Patents Represented by Attorney G. E. Shook
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Patent number: 4104084Abstract: A heterojunction or Schottky barrier photovoltaic device comprising a conductive base metal layer compatible with and coating predominately the exposed surface of the p-type substrate of the device such that a back surface field region is formed at the interface between the device and the base metal layer, a transparent, conductive mixed metal oxide layer in integral contact with the n-type layer of the heterojunction or Schottky barrier device having a metal alloy grid network of the same metal elements of the oxide constituents of the mixed metal oxide layer embedded in the mixed metal oxide layer, an insulating layer which prevents electrical contact between the conductive metal base layer and the transparent, conductive metal oxide layer, and a metal contact means convering the insulating layer and in intimate contact with the metal grid network embedded in the transparent, conductive oxide layer for conducting electrons generated by the photovoltaic process from the device.Type: GrantFiled: June 6, 1977Date of Patent: August 1, 1978Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: John C. Evans, Jr.
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Patent number: 4104091Abstract: Diffusants are applied onto semiconductor solar cell substrates using screen printing techniques. The method is applicable to square and rectangular cells and can be used to apply dopants of opposite types to the front and back of the substrate. Then, simultaneous diffusion of both dopants can be performed with a single furnace pass.Type: GrantFiled: May 20, 1977Date of Patent: August 1, 1978Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: John C. Evans, Jr., Henry W. Brandhorst, Jr., George A. Mazaris, Larry R. Scudder
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Patent number: 4099799Abstract: A gas-lubricated bearing employing at least one pad mounted on a rectangular cantilever beam to produce a lubricating wedge between the face of the pad and a moving surface. The load-carrying and stiffness characteristics of the pad are related to the dimensions and modulus of elasticity of the beam. The bearing is applicable to a wide variety of types of hydrodynamic bearings.Type: GrantFiled: April 28, 1977Date of Patent: July 11, 1978Inventors: James C. Administrator of the National Aeronautics and Space Administration, with respect to an invention of Fletcher, Izhak Etsion
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Patent number: 4085332Abstract: Apparatus for the separation and extraction of molecular isotopes. Molecules of one and the same isotope are preferentially photo-dissociated by a laser and an ultra-violet source, or by multi-photon absorption of laser radiation. The resultant ions are confined with a magnetic field, moved in opposite directions by an electric field, extracted from the photo-dissociation region by means of screening and accelerating grids, and collected in ducts.Type: GrantFiled: June 3, 1976Date of Patent: April 18, 1978Inventors: James C. Administrator of the National Aeronautics and Space Administration, with respect to an invention of Fletcher, Horst E. Wilhelm
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Patent number: 4084985Abstract: A solar cell panel is fabricated by photoetching a pattern of collector grid systems with appropriate interconnections and bus bar tabs into a glass or plastic sheet. These regions are then filled with a first, thin conductive metal film followed by a layer of a mixed metal oxide, such as InAsO.sub.x or InSnO.sub.x. The multiplicity of solar cells are bonded between the protective sheet at the sites of the collector grid systems and a back electrode substrate by conductive metal filled epoxy to complete the fabrication of an integrated solar panel.Type: GrantFiled: April 25, 1977Date of Patent: April 18, 1978Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: John C. Evans, Jr.
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Patent number: 4083097Abstract: Electrical connections to solar cells in a module are made at the same time the cells are encapsulated for protection. The encapsulating material is embossed to facilitate the positioning of the cells during assembly.Type: GrantFiled: November 30, 1976Date of Patent: April 11, 1978Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Evelyn Anagnostou, Americo F. Forestieri
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Patent number: 4082569Abstract: A transparent, conductive collector layer containing conductive metal channels is formed as a layer on a photovoltaic substrate by coating a photovoltaic substrate with a conductive mixed metal layer; attaching a heat sink having portions protruding from one of its surfaces which define a continuous pattern in combination with recessed regions among said protruding portions to said substrate such that said protruding portions of said heat sink are in contact with the conductive layer of said substrate; andHeating said substrate while simultaneously oxidizing the portions of the conductive layer exposed to a gaseous oxidizing substance forced into said recessed regions of said heat sink, thereby creating a transparent metal oxide layer on said substrate containing a continuous pattern of highly conductive metal channels in said layer.Type: GrantFiled: February 22, 1977Date of Patent: April 4, 1978Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: John C. Evans, Jr.
