Patents Represented by Attorney, Agent or Law Firm Eric R. Katz
  • Patent number: 5181808
    Abstract: A computerized apparatus and method for drilling holes in elongated workpieces. Predetermined locations for holes are input into a computer by visually aligning hole locations on a template with the drilling axis of the apparatus. The computer controls movement of the drill and of the ring segment relative to the drill. The workpiece is moved relative to the drill and is stopped at each predetermined location for drilling.
    Type: Grant
    Filed: September 18, 1991
    Date of Patent: January 26, 1993
    Assignee: Lockheed Corporation
    Inventors: R. Lamar Griggs, Norman E. Hatton
  • Patent number: 5163027
    Abstract: An ultrasonic calibration block for standardizing an output of a pulse-echo ultrasonic inspection system is provided with an insonification surface for receiving ultrasonic pulses from the inspection system and a plurality of reflective interfaces stacked on top of one another and positioned at different distances from the insonification surface, each reflective interface having a different and characteristic reflectivity. A method of calibrating the output of the inspection system, using the calibration block, employs standard waveforms generated by insonifying the calibration block to generate a look-up table of standard waveform amplitudes related to a standardized output of the inspection system for a given material of a part to be inspected.
    Type: Grant
    Filed: March 20, 1992
    Date of Patent: November 10, 1992
    Assignee: Lockheed Corporation
    Inventors: James T. Miller, Bonner W. Staff, Christopher M. Fortunko
  • Patent number: 4905378
    Abstract: Disclosed is a measuring device for determining both absolute and comparative depths of the countersunk portions of countersunk holes drilled in a workpiece, the measuring device being capable of centering itself within a hole being measured so that repetitive measurements can be made early and accurately; further the measuring device is capable of measuring the depth of a countersunk hole through a template.
    Type: Grant
    Filed: August 26, 1985
    Date of Patent: March 6, 1990
    Assignee: Lockheed Corporation
    Inventors: Raymond F. Culver, Sudershan K. Khurana
  • Patent number: 4854724
    Abstract: A method of and apparatus for the non-destructive evaluation of welds joining metal bodies employing infrared thermography; the method comprising the steps of applying thermal energy to a weld and observing temperature differentials that occur on the weld's surface. The apparatus comprises a device for applying thermal energy to welds being inspected; a device for scanning the weld surface for infrared radiation being emitted therefrom; a device for capturing the emitted radiation and converting it to a signal representative of the thermophysical characteristics of the weld; and a device for visually displaying the signal in a form suitable for interpretation.
    Type: Grant
    Filed: March 5, 1986
    Date of Patent: August 8, 1989
    Assignee: Lockheed Corporation
    Inventors: Mark J. Adams, Elton M. Crisman, Jr.
  • Patent number: 4846446
    Abstract: A novel rope tension damper device is adapted to be installed, for example, on the deck of a ship at a location between the winch that controls the effective length of the rope and the fairlead that guides the rope so that it does not snag or tangle as it is wound and unwound from the winch. The device comprises a co-planar pair of sheaves respectively mounted at opposite ends of a rotatable arm.
    Type: Grant
    Filed: June 14, 1984
    Date of Patent: July 11, 1989
    Assignee: Lockheed Corporation
    Inventors: George W. Peppel, Paul E. Sullivan
  • Patent number: 4844385
    Abstract: A pneumatic aerodynamic control surface is described for an aircraft having a region of upwash ahead of a powered-lift or high-lift wing, the control surface comprising blown engine nacelles immersed in the upwash region, and capable of generating moments about all three axes of the aircraft without any external moving parts.
