Patents Assigned to Lockheed Aircraft Corporation
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Patent number: 4222039Abstract: A modular panel of dual filament tungsten lamp switches with current limiting, fault indicating, continuous lamp filament testing, and remote control switching capabilities.In one embodiment, the dual filament, self monitoring tungsten lamps are mounted as switches in an array and identified by row and column, the panel including a drum assembly rotatable to a related one of the rows and carrying indicia indicative of the circuits associated with the lamp in each column in the selected row.In a second embodiment, the dual filament, self-monitoring lamps are mounted as switches in an array. Each lamp or the lens cover associated therewith includes circuit identifying indicia visible in daylight by normal contrast and illuminated sufficiently by the lamps for visibility in a dark adapted environment such as the cockpit of an aircraft at night.Type: GrantFiled: December 30, 1976Date of Patent: September 9, 1980Assignee: Lockheed Aircraft CorporationInventor: Michael J. Cronin
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Patent number: 4180222Abstract: An improved control system for the aileron segment of a combined flap and aileron (flaperon) wherein the flaperon, supported, extended and retracted by conventional means, is described. It consists of a splined shaft rotatably mounted on an aircraft wing, its longitudinal axis being substantially aligned with the extension and retraction path of the flap. A transfer gear box slidably engages the splined shaft and is supported by a roller assembly engaging a support track which is mounted in the wing and runs substantially parallel to the splined shaft. The transfer gear box incorporates gears to transfer rotation of the splined shaft, via a second angularly adjustable shaft, to an aileron segment rotation mechanism located on the flaperon at the axis of rotation of the aileron segment.Type: GrantFiled: December 27, 1976Date of Patent: December 25, 1979Assignee: Lockheed Aircraft CorporationInventor: Francis L. Thornburg
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Patent number: 4161650Abstract: A self-powered fiber optic interconnect system in which electrical output from data transmitting equipment is converted in a transmitter unit to optical signals in a fiber optic cable for transmission to a receiver unit for reconversion to electrical signals for data receiving equipment and a power source separate from the transmitting and receiving equipment so that the interconnect system can be completely interchangeable with an electrical copper wire interconnect system. When the data transmitting equipment is a computer with parallel data output, the transmitter unit converts the parallel output to serial data output for transmission to the receiver unit over a single fiber optic cable and the receiver unit reconverts the output to parallel data for the data receiving equipment.Type: GrantFiled: April 6, 1978Date of Patent: July 17, 1979Assignee: Lockheed Aircraft CorporationInventors: Kenneth O. Caouette, George H. Fortescue, Mohammad K. Zaman, Donald J. Oda
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Patent number: 4149999Abstract: An antistatic liquid, and method of use thereof, comprising an ionizable electroconductive polymer, an alcohol and a suitable solvent, for suppressing electrostatic charges which might otherwise develop in certain procedures relating to the manipulation and transport of microspheres, microbeads, or other microscopic particles, as well as the suppression of the reformation of polymers which might otherwise interfere with such procedures.Type: GrantFiled: October 11, 1977Date of Patent: April 17, 1979Assignee: Lockheed Aircraft CorporationInventor: John V. Butler
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Patent number: 4143410Abstract: Control circuit system wherein low level signals are delivered through small (miniature) gauge control conductors to remote control circuit breakers to control connection of load devices to load bus through use of solid state circuitry. Such control may be used between the flight station of an aircraft and the various load centers remote therefrom, in an automobile or in an industrial or utility system. The circuitry is also responsive to faults in the load circuits, and current limiting warning lights (CLWL's) located in the power supply of the control conductors may limit current and indicate the status of faults in the control and/or remote power circuits. A large number of CLWL's for the different circuits may be arranged in a matrix at a control station and means with corresponding load identifying indicia are provided to facilitate changes and correlation of lighted CLWL's with respect to the controlled load switching device.Type: GrantFiled: December 30, 1976Date of Patent: March 6, 1979Assignee: Lockheed Aircraft CorporationInventor: Michael J. Cronin
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Patent number: 4126659Abstract: The invention relates to a method and apparatus for making hollow, resin-impregnated fibrous fabric articles. Specifically, it relates to a method wherein a reusable mandrel is made sufficiently rigid to receive a lay-up of the article to be manufactured. The rigidized assembly is placed within a female mold, derigidized and expanded to apply pressure from within, thereby forcing the lay-up against the interior of the mold. Heat is applied to cure the resin, producing an article having a very high degree of dimensional accuracy.Type: GrantFiled: July 9, 1976Date of Patent: November 21, 1978Assignee: Lockheed Aircraft CorporationInventor: Leiv H. Blad