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Patent number: 4055707Abstract: The energy absorbing properties of solar heating panels are improved by depositing a black chrome coating of controlled thickness on a specially prepared surface of a metal substrate. The surface is prepared by depositing a dull nickel on the substrate, and the black chrome is plated on this low emittance surface to a thickness between 0.5 micron and 2.5 microns.Type: GrantFiled: December 22, 1975Date of Patent: October 25, 1977Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Glen E. McDonald
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Patent number: 4055416Abstract: Strong ferritic alloys of the Fe-Cr-Al type containing 0.4% to 2% tantalum have improved fabricability without sacrificing high temperature strength and oxidation resistance in the 800.degree. C (1475.degree. F) to 1040.degree. C (1900.degree. F) range.Type: GrantFiled: January 21, 1976Date of Patent: October 25, 1977Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Robert E. Oldrieve, Charles P. Blankenship
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Patent number: 4055705Abstract: A coating system which contains a bond coating and a thermal barrier coating is applied to metal surfaces such as turbine blades and which provides both low thermal conductivity and improved adherence when exposed to high temperature gases or liquids. The bond coating contains NiCrAlY and the thermal barrier coating contains a reflective oxide. The reflective oxides ZrO.sub.2 --Y.sub.2 O.sub.3 and ZrO.sub.2 --MgO have demonstrated significant utility in high temperature turbine applications.Type: GrantFiled: May 14, 1976Date of Patent: October 25, 1977Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Stephan Stecura, Curt H. Leibert
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Patent number: 4046560Abstract: A nickel base superalloy for use at temperatures of 2000.degree. F (1095.degree. C) to 2200.degree. F (1205.degree. C) as a stator vane material in advanced gas turbine engines. The alloy has a nominal composition in weight percent of 16 tungsten, 7 aluminum, 1 molybdenum, 2 columbium, 0.3 zirconium, 0.2 carbon and the balance nickel.Type: GrantFiled: December 30, 1975Date of Patent: September 6, 1977Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: John C. Freche, William J. Waters
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Patent number: 4045247Abstract: Thermocouples of the present invention provide stability and performance reliability in systems involving high temperatures and vacuums by employing a bimetallic thermocouple sensor wherein each metal of the sensor is selected from a group of metals comprising tantalum and rhenium and alloys containing only those two metals. The tantalum, rhenium thermocouple sensor alloys provide bare metal thermocouple sensors having advantageous vapor pressure compatibilities and performance characteristics. The compatibility and physical characteristics of the thermocouple sensor alloys of the present invention result in improved emf, temperature properties and thermocouple hot junction performance. The thermocouples formed of the tantalum, rhenium alloys exhibit reliability and performance stability in systems involving high temperatures and vacuums and are adaptable to space propulsion and power systems and nuclear environments.Type: GrantFiled: November 6, 1975Date of Patent: August 30, 1977Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: James F. Morris
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Patent number: 4040867Abstract: A solar cell shingle may be made of an array of solar cells on a lower portion of a substantially rectangular shingle substrate made of fiberglass cloth or the like. The solar cells may be encapsulated in flourinated ethylene propylene (FEP) or some other weatherproof translucent or transparent encapsulant to form a combined electrical module and a roof shingle. The interconnected solar cells are connected to connectors at the edge of the substrate through a connection to a common electrical bus or busses. An overlap area is arranged to receive the overlap of a cooperating similar shingle so that the cell portion of the cooperating shingle may overlie the overlap area of the roof shingle. Accordingly the same shingle serves the double function of an ordinary roof shingle which may be applied in the usual way and an array of cooperating solar cells from which electrical energy may be collected.Type: GrantFiled: August 24, 1976Date of Patent: August 9, 1977Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Americo F. Forestieri, Anthony F. Ratajczak, Leroy G. Sidorak
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Patent number: 4035037Abstract: A hydrostatic bearing support system is provided which comprises a bearing housing having a polygonally configured outer surface which defines at least three symmetrically disposed working faces and a plurality of pressure plates, each of which is disposed relatively opposite a corresponding working face and spaced therefrom to define a gap therebetween. A hydrostatic support film is created in the gap for supporting the housing in spaced relationship to the pressure plates.Type: GrantFiled: March 2, 1976Date of Patent: July 12, 1977Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Robert E. Cunningham