    Type: Grant
    Filed: April 3, 1987
    Date of Patent: July 4, 1989
    Assignee: Lockheed Corporation
    Inventors: John A. Bennett, Robert J. Englar, Andrew S. W. Thomas
  • Patent number: 4828639
    Abstract: An improved method for forming an assembly of laminated materials is provided. The method eliminates an necessity to evacuate a package or position the assembly in an autoclave for forming. In the method, the assembly (14, 70) is positioned against the die face of a rigid die (12, 72). A cavity of essentially constant volume is formed about the die and assembly and encloses the side of the assembly opposite that in contact with the rigid die. The cavity is filled with expandable spheroids (56). The spheroids are expanded to provide the necessary force on the assembly to urge the assembly against the rigid die to form the completed assembly. Preferably, the expandable spheroids (56) are thermally expandable and can comprise, for example, silicone rubber having a coefficient of thermal expansion of about 50.times.10.sup.-5 inches per inch per degree Fahrenheit.
    Type: Grant
    Filed: August 26, 1987
    Date of Patent: May 9, 1989
    Assignee: Lockheed Corporation
    Inventors: Sam C. Aker, Jay W. Jackson, Pettice M. Phillips
  • Patent number: 4822743
    Abstract: A reusable indicating material for detecting leaks in sealed structures and other closed bodies comprises a fabric saturated with an indicator solution containing an acid-base indicator, a surfactant, a buffering system and a humectant. The indicator solution remains reactive when the fabric is dry to the touch and will indicate the presence of leaks in the structure being tested by changing color when a reactive gas escapes from the structure being tested. Upon removal from the tested structure the indicator material reverts to its original color and is available for subsequent tests.
    Type: Grant
    Filed: December 13, 1984
    Date of Patent: April 18, 1989
    Assignee: Lockheed Corporation
    Inventor: Jeffrey G. Wegrzyn
  • Patent number: 4813713
    Abstract: A fluid coupling accommodates misalignments of ducts to be connected in any one or any combination of three basic directions, these being axial, angular and radial. The coupling also provides for duct flexibility while minimizing the number of necessary sealing elements.
    Type: Grant
    Filed: April 30, 1987
    Date of Patent: March 21, 1989
    Assignee: Lockheed Corporation
    Inventor: Bertram A. Peaster
  • Patent number: 4796862
    Abstract: An improved compensating winch (10, 200) is disclosed which incorporates elastomeric elements (20, 118, 202, 204) which are deformable in torsional shear about the rotational axis of the drum of the winch to absorb shock loading of the cable (22) to increase the service life of the cable and winch and resist catastrophic failure. The elastomeric element can comprise a series of alternating elastomeric rings and rigid rings bonded together to form a unitary structure. Concentric elastomeric elements (202, 204) can be connected in a series relationship to provide for greater annular deflection of a drum versus a drive element.
    Type: Grant
    Filed: December 4, 1987
    Date of Patent: January 10, 1989
    Assignee: Lockheed Corporation
    Inventor: George W. Peppel
  • Patent number: 4797680
    Abstract: An airborne antenna platform is disclosed capable of providing near-continuous spherical coverage of the volume surrounding the airborne platform.
    Type: Grant
    Filed: September 16, 1985
    Date of Patent: January 10, 1989
    Assignee: Lockheed Corporation
    Inventor: Rollo G. Smethers, Jr.
  • Patent number: 4795906
    Abstract: A method and apparatus for the non-destructive identification of coated and uncoated metal parts employing infrared thermography. The apparatus comprises a means for directing infrared radiation onto the surface of a part; a means for scanning the part surface for reflected infrared radiation; a means for capturing the reflected radiation and converting it into a signal representative of variations in radiation reflected from the surface of the part; means for etching an identifying code into the surface of the part; and means for displaying the signal as a video image. The method comprises altering the surface reflective characteristics of a part to produce an identifying code, irradiating the part with infrared radiation of a specific wavelength and detecting differences in the amount and intensity of radiation reflected from the part.