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Patent number: 4112363Abstract: A test probe apparatus having a housing movable into engagement with a printed circuit device connected to a circuit board with a plurality of electrical contact members extending at various angles to the circuit board, and a plurality of contact probes mounted by said housing for engaging each of said contact members with a constant force insufficient to damage their connection to the circuit device, and a mounting device for holding the housing in engagement with the circuit device while attached to the printed circuit board.Type: GrantFiled: December 27, 1976Date of Patent: September 5, 1978Assignee: Lockheed Aircraft CorporationInventors: Robert A. Morrison, Lyle C. Armstrong
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Patent number: 4109750Abstract: A broadband sound attenuating, acoustically lined, duct of varying cross-sectional shape but in the usual case having a constant cross-sectional area, and wherein the duct liner is configured to maintain an essentially constant acoustic resistance and scaled acoustic reactance throughout provided by means of changes in the effective depth of the liner. Design tradeoffs permit some variation in the cross-sectional area of the duct with concomitant changes in liner properties. In all cases, the duct is designed so that every section along its major axis is optimally tuned to absorb most efficiently some part of the frequency spectrum of interest. The device is particularly suitable for sound suppression of jet aircraft engines.Type: GrantFiled: May 24, 1977Date of Patent: August 29, 1978Assignee: Lockheed Aircraft CorporationInventor: Leslie S. Wirt
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Patent number: 4110809Abstract: Power controllers comprising solid state elements responsive to control signals of low power from a remote control location selectively close and open relatively high power circuits to load devices, and including logic circuitry for opening selectively closed power circuits upon occurrence of overloads therein. The controllers also act upon their failure to respond to commands to open or close the power circuit by blowing a protective fuse in the former case and signaling in the latter. The controllers may employ power darlington switches for closing and opening the power circuits. All or most of the logic circuitry may function in providing the control and the overload or mode failure response for two or more load devices.Type: GrantFiled: December 30, 1976Date of Patent: August 29, 1978Assignee: Lockheed Aircraft CorporationInventor: Michael J. Cronin
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Patent number: 4107530Abstract: An infrared acquisition device is described which surveys a relatively large field of view in which an emissive target is likely to appear. An optical system focuses an image of the target onto a mosaic of separate detectors arranged in concentric fields and so arranged that the appearance of the target image on the outer or peripheral field will reposition the optical system so as to move the image onto the inner or central field. Chopper means are provided for modulating the signal for processing into servo control signals and also for discriminating against background radiation.Type: GrantFiled: January 26, 1966Date of Patent: August 15, 1978Assignee: Lockheed Aircraft CorporationInventors: Elvin S. Brumfield, Edgar W. Kutzscher, James N. Lovelady
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Patent number: 4106013Abstract: Low level control circuitry for controlling a plurality of spaced electrical load devices in an airplane is provided with parallel logic operable to provide for simultaneous manual or condition-responsive dropping of a preselected plurality of said load devices that are considered low priority. Program cards which may be in the form of printed circuit diode boards or separate programmable wiring matrices permit programming to preselect different combinations of load devices for low-priority treatment in response to different levels of emergency and or other logic signals.Type: GrantFiled: December 30, 1976Date of Patent: August 8, 1978Assignee: Lockheed Aircraft CorporationInventor: Michael J. Cronin
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Patent number: 4104620Abstract: A status indicating and current limiting circuit includes a pair of lamp filaments connected in parallel to provide a high reliability for status indication of a monitored switch. The circuit indicates the status of the lamps as well as the open or closed status of the switch. In one embodiment, the pair of lamp filaments are serially connected in parallel between a source of current and the switch so that both the lamp filaments emit bright light when the switch is closed. The lamps are also connected to ground potential through a resistive element to maintain current flow through the lamp filaments when the switch is open, the current being at a level just below the current flow necessary to dimly light the filaments. In the event of a failure of one of the filaments, the other filament will begin to emit a dim but visible light even though the monitored switch is open indicating the failure of the one lamp filament.Type: GrantFiled: December 30, 1976Date of Patent: August 1, 1978Assignee: Lockheed Aircraft CorporationInventor: Michael Joseph Cronin
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Patent number: 4100586Abstract: A current limiting and fault indicating circuit for connection between a load and a source of electrical current including a pair of tungsten lamp filaments connected in parallel. The lamp filaments are chosen so that the current drawn by the load during the normal operation of the load produces only a small voltage drop. In the event of an overload or a short circuit, however, the increased current flow through the lamp filaments will heat the filaments to incandescence and the non-linear increase in impedence will absorb the source voltage and indicate the circuit to malfunction by the emission of bright light. The current flowing as a result of the fault will be limited to the rated current of the lamps.Type: GrantFiled: December 30, 1976Date of Patent: July 11, 1978Assignee: Lockheed Aircraft CorporationInventor: Michael Joseph Cronin