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Patent number: 4033504Abstract: The formation of voids through interdiffusion in bimetallic welded structures exposed to high operating temperatures is inhibited by utilizing an alloy of the parent materials in the junction of the parent materials or by preannealing the junction at an ultrahigh temperature. These methods are also used to reduce the concentration gradient of a hardening agent.Type: GrantFiled: October 24, 1975Date of Patent: July 5, 1977Inventors: James C. Administrator of the National Aeronautics and Space Administration, with respect to an invention of Fletcher, Frank G. Arcella, Gerald G. Lessmann, Russell A. Lindberg
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Patent number: 4023266Abstract: In a process or method according to the invention the parts of an electrical contact device, such as a slip ring comprising the ring to receive the liquid metal and the probe or brush for contacting the liquid metal are treated by sputter etching to remove the parent metal oxide. Prior to exposure of the electrodes to any oxygen, a sacrificial metal is sputter deposited on the parts. Preferably this sacrificial metal is one that oxidizes slowly and is readily dissolved by the liquid metal. The sacrificial metal may then be removed from unwanted areas. The remainder of the ring and the probe to be wet by the liquid metal are submerged in the liquid metal or the liquid metal is flushed over these areas, preferably while they are being slightly abraded, until all the sacrificial material on these portions is wet by the liquid metal. In doing so the liquid metal dissolves the sacrificial metal and permanently wets the parent metal.Type: GrantFiled: July 26, 1976Date of Patent: May 17, 1977Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Robert R. Lovell, Frank D. Berkopec, David H. Culp
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Patent number: 4011719Abstract: The invention is directed to a screen anode for an ion thruster. The anode is constructed of a woven mesh screen, preferably of a stainless steel wire cloth with a mesh size less than the intergrid gap or openings of the screen grid or accelerator grid systems of the ion thruster. The screen anode is sputter coated with tantalum as a result of thruster operation. Because of the fineness of the screen anode any spalled material from the tantalum coated anode is in such small dimensions that the spalled pieces cannot interfere with the accelerator and screen grid systems and with the focusing therebetween.Type: GrantFiled: March 8, 1976Date of Patent: March 15, 1977Assignee: The United States of America as represented by the United States National Aeronautics and Space Administration Office of General Counsel-Code GPInventor: Bruce A. Banks
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Patent number: 4012237Abstract: An improved material for use in a catalytic reactor which reduces nitrogen oxide from internal combustion engines is in the form of a zirconium-modified, precipitation-strengthened nickel-copper alloy. This material has a nominal composition of Ni-30 Cu-0.2 Zr and is characterized by improved high temperature mechanical properties.Type: GrantFiled: June 5, 1975Date of Patent: March 15, 1977Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: John D. Whittenberger
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Patent number: 3996067Abstract: A non-oxide anti-reflective coating is used with a transparent plastic cover of fluorinated ethylene propylene copolymer on a silicon solar cell to increase the resistance to damage caused by electron bombardment.Type: GrantFiled: December 30, 1975Date of Patent: December 7, 1976Assignee: The United States of America as represented by the National Aeronautics and Space AdministrationInventor: Jacob D. Broder
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Patent number: 3983695Abstract: An ion thruster beam shield is provided that comprises a cylindrical housing that extends downstream from the ion thruster and a plurality of annular vanes which are spaced along the length of the housing, and extend inwardly from the interior wall of the housing. The shield intercepts and stops all charge exchange and beam ions, neutral propellant, and sputter products formed due to the interaction of beam and shield emanating from the ion thruster outside of a fixed conical angle from the thruster axis. Further, the shield prevents the sputter products formed during the operation of the engine from escaping the interior volume of the shield.Type: GrantFiled: September 12, 1975Date of Patent: October 5, 1976Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: John L. Power