Patents Represented by Attorney Richard H. Bryer
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Patent number: 5122671Abstract: This invention relates to terbium activated silicate luminescent glasses exhibiting reduced afterglow and enhanced luminescence due to incorporation therein of selected rare earth oxides of cerium, europium and godolinium.Type: GrantFiled: June 24, 1991Date of Patent: June 16, 1992Assignee: Lockheed Missiles & Space Company, Inc.Inventors: Robert A. Buchanan, Clifford Bueno
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Patent number: 5120970Abstract: This invention relates to terbium activated silicate luminescent glasses exhibiting reduced afterglow and enhanced luminescence due to incorporation therein of selected rare earth oxides of cerium, europium and gadolinium.Type: GrantFiled: June 24, 1991Date of Patent: June 9, 1992Assignee: Lockheed Missiles & Space Company, Inc.Inventors: Robert A. Buchanan, Clifford Bueno
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Patent number: 5108959Abstract: This invention relates to terbium activated borate luminescent glasses exhibiting enhanced x-ray absorption characteristics and conversion of absorbed energy into green light due to incorporation therein of gadolinium oxide.Type: GrantFiled: November 16, 1990Date of Patent: April 28, 1992Assignee: Lockheed Missiles & Space Company, Inc.Inventors: Robert A. Buchanan, Clifford Bueno, Harold Berger
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Patent number: 4818625Abstract: Hydrogenated boron-silicon alloy films having unexpected properties permitting in one embodiment the bonding together of metal and ceramic substrates by coating the surfaces to be bonded with the film mating the surfaces and heat treating the mated surfaces to expell hydrogen therefrom and to react to resulting boron-silicon alloy film with the substrates to form a liquid reaction product which forms a surface bond with the substrates or is at least partially absorbed in the substrates. In another embodiment, at least one surface of an intermetallic compound formed from elements selected from groups III and V of the periodic table is sealed against structural degradation by forming on the surface a solid boron-silicon-hydrogen alloy film. In still another embodiment, metal and organic resin substrates are protected against attack by water vapor, dissociated oxygen and molecular oxygen by forming a solid boron-silicon-hydrogen alloy film on the substrates.Type: GrantFiled: March 23, 1987Date of Patent: April 4, 1989Assignee: Lockheed Missiles & Space Company, Inc.Inventors: Henry W. Lavendel, John C. Robinson
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Patent number: 4810532Abstract: Hydrogenated boron-silicon alloy films having unexpected properties permitting in one embodiment the bonding together of metal and ceramic substrates by coating the surfaces to be bonded with the film mating the surfaces and heat treating the mated surfaces to expell hydrogen therefrom and to react to resulting boron-silicon alloy film with the substrates to form a liquid reaction product which forms a surface bond with the substrates or is at least partially absorbed in the substrates. In another embodiment, at least one surface of an intermetallic compound formed from elements selected from groups III and V of the periodic table is sealed against structural degradation by forming on the surface a solid boron-silicon-hydrogen alloy film. In still another embodiment, metal and organic resin substrates are protected against attack by water vapor, dissociated oxygen and molecular oxygen by forming a solid boron-silicon-hydrogen alloy film on the substrates.Type: GrantFiled: May 31, 1988Date of Patent: March 7, 1989Assignee: Lockheed Missiles & Space Company, Inc.Inventors: Henry W. Lavendel, John C. Robinson
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Patent number: 4806431Abstract: Hydrogenated boron-silicon alloy films having unexpected properties permitting in one embodiment the bonding together of metal and ceramic substrates by coating the surfaces to be bonded with the film mating the surfaces and heat treating the mated surfaces to expell hydrogen therefrom and to react to resulting boron-silicon alloy film with the substrates to form a liquid reaction product which forms a surface bond with the substrates or is at least partially absorbed in the substrates. In another embodiment, at least one surface of an intermetallic compound formed from elements selected from groups III and V of the periodic table is sealed against structural degradation by forming on the surface a solid boron-silicon-hydrogen alloy film. In still another embodiment, metal and organic resin substrates are protected against attack by water vapor, dissociated oxygen and molecular oxygen by forming a solid boron-silicon-hydrogen alloy film on the substrates.Type: GrantFiled: March 23, 1987Date of Patent: February 21, 1989Assignee: Lockheed Missiles & Space Company, Inc.Inventors: Henry W. Lavendel, John C. Robinson