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Patent number: 4088053Abstract: An assemblage of a rivet for securing at least a pair of sheets or other members, wherein the rivet is formed with a cavity in its upset end of predetermined dimensions with respect to the sheets and the remainder of the rivet. The cavity preferably terminates in the thickness of the bottom sheet, thus facilitating rivet upset while providing maximum strength.Type: GrantFiled: February 26, 1975Date of Patent: May 9, 1978Assignee: Lockheed Aircraft CorporationInventor: Gerald W. Tyree
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Patent number: 4067286Abstract: A hydro-ski craft in which load alleviation is attained by reducing the effective wetted area of the planing surfaces at high speeds, and in which elongated flaps extending longitudinally of the craft are mounted to swing about longitudinal axes between generally horizontal planing positions and upwardly swung retracted positions. Spray control dams may be carried by the flaps to themselves automatically swing between inactive and active positions in response to upward swinging movement of the flaps.Type: GrantFiled: February 18, 1975Date of Patent: January 10, 1978Assignee: Lockheed Aircraft CorporationInventors: Ernest G. Stout, Francis L. Thornburg
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Patent number: 4055975Abstract: A process of precision forging of titanium or a titanium alloy in which the forging stock and a segmented die are first heated to forging temperature while separated, and are then assembled together and heated again to that temperature, with the stock being covered by a protective coating preferably containing glass grit, and the die sections being coated with lubricant. The heated die and contained heated forging stock are then inserted in a heated holder and the stock subjected to forging force, to partially but not completely deform the stock to the shape of the die cavity, following which the die and stock are separated and the stock allowed to cool, flashing is removed from the stock, the die is cleaned, the die and stock are recoated and then reheated separately and then together, and the stock is forged again to assume more closely the shape of the die cavity.Type: GrantFiled: April 1, 1977Date of Patent: November 1, 1977Assignee: Lockheed Aircraft CorporationInventors: Tibor Serfozo, Rod F. Simenz
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Patent number: 4053667Abstract: A novel stiffened structural laminate formed by contacting at least one layer of a curable resin-impregnated fabric with at least one strip of cellular honeycomb core, disposing another piece of said curable resin-impregnated fabric over said strip of core, and curing said resin under laminating conditions to bond said honeycomb core to said fabric and produce a unitary laminate which includes said strip as a stiffening bead.Type: GrantFiled: September 9, 1974Date of Patent: October 11, 1977Assignee: Lockheed Aircraft CorporationInventor: Bruce W. Smith
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Patent number: 4049221Abstract: Apparatus for equalizing the pressure between two compartments of an airplane in the event of sudden depressurization of one of the compartments, and including a closure panel disposed across an opening between the two compartments and functioning as either a blowout panel to be forced bodily from the opening upon development of an excessive differential pressure between the two compartments, or as a frangible panel which is shattered in response to attainment of the undesired differential pressure, to thus allow very open communication between the compartments preventing damage to a wall therebetween.Type: GrantFiled: December 24, 1975Date of Patent: September 20, 1977Assignee: Lockheed Aircraft CorporationInventor: Claude Lloyd Fountain
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Patent number: 4040334Abstract: A mechanism rapidly and repetitively launches missiles from inside an aircraft during flight. One or more missiles are carried and launched through a tube protruding through the front of the aircraft thus obviating the necessity for bomb bay or other sizeable, open doors. The aircraft interior may be used as a large accumulator so that pressurized internal air is utilized as the propellant when admitted to a breech. Thus, a "cold" launch is achieved negating the possibility of a "hang fire". Multiple missiles can be carried in revolving chambers which are capable of rapid rotation into firing position. The advantages of the system include the ability to launch at high aircraft altitudes and speeds with the missile moving toward the target.Type: GrantFiled: April 20, 1976Date of Patent: August 9, 1977Assignee: Lockheed Aircraft CorporationInventor: Rollo G. Smethers, Jr.
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Patent number: 4039454Abstract: A device for separating, in an ice environment, fluids having differing physical properties which combine an oleophilic pick-up device with a rotating tumbler mechanism which tends to agitate and propel oil coated pieces of ice rearward and along a perforated inclined through-put barrier where oil jarred off the ice chunks is allowed to rise through the perforations and be contained in an area where it can be accumulated and recovered by the pick-up unit.Type: GrantFiled: June 29, 1976Date of Patent: August 2, 1977Assignee: Lockheed Aircraft CorporationInventors: Henry Francis Miller, Michael George Hoard