Patents Represented by Attorney Gene E. Shook
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Patent number: 5326172Abstract: A method and apparatus for detecting the temperature of gray and non-gray bodies in the presence of interfering radiation. A gray body has a constant emissivity less than 1 and a non-gray body has an emissivity which varies with wavelength. The emissivity and reflectivity of the surface is determined over a range of wavelengths. Spectra are also measured of the extraneous interference radiation source and the surface of the object to be measured in the presence of the extraneous interference radiation source. An auxiliary radiation source is used to determine the reflectivity of the surface and also the emissivity. The measured spectrum of the surfaces in the presence of the extraneous interference radiation source is set equal to the emissivity of the surface multiplied by a Planck function containing a temperature term T plus the surface reflectivity multiplied by the spectrum of the extraneous interference radiation source. The equation is then solved for T to determine the temperature of the surface.Type: GrantFiled: December 14, 1992Date of Patent: July 5, 1994Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Daniel L. P. Ng
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Patent number: 5325661Abstract: The present invention generally relates to providing an improved jet mixer noise suppressor for high speed jets that rapidly mixes high speed air flow with a lower speed air flow, and more particularly, relates to an improved jet mixer noise suppressor that uses feedback of acoustic waves produced by the interaction of sheer flow instability waves with an obstacle downstream of the jet nozzle.Type: GrantFiled: April 14, 1993Date of Patent: July 5, 1994Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Edward J. Rice
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Patent number: 5322573Abstract: The invention features a thin light transmissive layer of the ternary semiconductor indium aluminum arsenide (InAlAs) as a front surface passivation or "window" layer for p-on-n InP solar cells. The window layers of the invention effectively reduce front surface recombination of the object semiconductors thereby increasing the efficiency of the cells.Type: GrantFiled: October 2, 1992Date of Patent: June 21, 1994Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Raj K. Jain, Geoffrey A. Landis
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Patent number: 5322924Abstract: Addition polyimide resins having improved thermo-oxidative stability and enhanced processability are prepared by the reaction of a mixture of monomers comprising a non-planar polyphenyl diamine (a), a diester of tetracarboxylic acid or the corresponding dianhydride (b) and an end-capping agent (c), or a diamine (d), a non-planar polyphenyl diester or dianhydride of a tetracarboxylic acid (e) and an end-capping agent (c).Type: GrantFiled: October 7, 1991Date of Patent: June 21, 1994Assignee: The United States of America as represented by the United States National Aeronautics and Space AdministrationInventors: Chun-Hua K. Chuang, Raymond D. Vannucci
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Patent number: 5316080Abstract: Gas derived graphite fibers generated by the decomposition of an organic gas are joined with a suitable binder. This produces a high thermal conductivity composite material which passively conducts heat from a source, such as a semiconductor, to a heat sink.The fibers may be intercalated. The intercalate can be halogen or halide salt, alkaline metal, or any other species which contributes to the electrical conductivity improvement of the graphite fiber.The fibers are bundled and joined with a suitable binder to form a high thermal conductivity composite material device. The heat transfer device may also be made of intercalated highly oriented pyrolytic graphite and machined, rather than made of fibers.Type: GrantFiled: February 10, 1993Date of Patent: May 31, 1994Assignee: The United States of America as represented by the Administrator of the National Aeronautics & Space AdministrationInventors: Bruce A. Banks, James R. Gaier
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Patent number: 5314247Abstract: A plug-type heat flux gauge can simultaneously measure heat flux on two opposite surfaces of thick or very thin convection or impingement cooled metal walls. The gauge is capable of continuously measuring transient and steady heat flux under transient and steady state gauge temperature operating conditions. The length of the gauge extends through the entire thickness of the material. A non-linear temperature gradient through the gauge can be measured by attaching 3-5 thermocouples along the length of the gauge.Type: GrantFiled: April 16, 1993Date of Patent: May 24, 1994Assignee: The United States of America as represented by the Administrator of the National Aeronautics & Space AdministrationInventors: Curt H. Liebert, John Koch, Jr.
