Patents Assigned to LTV Aerospace & Defense Company
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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: 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: 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: 4980133Abstract: This invention provides a method and apparatus for controlled crystal growth. The apparatus involves two tandemly aligned heat pipes separated by a conductive sleeve. The heat pipes establish two different isothermal temperature zones while the sleeve defines a gradient zone. A crystallization zone is located in this gradient zone. The method for controlled growth of a crystal involves lowering an ampoule through the gradient zone at an effective rate.Type: GrantFiled: March 16, 1988Date of Patent: December 25, 1990Assignee: LTV Aerospace & Defense CompanyInventor: Mark E. Koch
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Patent number: 4971745Abstract: A method for applying a uniform sealant coating over the portion of a fastener exposed above a panel includes applying a sealant retaining shell over the exposed portion of the fastener to define a closed volume between the shell, fastener and panel. The shell has an aperture, removed from the mouth of the shell, for receiving sealant therethrough. An injection nozzle receiving structure for receiving a sealant injector nozzle therein is provided adjacent and substantially aligned with the aperture. Sealant is injected into the shell through the injection nozzle receiving structure and through the aperture therein to fill the area between the fastener and the shell. A pressure is selected for injecting the sealant such that injection is stopped when the shell is filled. The sealant is allowed to cure and the retaining shell is removed.Type: GrantFiled: June 30, 1986Date of Patent: November 20, 1990Assignee: LTV Aerospace & Defense CompanyInventors: Robert R. Ferenc, Jay B. Mize
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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: 4950170Abstract: 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: June 23, 1988Date of Patent: August 21, 1990Assignee: LTV Aerospace & Defense CompanyInventor: Grady A. Miller, Jr.
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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: 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
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Patent number: 4931241Abstract: A process for producing a green composite structure by isostatic compression and filtration. A suspension of colloidal size matrix powders is established in a carrier liquid. The suspension is incorporated into a die chamber having a filter opening containing a filter which is permeable to filtrate from the suspension under applied pressure but substantially impermeable to the matrix powders. An elevated pressure is isostatically imposed on the colloidal suspension within the die chamber. The pressure is maintained for a period of time to expel at least 20% of the liquid originally in the colloidal suspension through the filter opening. A specific die chamber comprises a rigid cage structure and an expandable bladder within the cage structure into which the colloidal suspension is introduced. The cage structure is disposed within a pressure vessel which can be initially evacuated to cause the bladder to conform to the cage structure and then pressurized with fluid for the isostatic compression procedure.Type: GrantFiled: August 6, 1987Date of Patent: June 5, 1990Assignee: LTV Aerospace and Defense CompanyInventor: Douglas W. Freitag
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Patent number: 4876800Abstract: A portable grip length indicator for determining a discrete fastener length for a fastener to be used in fastening a stack of two or more pieces of material. The indicator comprises a body, a probe attached to the body and capable of extending beyond the body for determining the thickness of the stack, a transducer connected to the probe for sensing the relative movement of the probe and translating the movement into an electrical output signal, and an electrical processor for computing the discrete fastener length from the output signal of the transducer according to a predetermined correlation of the thickness of the stack and the type of fastener to be used.Type: GrantFiled: October 7, 1988Date of Patent: October 31, 1989Assignee: LTV Aerospace and Defense CompanyInventors: Gary W. Pekar, Jack W. Mason, Michael Blanc