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Patent number: 4778726Abstract: Hydrogenated boron-silicon alloy films having unexpected properties permitting in one embodiment the bonding together of metal and ceramic substrates by coating the surfaces to be bonded with the film mating the surfaces and heat treating the mated surfaces to expell hydrogen therefrom and to react to resulting boron-silicon alloy film with the substrates to form a liquid reaction product which forms a surface bond with the substrates or is at least partially absorbed in the substrates. In another embodiment, at least one surface of an intermetallic compound formed from elements selected from groups III and V of the periodic table is sealed against structural degradation by forming on the surface a solid boron-silicon-hydrogen alloy film. In still another embodimemt, metal amd organic resin substrates are protected against attack by water vapor, dissociated oxygen and molecular oxygen by forming a solid boron-silicon-hydrogen alloy film on the substrates.Type: GrantFiled: May 1, 1987Date of Patent: October 18, 1988Assignee: Lockheed Missiles & Space Company, Inc.Inventors: Henry W. Lavendel, John C. Robinson
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Patent number: 4692388Abstract: Hydrogenated boron-silica alloy films having unexpected properties permitting in one embodiment the bonding together of metal and ceramic substrates by coating the surfaces to be bonded with the film mating the surfaces and heat treating the mated surfaces to expell hydrogen therefrom and to react to resulting boron-silicon alloy film with the substrates to form a liquid reaction product which forms a surface bond with the substrates or is at least partially absorbed in the substrates. In another embodiment, at least one surface of an intermetallic compound formed from elements selected from groups III and V of the periodic table is sealed against structural degradation by forming on the surface a solid boron-silicon-hydrogen alloy film. In still another embodiment, metal and organic resin substrates are protected against attack by water vapor, dissociated oxygen and molecular oxygen by forming a solid boron-silicon-hydrogen alloy film on the substrates.Type: GrantFiled: December 2, 1986Date of Patent: September 8, 1987Assignee: Lockheed Missiles & Space Company, Inc.Inventors: Henry W. Lavendel, John C. Robinson
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Patent number: 4689104Abstract: Hydrogenated boron-silicon alloy films having unexpected properties permitting in one embodiment the bonding together of metal and ceramic substrates by coating the surfaces to be bonded with the film mating the surfaces and heat treating the mated surfaces to expell hydrogen therefrom and to react to resulting boron-silicon alloy film with the substrates to form a liquid reaction product which forms a surface bond with the substrates or is at least partially absorbed in the substrates. In another embodiment, at least one surface of an intermetallic compound formed from elements selected from groups III and V of the periodic table is sealed against structural degradation by forming on the surface a solid boron-silicon-hydrogen alloy film. In still another embodiment, metal and organic resin substrates are protected against attack by water vapor, dissociated oxygen and molecular oxygen by forming a solid boron-silicon-hydrogen alloy film on the substrates.Type: GrantFiled: June 24, 1985Date of Patent: August 25, 1987Assignee: Lockheed Missiles & Space Company, Inc.Inventors: Henry W. Lavendel, John C. Robinson
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Patent number: 4557770Abstract: Aluminum base alloys characterized by low density, high elastic modulus and high strength and having a composition consisting esentially of aluminum--about 0.5 to about 4.3 weight percent lithium--about 0.02 to about 20 weight percent beryllium.Type: GrantFiled: August 8, 1983Date of Patent: December 10, 1985Assignee: Lockheed Missiles & Space Company, Inc.Inventors: Aldo E. Vidoz, Donald D. Crooks, Richard E. Lewis, Ian G. Palmer, Jeffrey Wadsworth
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Patent number: 4549187Abstract: This invention relates to an antenna material and more particularly to an antenna material comprising, in its preferred embodiment, a woven mesh of amorphous silica fibers, a conductive metal coating on at least the outer surfaces of the mesh and a lubricant covering and adhering to non-metallized surfaces of the silica fibers.Type: GrantFiled: April 5, 1982Date of Patent: October 22, 1985Assignee: Lockheed Missiles & Space Company, Inc.Inventor: Donald J. Levy
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Patent number: 4540914Abstract: A faceplate of a cathode ray tube is shown wherein a cathodoluminescent phosphor material 1 is deposited on glass faceplate 2. A metal nitride metal absorbing inhomogeneous film 3, where the metal is aluminum or silicon, is deposited on the back side of the phosphor material 1. To avoid unwanted reflections at the interface between the glass 2 and the phosphor 1, a homogeneous film 4 is optionally deposited on glass plate 2 prior to deposition of the phosphor film 1. Additionally, an anti-reflection coating 5 may also be optionally applied to the exterior of the glass plate 2 to eliminate reflection that would otherwise occur at the air-glass interface.Type: GrantFiled: December 17, 1982Date of Patent: September 10, 1985Assignee: Lockheed Missiles & Space Company, Inc.Inventor: T. Grant Maple
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Patent number: 4421806Abstract: Filament-wound composite bodies are disclosed. These bodies contain filament-wound fibers and resin. The resin, when cured, has a density of less than 1.05 g/cc and exhibits a water pick up of less than 1% by weight. When uncured, the resin contains an aromatic vinyl hydrocarbon monomer and as its major component poly(1,2-butadiene), carboxy-terminated poly(1,2-butadiene) or mixtures thereof and has a viscosity of less than 2000 cps at 45.degree. C. These filament-wound bodies advantageously are embodied as rocket motor cases.Type: GrantFiled: August 13, 1981Date of Patent: December 20, 1983Assignee: Lockheed Missiles & Space Company, Inc.Inventors: Burton S. Marks, Richard E. Mauri, Gazel W. Watsey
