Patents Assigned to LTV Aerospace and Defense
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Patent number: 5283982Abstract: The milling machine disclosed herein offers significant advantages over prior milling machines, particularly in the field of milling composite panels. The structure of the milling machine, having a C-shaped frame with a clamping mechanism that cooperates with roller transfer balls, provides an accurate and stable reference during the milling operation. A vacuum system substantially eliminates the dust produced during the milling operation, so that the machine is cleaner and grinds more accurately. An electrical system, having a retractable bit control and emergency stopping modes, facilitates even more accurate grinding without undesirable results.Type: GrantFiled: April 1, 1992Date of Patent: February 8, 1994Assignee: LTV Aerospace and Defense CompanyInventors: Jack E. Harper, Jr., John R. Bailleu, Scott J. Pleva, Ronald C. Smith
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Patent number: 5222699Abstract: A variable contour control surface (30a) and a transition section (30a) are designed to eliminate the discontinuities that exist between an aircraft wing control surface and the wing itself. The variable contour is provided by translating the top skin of the control surface relative to the top surface of the wing with the bottom surfaces of the wing and control surface being joined as a single surface. This movement results in a change in the camber of the control surface. The transition section (30a) is a flexible connection between the inboard and outboard ends of the control surface (30a) and the wing. The transition section (30a) is stiffened by rods (40, 41) which run both fore to aft and spanwise within an elastomeric material. The transition section (30b) may be used in conjunction with either a fixed contour control surface or a variable contour control surface.Type: GrantFiled: April 16, 1990Date of Patent: June 29, 1993Assignee: LTV Aerospace and Defense CompanyInventors: Walter C. Albach, Kenneth J. Fewel
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Patent number: 5182779Abstract: A system for monitoring strains and stresses on rope structures and rigid structures containing the ropes is provided wherein a fiber optic is included in a rope structure and change in the fiber's light transmissive/reflective properties, which are caused by strains and stresses on the fiber, are monitored.Type: GrantFiled: April 5, 1990Date of Patent: January 26, 1993Assignee: LTV Aerospace and Defense CompanyInventors: William L. D'Agostino, Michael D. Barrick, Glen R. Williams
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Patent number: 5166696Abstract: Provided is a method and apparatus for deploying an inflatable antenna from a compressed storage position on the trailer bed of a transport vehicle. A support structure is provided having a pair of spaced apart actuating rails for engagement with the antenna during deployment and a storage compartment stored on the trailer bed of the transport vehicle. The storage compartment is formed of a base wall which is pivotally affixed to both the trailer bed and one end of the compressed antenna, and a deployment structure affixed to the opposing end of the compressed antenna. The deployment structure is partitioned lengthwise to form first and second shelter compartments which are hinged together at one end and pivotable with respect to one another between a closed storage position and an open A-frame position.Type: GrantFiled: November 20, 1990Date of Patent: November 24, 1992Assignee: LTV Aerospace and Defense Co.Inventors: Richard B. Rupp, Richard J. Blum
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Patent number: 5164953Abstract: Devices and methods are taught by this invention of populating excited energy levels with fundamental particles. When these populated excited energy levels are further pumped, a population inversion used in quantum electronic applications can result. Each of the various methods involve pumping on an excited energy level of an elemental physical system to cause, by the absorption of energy, the transition of fundamental particles from the excited energy level to a higher energy level. Part of the energy is used for transition of fundamental particles residing in neighboring elemental physical systems from the lowest energy to the excited energy level.Type: GrantFiled: October 26, 1990Date of Patent: November 17, 1992Assignee: LTV Aerospace and Defense CompanyInventors: William E. Case, Mark E. Koch
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Patent number: 5155905Abstract: A method and apparatus are provided for mounting a gate array device 12 on a printed circuit board 14. The device 12 includes at least two pin-type electrical contacts 22, 24 and a plurality of button-type contacts. A sheet of boron nitride 26 is positioned between the printed circuit 14 and the gate array device 12. The sheet of boron nitride 26 includes a plurality of openings extending therethrough in a pattern corresponding to the pattern of electrical contacts 18 on the gate array device 12. The openings 32 in the sheet of boron nitride 26 have resilient electrical contacts 34 disposed therein. The printed circuit board 14 includes a plurality of button-type contacts 40 disposed on a surface thereof in a pattern corresponding to the button-type contacts of the gate array device 12 and the resilient electrical contacts 34.Type: GrantFiled: May 3, 1991Date of Patent: October 20, 1992Assignee: LTV Aerospace and Defense CompanyInventor: Grady A. Miller, Jr.
