Date of Patent: February 24, 1987
    Assignee: LTV Aerospace and Defense Company
    Inventors: Donald M. While, Edward C. Matza
  • Patent number: 4637761
    Abstract: An automated tool positioning 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 response 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: Grant
    Filed: March 19, 1984
    Date of Patent: January 20, 1987
    Assignee: LTV Aerospace and Defense Company
    Inventors: William J. Murray, George A. Earle, III