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Patent number: 5312685Abstract: Structures composed at least partially of an organic substrate may be protected from oxidation by applying a catalyst onto said substrate for promoting the combination of atomic oxygen to molecular oxygen. The structure may also be protected by applying both a catalyst and an atomic oxygen shielding layer onto the substrate. The structures to be protected include spacecraft surfaces.Type: GrantFiled: July 6, 1992Date of Patent: May 17, 1994Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Bruce A. Banks, Sharon K. Rutledge
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Patent number: 5302465Abstract: A thermal barrier coating system consists of two layers of a zirconia-yttria ceramic. The first layer is applied by low pressure plasma spraying. The second layer is applied by conventional atmospheric pressure plasma spraying. This facilitates the attachment of a durable thermally insulating ceramic coating directly t the surface of a highly oxidation resistant NiAl-based intermetallic alloy after the alloy has been preoxidized to promote the formation of a desirable Al.sub.2 O.sub.3 scale.Type: GrantFiled: October 26, 1992Date of Patent: April 12, 1994Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Robert A. Miller, Joseph Doychak
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Patent number: 5297384Abstract: A wave rotor system includes a wave rotor coupled to first and second end plates. Special ports are provided, one in each of the first and second end plates, to cancel expansion waves generated by the release of working fluid from the wave rotor. One of the expansion waves is reflected in the wave rotor from a reflecting portion, and provided to the special port in the second end plate. Fluid present at the special port in the second end plate has a stagnation pressure and mass flow which is substantially the same as that of the cells of the wave rotor communicating with such special port. This allows for cancellation of the expansion wave generated by the release of working fluid from the wave rotor. The special port in the second end plate has a first end corresponding substantially to the head of the expansion wave, and a second end corresponding substantially to the tail of the expansion wave.Type: GrantFiled: July 6, 1993Date of Patent: March 29, 1994Assignee: The United States of America as represented by the Administrator of the National Aeronautics & Space AdministrationInventor: Daniel E. Paxson
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Patent number: 5290121Abstract: Service equipment for use in hostile environments includes a detachable service unit secured to a stationary service unit. The detachable service unit includes a housing with an exterior plate, a power control interface for connection to an exterior power source, locating pins located in said exterior plate, an electrical connector in the exterior plate electrically coupled to said power control interface, and a pair of clamping receptacles formed in the exterior plate and located on adjacent opposite edges of the exterior plate. The stationary unit includes an electrical connector for connection to the electrical connector of the detachable service unit, a clamping apparatus for clamping and unclamping the detachable service unit from the stationary unit, a base clamp assembly for mounting the clamping apparatus onto the stationary unit, and locating pin holes for receiving the locating pins and aligning the detachable service unit onto the stationary unit.Type: GrantFiled: May 28, 1992Date of Patent: March 1, 1994Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: James L. Dolce, Andrew L. Gordan
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Patent number: 5286471Abstract: Graphite fluoride is produced from graphitized carbon. A bromine iodine mixture reacts with graphitized carbon to produce iodine intercalated graphitized carbon that is then exposed to fluorine.Type: GrantFiled: May 15, 1992Date of Patent: February 15, 1994Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Ching-Cheh Hung
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Patent number: 5286162Abstract: The present invention is directed to a method and apparatus for improving the flow range in centrifugal pumps and compressors. Bleed holes are introduced into a volute tongue of a centrifugal pump or compressor thereby providing a double acting means of boundary layer control at the volute tongue.Type: GrantFiled: January 4, 1993Date of Patent: February 15, 1994Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Joseph P. Veres
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Patent number: 5284290Abstract: NiAl is preheated to a temperature between 1530.degree. C. and 1638.degree. C. causing some of the aluminum to evaporate along the faying surfaces thereby forming a glazed layer of nickel rich self-generated filler metal. The glazed faying surfaces are placed in contact, heated to 1530.degree. C. to 1570.degree. C., and pressed together to form a fusion weld.Type: GrantFiled: April 23, 1993Date of Patent: February 8, 1994Assignee: The United States of America as represented by the Adminstrator of the National Aeronautics and Space AdministrationInventors: Thomas J. Moore, Joseph M. Kalinowski