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Patent number: 5132699Abstract: Provided is a collapsible antenna formed of one or more generally planar and vertically inclined inflatable panels. According to the invention, each of the panels has a continuous outer wall, a continuous inner wall and a plurality of web partitions extending between the inner and outer walls to form a series of tubular members. The inner wall of the collapsible antenna is at least partially covered by a metallic material and a plurality of dipole elements are affixed to the web partitions and spaced from the inner wall in a predetermined relationship such that the antenna will operate at a preselected frequency when inflated.Type: GrantFiled: November 19, 1990Date of Patent: July 21, 1992Assignee: LTV Aerospace and Defense Co.Inventors: Richard B. Rupp, Richard J. Blum, Anthony V. Alongi
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Patent number: 5128671Abstract: A hand-held joystick has spaced-apart groups of accelerometers and is free to move or rotate on multiple axes. Each group has, for example, three mutually perpendicular accelerometers, with each one producing an electrical signal responsive to linear acceleration along one axis. The signals are combined to derive a definition of acceleration of the joystick along the three mutually perpendicular linear axes and/or rotation about these axes. The combined signal is used by an electrical control system which provides input to a device being controlled. The signal to the device under control is responsive to the motion of the joystick.Type: GrantFiled: April 12, 1990Date of Patent: July 7, 1992Assignee: LTV Aerospace and Defense CompanyInventor: William A. Thomas, Jr.
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Patent number: 5126948Abstract: A digitizing system for automatically recording data points representative of, for example, sheet metal templates having varying shapes is disclosed. A stylus connected to a tracing arm is guided along the edge of a template. As the arm moves, digital scales generate a stream of encoded electrical pulses which yield direction and distance information. These pulses are then decoded, counted, and stored. If the operator has selected the automatic digitize mode, a data point is automatically stored each time the stylus moves a predetermined distance in the X, Y, or Z direction. The present invention also provides an improved method of optimizing or compressing the stored set of data points.Type: GrantFiled: November 8, 1989Date of Patent: June 30, 1992Assignee: LTV Aerospace and Defense CompanyInventors: Lee D. Mitchell, Mark Rice
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Patent number: 5118571Abstract: A metal structural component (10) is formed by placing metal tubes (16) between two metal sheets (12) and plastically deforming the tubes (16) by injecting pressured gas therein. The injected gas expands the tubes by superplastic deformation until diffusion bonding occurs between the metal sheets (12) and expanded tubes (16) to form the desired support structure between the metal sheets (12).Type: GrantFiled: December 21, 1990Date of Patent: June 2, 1992Assignee: LTV Aerospace and Defense CompanyInventor: Donald H. Petersen
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Patent number: 5059130Abstract: A system of printed circuit boards is interconnected by using connectors having electrically conductive assemblies that include both pins and sockets. The pins of the assemblies of one connector pass through apertures in the printed circuit boards and engage the sockets of assemblies of another connector on the other side of the printed circuit board. In this manner any number of printed circuit boards may be interconnected to form continuous electrical circuits from one printed circuit board to the next and also provide a mechanical means of holding the system of printed circuit boards together.Type: GrantFiled: May 11, 1990Date of Patent: October 22, 1991Assignee: LTV Aerospace and Defense CompanyInventor: Grady A. Miller, Jr.
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Patent number: 5043839Abstract: The flooring structure of this invention controls electrostatic charges. The normal presence of moisture will not affect the flooring structure's ability to control electrostatic charges. A moisture detector circuit will, however, indicate the presence of moisture, and can activate means for drying this moisture. The resistance of the flooring structure can be adjusted so that electrostatic charges are dissipated at different rates. Multiple flooring structures with different resistance values can be placed side by side.Type: GrantFiled: May 26, 1989Date of Patent: August 27, 1991Assignee: LTV Aerospace and Defense CompanyInventor: William D. Wallace
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Patent number: 5010658Abstract: The present invention provides a hole profile gage comprising a probe that senses deviations in the contour of the inner surface of a bore while it is retracted through the bore. The profile gage includes a processing unit that samples the output from the probe, develops a profile for the hole, and evaluates whether the profile is within predetermined tolerance limits. In a preferred embodiment, the probe comprises a split ball probe coupled with a transducer. In use, the probe is retracted through the bore by a spring coupled with a damping device.Type: GrantFiled: November 22, 1988Date of Patent: April 30, 1991Assignee: LTV Aerospace and Defense CompanyInventors: Jerry T. Griffith, Scott J. Pleva
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Patent number: 5006936Abstract: An encoder circuit utilizes a pair of digital memories clocked at a slower write than read rate to compact analog input data, blanking and synchronization pulse intervals, and generate NTSC video. The NTSC formatted data may be stored utilizing conventional NTSC tape or disc recording equipment or may be transmitted, duplicated, monitored or transcribed utilizing readily available NTSC video equipment. A decoder circuit is provided to reprocess the NTSC video formatted data and restore it to its original form by removing the synchronization and blanking intervals and, utilizing a pair of digital memories clocked at a faster write than read rate, re-stretch the data which was compacted in the time dimension by the encoder circuit.Type: GrantFiled: November 2, 1988Date of Patent: April 9, 1991Assignee: LTV Aerospace and Defense CompanyInventor: John T. Hooks, Jr.