    Type: Grant
    Filed: September 2, 1987
    Date of Patent: January 3, 1989
    Assignee: Lockheed Corporation
    Inventors: Mark J. Adams, Elton M. Crisman, Jr., Asrar A. Khan
  • Patent number: 4784959
    Abstract: A method of and apparatus for detecting fuel leaks employing color variable indicators. The method comprises the steps of preparing and applying a water soluble non-staining indicator dye to a test surface, observing color changes indicative of hydrocarbon leaks and removing the indicator dye from the test surface. The apparatus comprises in combination means for preparing the indicator dye, means for applying the indicator dye to the test surface and means for removing the dye from the test surface. The indicator dye comprises a major portion of a dry inert mineral carrier from about 0.1 to about 5.0 weight percent of a direct dye which is non-staining on painted surfaces and which does not migrate into or penetrate polyurethane or epoxy resin base painted surfaces, and from 0.1 to about 1.0 weight percent of a surfactant.
    Type: Grant
    Filed: July 14, 1986
    Date of Patent: November 15, 1988
    Assignee: Lockheed Corporation
    Inventor: Jeffrey G. Wegrzyn
  • Patent number: 4784410
    Abstract: Several versions of a flex joint (10, 100, 200) are disclosed which provides for relative flexible movement between a first member and a second member about a pivot point. The pivotal motion is provided by the use of elastomeric assemblies which are placed in elastomeric shear as one member pivots relative to the other. With each of the flex joints, at least two concentric and separate passages are formed through the flex joint for carrying fluids and the like through the flex joint. The passages remain separate and essentially unchanging in cross-section throughout the entire range of pivotal motion of the flex joint.
    Type: Grant
    Filed: January 30, 1987
    Date of Patent: November 15, 1988
    Assignee: Lockheed Corporation
    Inventors: George W. Peppel, Paul E. Sullivan
  • Patent number: 4783228
    Abstract: Disclosed is a method and apparatus for joining a metal skin to an internal structure comprising forming the metal skin to a permanent desired contour; assembling a lattice of ribs and spars and bonding the lattice to the contoured skin and subsequently forming the completed structure by bonding a pair of skin-superstructure assemblies together. Also disclosed is a diaphram designed to apply pressure to the skin only along structurally supported area of the skin to prevent damage.
    Type: Grant
    Filed: July 3, 1986
    Date of Patent: November 8, 1988
    Assignee: Lockheed Corporation
    Inventors: Sam C. Aker, Pettice M. Phillips
  • Patent number: 4781405
    Abstract: A fluid coupling accommodates misalignments of ducts to be connected in any one or any combination of three basic directions, these being axial, angular and radial. The coupling also provides for duct flexibiity while minimizing the number of necessary sealing elements.
    Type: Grant
    Filed: April 30, 1987
    Date of Patent: November 1, 1988
    Assignee: Lockheed Corporation
    Inventor: Bertram A. Peaster
  • Patent number: 4764060
    Abstract: Disclosed is a quick-change nosepiece (10) for a power drill (27) capable of telescoping by very small increments in the longitudinal direction, of angular or rotational displacement, and of quick and easy engagement and disengagement so as to provide access to the drill bit (29). Alternatively, a nosepiece (10) may be changed with one of greater or lesser length to correspond to the length of the drill bit (29) as the bit is changed.
    Type: Grant
    Filed: April 16, 1987
    Date of Patent: August 16, 1988
    Assignee: Lockheed Corporation
    Inventor: Sudershan K. Khurana
  • Patent number: D298227
    Type: Grant
    Filed: September 16, 1985
    Date of Patent: October 25, 1988
    Assignee: Lockheed Corporation
    Inventor: Rollo G. Smethers, Jr.
  • Patent number: D309168
    Type: Grant
    Filed: November 23, 1987
    Date of Patent: July 10, 1990
    Inventor: John W. Smith
  • Patent number: D319041
    Type: Grant
    Filed: March 24, 1988
    Date of Patent: August 13, 1991
    Assignee: Lockheed Corporation
    Inventor: Jerry W. Phillips