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Patent number: 5281559Abstract: A fiber-reinforced composite composed of a B.sub.a O--Al.sub.2 O.sub.3 --2SiO.sub.2 (BAS) glass ceramic matrix is reinforced with CVD silicon carbide continuous fibers. A slurry of BAS glass powders is prepared and celsian seeds are added during ball melting. The slurry is cast into tapes which are cut to the proper size.Continuous CVD-SiC fibers are formed into mats of the desired size. The matrix tapes and the fiber mats are alternately stacked in the proper orientation. This tape-mat stack is warm pressed to produce a "green" composite.The "green" composite is then heated to an elevated temperature to burn out organic constituents. The remaining interim material is then hot pressed to form a silicon carbide fiber-reinforced celsian (BAS) glass-ceramic matrix composite which may be machined to size.Type: GrantFiled: June 30, 1993Date of Patent: January 25, 1994Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Narottam P. Bansal
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Patent number: 5280174Abstract: Atomic oxygen atoms are routed to a material through a sufficiently tortuous path so that vacuum ultraviolet radiation is obstructed from arriving at the surface of the material. However, the material surface continues to be exposed to the atomic oxygen.Type: GrantFiled: January 25, 1993Date of Patent: January 18, 1994Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Bruce A. Banks, Sharon K. Rutledge
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Patent number: 5275670Abstract: A thermocouple having an electropositive leg formed of a noble metal-Al alloy and an electronegative leg electrically joined at respective ends thereof to form a thermocouple junction. The thermocouple provides for accurate and reproducible measurement of high temperatures (600.degree.-1300.degree. C.) in inert, oxidizing, or reducing environments, gases or vacuum. Furthermore, the thermocouple circumvents the need for expensive, strategic precious metals such as rhodium as a constituent component. Selective oxidation of rhodium is also thereby precluded.Type: GrantFiled: July 6, 1993Date of Patent: January 4, 1994Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: James L. Smialek, Michael G. Gedwill
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Patent number: 5267432Abstract: A wave rotor system includes a wave rotor coupled to first and second end plates. Special ports are provided, one in each of the first and second end plates, to cancel expansion waves generated by the release of working fluid from the wave rotor. One of the expansion waves is reflected in the wave rotor from a reflecting portion, and provided to the special port in the second end plate. Fluid present at the special port in the second end plate has a stagnation pressure and mass flow which is substantially the same as that of the cells of the wave rotor communicating with such special port. This allows for cancellation of the expansion wave generated by the release of working fluid from the wave rotor. The special port in the second end plate has a first end corresponding substantially to the head of the expansion wave, and a second end corresponding substantially to the tail of the expansion wave.Type: GrantFiled: May 26, 1992Date of Patent: December 7, 1993Assignee: The United States of America as represented by the Administrator of the National Aeronautics & Space AdministrationInventor: Daniel E. Paxson
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Patent number: 5260124Abstract: Highly conducting lightweight hybrid materials are obtained by weaving strands of carbon or graphite fibers into a 2-dimensional fabric-like structure, depositing a layer of carbon onto the fibers of the fabric-like structure, heating the fabric-like structure to graphitize the carbon layer and intercalating the graphitized carbon layer. Composite materials for use in lightning strike protection are composed of at least one layer of the highly conducting lightweight hybrid material and at least one layer of traditional composite materials.Type: GrantFiled: November 25, 1991Date of Patent: November 9, 1993Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: James R. Gaier
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Patent number: 5256451Abstract: The use of guanidine salts of organic fatty acids (guanidine soaps) as vehicles and binders for coating substrate surfaces is disclosed. Being completely organic, the guanidine soaps can be burned off leaving no undesirable residue. Of special interest is the use of guanidine 2-ethyl hexanoate as the vehicle and binder for coating problematic surfaces such as in coating alumina fibers with platinum or zirconia. For this application the guanidine soap is used as a melt. For other applications the guanidine soap may be use in a solution with a variety of solvents, the solution containing chlorometalates or powdered metals, refractories or ceramics.Type: GrantFiled: March 13, 1992Date of Patent: October 26, 1993Assignee: The United States of America as represented by the United States National Aeronautics and Space AdministrationInventors: Warren H. Philipp, Lisa C. Veitch, Martha H. Jaskowiak
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Patent number: 5256610Abstract: Oxides having a composition of (Ba.sub.1-x Sr.sub.x)O--Al.sub.2 O.sub.3 --2SiO.sub.2 are used as sintering aids for producing an improved silicon nitride ceramic material. The x must be greater than 0 to insure the formation of the stable monoclinic celsian glass phase.Type: GrantFiled: November 27, 1992Date of Patent: October 26, 1993Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Narottam P. Bansal, Stanley R. Levine, William A. Sanders