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Patent number: 4977562Abstract: A method and apparatus for stabilizing the frequency at which a laser cavity oscillates comprising a passive system which provides a plurality or continuum of optical paths of differing lengths. The various paths correspond to differences in mode parameters in the cavity, and involve compensating changes in polarization, beam direction, beam divergence, and the like, in exchange for a constant optical path length in the laser cavity. The unchanging optical path length results in a stable frequency of oscillation despite physical changes in the cavity which might otherwise alter that path length.Type: GrantFiled: October 19, 1989Date of Patent: December 11, 1990Assignee: LTV Aerospace and Defense Co.Inventors: Albert B. Welch, Marion W. Scott
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Patent number: 4970403Abstract: The present invention relates to an optical reimaging system which incorporates multiple sets of lenses to transmit an image from one plane to another in the form of image segments which are detected by one or more discrete detector arrays. Signals generated by the detector array or arrays can be used to recombine the image segments to reproduce the image transmitted from the first focal plane. These image segments can be contiguous or separated, inverted or not, depending on the lens arrangment and magnification used. In infrared applications, all or a portion of the reimaging system may be cooled to reduce contaminating warm radiation.Type: GrantFiled: November 18, 1988Date of Patent: November 13, 1990Assignee: LTV Aerospace and Defense CompanyInventor: Nicholas J. Krasutsky
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Patent number: 4946526Abstract: A process for producing reinforced laminate plastic panel structures by thermoplastic compression employing internal mold mandrels which are significantly embrittled during or subsequent to the compression step. Hat stiffened panels formed from two thermoplastic resin sheets may be produced by using elongated mandrels formed of ceramic particulate material adhered together by a binder such as an alkali metal silicate. The mandrels are arranged between a skin sheet and hat stiffener sheets with the respective sheets disposed between the platens of a hydraulic press or other suitable compression molding mechanism. Sandwich laminate structures can be formed employing free thermoplastic resin sheets with a first set of ceramic particulate mandrels interposed between one adjacent pair of sheets and a second set of such mandrels interposed between the other adjacent pair of sheets.Type: GrantFiled: October 29, 1987Date of Patent: August 7, 1990Assignee: LTV Aerospace and Defense CompanyInventors: Jamie L. Petty-Galis, James C. Foster
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Patent number: 4938916Abstract: A neutron radiography system having a high energy neutron generator (100) of the type comprising an ion accelerator (106) and a tritium target (110) located downstream of the accelerator. The generator is disclosed in a housing (22) containing a moderator medium (140) adapted to absorb part of the energy of the neutrons, thereby creating thermal neutrons. A neutron flux booster (130) comprised of a high neutron cross section material, such as depleted uranium, is disposed between the target and the moderator medium such that collisions of high energy neutrons produced at the target will collide with the uranium to release additional high energy neutrons from the booster into the moderator medium. A collimator (40) is disposed in communication with the moderator material for discharging thermal neutrons from the moderator medium.Type: GrantFiled: March 7, 1986Date of Patent: July 3, 1990Assignee: LTV Aerospace and Defense Co.Inventor: William E. Dance
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Patent number: 4936941Abstract: The invention is an automatic skin taping machine for use in applying a protective coating to sheets of material, especially aluminum. The machine comprises a main frame, a transfer car movable within the main frame, an applicator that uniformly applies the coating to the sheet of material by moving over the surface of the sheet, a retainer that immobilizes the sheet of material while the applicator is applying the coating, and a vacuum lift system for transferring the sheet of material from an application position to a storage position. In a preferred embodiment, the application includes a floating roller and a squeegee device.Type: GrantFiled: April 8, 1988Date of Patent: June 26, 1990Assignee: LTV Aerospace and Defense Co.Inventors: Clyde L. Williams, James E. Knight, William W. Tilly
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Patent number: 4933951Abstract: A planar thermal radiator for use in outer space is disclosed. The radiator is adapted to rotate on two mutually perpendicular x and y axes which are in x and y planes respectively that are perpendicular to each other and to the planar surfaces of the radiator. It utilizes a plurality of pairs of heat sensors wherein each heat sensor provides a value of electrical resistance which is representative of the incident heat energy along the sensitive axis of that heat sensor. A common heat sensor pair detects incident heat energy which is perpendicular to the radiator. A first plurality of heat sensor pairs is used to detect incident heat energy along sensitive axes that are parallel to the x-plane and a second plurality of heat sensor pairs is used to detect incident heat energy along sensitive axes that are parallel to the y-plane. One sensor of each heat sensor pair is mounted on the opposite surface of the radiator. Each heat sensor pair has an associated heat sensor pair in its respective plurality.Type: GrantFiled: August 10, 1988Date of Patent: June 12, 1990Assignee: LTV Aerospace and Defense CompanyInventor: Homer W. Heinzman