Patents Represented by Attorney James A. Mackin
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Patent number: 5635654Abstract: A particulate reinforced NiAl-AlN composite alloy has a NiAl matrix and greater than about 13 volume percent fine particles of AlN within the matrix. The particles preferably have a diameter from about 15 nanometers to about 50 nanometers. The particulate reinforced NiAl-AlN composite alloy may be prepared by cryomilling prealloyed NiAl in liquid nitrogen using grinding media having a diameter of from about 2 mm to about 6 mm at an impeller speed of from about 450 RPM to about 800 RPM. The cryomilling may be done for a duration of from about 4 hours to about 20 hours to obtain a cryomilled powder. The cryomilled powder may be consolidated to form the particulate reinforced NiAl-AlN composite alloy. The particulate reinforced alloy can further include a toughening alloy. The toughening alloy may include NiCrAlY, FeCrAY and FeAl.Type: GrantFiled: May 5, 1994Date of Patent: June 3, 1997Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Mohan G. Hebsur, John D. Whittenberger, Carl E. Lowell
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Patent number: 5429997Abstract: A pest resistant molybdenum disilicide composition is provided for use in high temperature structural applications. The composition includes molybdenum disilicide and silicon nitride and can be used to prepare improved reinforced composites.Type: GrantFiled: April 7, 1993Date of Patent: July 4, 1995Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Mohan G. Hebsur
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Patent number: 5412429Abstract: Digital data coders/decoders are used extensively in video transmission. A digitally encoded video signal is separated into subbands. Separating the video into subbands allows transmission at low data rates. Once the data is separated into these subbands it can be coded and then decoded by statistical coders such as the Lempel-Ziv based coder.Type: GrantFiled: March 11, 1993Date of Patent: May 2, 1995Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Daniel R. Glover
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Patent number: 5371110Abstract: An ion exchange polymer comprised of an alkali metal or alkaline earth metal salt of a poly(carboxylic acid) in a poly(vinyl acetal) matrix is described. The polymer is made by treating a mixture made of poly(vinyl alcohol) and poly(acrylic acid) with a suitable aldehyde and an acid catalyst to cause acetalization with some cross-linking. The material is then subjected to an alkaline aqueous solution of an alkali metal salt or an alkali earth metal salt. All of the film forming and cross-linking steps can be carried out simultaneously, if desired.Type: GrantFiled: June 21, 1993Date of Patent: December 6, 1994Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Warren H. Philipp, Kenneth W. Street, Jr.
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Patent number: 5363800Abstract: This invention is a method for the controlled growth of single-crystal semiconductor-device-quality films of SiC polytypes on vicinal (0001) SiC wafers with low tilt angles. Both homoepitaxial and heteroepitaxial SiC films can be produced on the same wafer. In particular, 3C-SiC and 6H-SiC films can be produced within selected areas of the same 6H-SiC wafer.Type: GrantFiled: November 9, 1992Date of Patent: November 15, 1994Assignee: The United States of America as represented by the United States National Aeronautics and Space AdministrationInventors: David J. Larkin, Powell, J. Anthony
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Patent number: 5334733Abstract: Synthetic procedures to tetraalkyls, tetraacids and dianhydrides substituted 1,1,1-triaryl-2,2,2-trifluoroethanes which comprises: (1) 1,1-bis(dialkylaryl)-1-aryl-2,2,2-trifluoroethane, (2) 1,1-bis(dicarboxyaryl)-1-aryl-2,2,2-trifluoroethane or (3) cyclic dianhydride or diamine of 1,1-bis(dialkylaryl)-1-aryl-2,2,2-trifluoroethanes. The synthesis of (1) is accomplished by the condensation reaction of an aryltrifluoromethyl ketone with a dialkylaryl compound. The synthesis of (2) is accomplished by oxidation of (1). The synthesis dianhydride of (3) is accomplished by the conversion of (2) to its corresponding cyclic dianhydride. The synthesis of the diamine is accomplished by the similar reaction of an aryltrifluoromethyl ketone with aniline or alkyl substituted or disubstituted anilines. Also, other derivatives of the above are formed by nucleophilic displacement reactions.Type: GrantFiled: January 17, 1992Date of Patent: August 2, 1994Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: William B. Alston, Roy F. Gratz
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Patent number: 5332239Abstract: A high-temperature hybrid seal is constructed of multiple elements to meet the many demands placed on the seal. The primary elements are: a central high-temperature bellows, a braided ceramic sheath covering the bellows, an outer abrasion resistant sheath covering the ceramic sheath, and a structurally-sound seal-end termination.Type: GrantFiled: January 22, 1993Date of Patent: July 26, 1994Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Bruce M. Steinetz, Paul J. Sirocky
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Patent number: 5330590Abstract: Cr.sub.3 Si is alloyed with molybdenum which produces a two-phase microstructure of (Cr,Mo).sub.3 Si and (Cr,Mo).sub.5 Si.sub.3. About 50 weight percent of molybdenum is present in the alloy. The alloy forms two protective oxides over a wide range of temperatures. Chromium and molybdenum oxide volatize under flowing air at high temperatures above 1200.degree. C. which facilitates the formation of SiO.sub.2 on the surface. Below 1200.degree. C. Cr.sub.2 O.sub.3 is formed. The new alloy has excellent high temperature strength and creep properties.Type: GrantFiled: May 26, 1993Date of Patent: July 19, 1994Assignee: The United States of America, as represented by the Administrator of the National Aeronautics & Space AdministrationInventor: Sai V. Raj
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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