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Patent number: 4420460Abstract: As-cast titanium alloys characterized by fine grain structures are readily produced by inoculation of the alloys prior to or during the casting thereof with small amounts of at least one composition selected from the group consisting of titanium--0.4 to 15 weight percent carbon, titanium--1.4 to 6 weight percent nitrogen and titanium--1.3 to 10 weight percent oxygen.Type: GrantFiled: December 2, 1982Date of Patent: December 13, 1983Assignee: Lockheed Missiles & Space Company, Inc.Inventor: Frank A. Crossley
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Patent number: 4297584Abstract: This invention relates to rare earth phosphor screens for converting image carrying incident radiation to image carrying visible or near-visible radiation and to the rare earth phosphor materials utilized in such screens. The invention further relates to methods for converting image carrying charged particles to image carrying radiation principally in the blue and near-ultraviolet region of the spectrum and to stabilized rare earth phosphors characterized by having a continuous surface layer of the phosphors of the invention.Type: GrantFiled: April 11, 1977Date of Patent: October 27, 1981Assignee: Lockheed Missiles & Space Company, Inc.Inventors: Robert A. Buchanan, T. Grant Maple, Alden F. Sklensky
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Patent number: 4269907Abstract: An electrochemical cell is shown wherein anode 1 of a reactive metal having an insulating film 2 thereon is separated from cathode 6 by a non-conductive flow screen 4. A porous, expandable element 5 is positioned between screen 4 and cathode 6 to maintain essentially uniform dimensions of the electrolyte flow channel defined by screen 4 as the anode is consumed during cell operation. Preferably, when a multiplicity of cells are electrically connected together, a plurality of separator elements 8 between the respective anodes and cathodes are utilized to ensure that each cell in the multi-cell configuration is subject to essentially identical compression forces in assembly and during discharge.Type: GrantFiled: May 5, 1980Date of Patent: May 26, 1981Assignee: Lockheed Missiles & Space Company, Inc.Inventors: William R. Momyer, Ernest L. Littauer
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Patent number: 4254089Abstract: A method and apparatus for safely and economically converting sodium sludge and other dangerous wastes containing metallic sodium, lithium and potassium into products of economic value. The process reacts solid or molten wastes with an aqueous solution to yield products of the metal hydroxides, hydrogen gas and waste heat while consuming only water. Both scrap sodium and sodium sludge are acceptable feedstocks for this unique float/spray process.Type: GrantFiled: October 29, 1979Date of Patent: March 3, 1981Assignee: Lockheed Missiles & Space Company, Inc.Inventor: Donald J. Levy
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Patent number: 4200617Abstract: A method and apparatus for safely and economically converting sodium sludge and other dangerous wastes containing metallic sodium, lithium and potassium into products of economic value. The process reacts solid or molten wastes with an aqueous solution to yield products of the metal hydroxides, hydrogen gas and waste heat while consuming only water. Both scrap sodium and sodium sludge are acceptable feedstocks for this unique float/spray process.Type: GrantFiled: November 9, 1977Date of Patent: April 29, 1980Assignee: Lockheed Missiles & Space Co., Inc.Inventor: Donald J. Levy
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Patent number: 4180623Abstract: An electrically rechargeable battery comprising an inert cathode, a zinc anode and an aqueous alkaline electrolyte, for example, NaOH, in which said anode and cathode are immersed. The alkaline electrolyte in the vicinity of the cathode contains an alkali metal ferricyanide salt, such as K.sub.3 Fe(CN).sub.6 or Na.sub.3 Fe(CN).sub.6. Optionally, a mechanical separator is utilized between the anode and cathode to prevent gross mixing of the saturated electrolyte at the cathode with the electrolyte in the vicinity of the anode. Preferably, the separator is of the ion exchange type. During electrical discharge, at the anode and cathode, the battery produces soluble reaction products which are transported in the electrolyte to respective external storage tanks which increase battery capacity. During the charge cycle, the reverse conditions occur.Type: GrantFiled: July 28, 1978Date of Patent: December 25, 1979Assignee: Lockheed Missiles & Space Company, Inc.Inventor: George B. Adams
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Patent number: 4163084Abstract: In an electrochemical cell, a cathode having an essentially continuous layer of ruthenium on its surface which improves the performance of the cathode during the electrochemical reduction of chlorine, oxygen or peroxyl ions in an aqueous salt electrolyte.Type: GrantFiled: July 27, 1978Date of Patent: July 31, 1979Assignee: Lockheed Missiles & Space Company, Inc.Inventors: Keh-Chi Tsai, Ernest L. Littauer