Patents Represented by Attorney J. R. Manning
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Patent number: 4260166Abstract: A self-stabilizing radial face seal comprising an axial member, a primary seal ring juxtapositioned to a seal seat, at least one of said primary seal ring and seal seat being affixed to said axial member so as to rotate therewith, said primary seal ring having a front face which opposes a face of said seal seat, said seal having both high-pressure and low-pressure regions of fluid, said seal seat being provided with a porous ring-like circumferential structure in the face of said seal seat opposite said front face of said primary seal ring.Type: GrantFiled: November 17, 1978Date of Patent: April 7, 1981Inventors: Robert A. Administrator of the National Aeronautics and Space Administration, with respect to an invention of Frosch, Izhak Etsion
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Patent number: 4256093Abstract: A pump/valve unit for controlling the inflation and deflation of a urethral collar in a prosthetic urinary sphincter device is disclosed including a compressible bulb pump defining a reservoir made integral with a valve unit for implant wherein the valve unit includes a movable valve member operable by depression of a flexible portion of the valve unit housing for controlling fluid flow between the reservoir and collar and a pressure sensing means which operates the valve member to relieve an excess pressure in the collar should too much pressure be applied by the patient.Type: GrantFiled: October 12, 1978Date of Patent: March 17, 1981Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Curtis R. Helms, Harold M. Smyly
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Patent number: 4255495Abstract: The object of the invention is to provide a thermal barrier coating system for protecting metal surfaces at high temperature in normally corrosive environments.The thermal barrier coating system includes a metal alloy bond coating, the alloy containing nickel, cobalt, iron, or a combination of these metals. The system further includes a corrosion resistant thermal barrier oxide coating containing at least one alkaline earth silicate.The preferred oxides are calcium silicate, barium silicate, magnesium silicate, or combinations of these silicates.Type: GrantFiled: October 31, 1979Date of Patent: March 10, 1981Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Stanley R. Levine, Robert A. Miller, Philip E. Hodge
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Patent number: 4245768Abstract: A method for cold welding metal joints. In order to remove the contamination layer on the surface of the metal, an ion beam generator is used in a vacuum environment. A gas, such as xenon or argon, is ionized and accelerated toward the metal surface. The beam of gas effectively sputters away the surface oxides and contamination layer so that clean underlying metal is exposed in the area to be welded. The use of this method allows cold welding with minimal deformation. Both similar and dissimilar metals can be cold welded with this method.Type: GrantFiled: July 28, 1978Date of Patent: January 20, 1981Assignee: The Unites States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Bernard L. Sater
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Patent number: 4229196Abstract: Atomic hydrogen, for use as a fuel or as an explosive, is stored in the presence of a strong magnetic field in exfoliated layered compounds such as molybdenum disulfide or an elemental layer material such as graphite. The compound is maintained at liquid helium temperatures and the atomic hydrogen is collected on the surfaces of the layered compound which are exposed during delamination (exfoliation). The strong magnetic field and the low temperature combine to prevent the atoms of hydrogen from recombining to form molecules.Type: GrantFiled: February 6, 1979Date of Patent: October 21, 1980Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: John A. Woollam
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Patent number: 4227096Abstract: A microwave integrated circuit, comprised of one or more Josephson junctions and short sections of microstrip or stripline transmission line, is fabricated from thin layers of superconducting metal on a dielectric substrate. The short sections of transmission line are combined to form the elements of the circuit, and particularly, two microwave resonators. The Josephson junctions are located between the resonators, and the impedance of the Josephson junctions forms part of the circuitry that couples the two resonators. The microwave integrated circuit has an application in Josephson voltage standards. In this application, the device is asymmetrically driven at a selected frequency (approximately equal to the resonance frequency of the resonators), and a D.C. bias is applied to the junction. By observing the current-voltage characteristic of the junction, a precise voltage, proportional to the frequency of the microwave drive signal, is obtained.Type: GrantFiled: August 31, 1978Date of Patent: October 7, 1980Inventors: Robert A. Administrator of the National Aeronautics and Space Administration, with respect to an invention of Frosch, Louis B. Holdeman, Jaan Toots, Chu-Cheng Chang
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Patent number: 4218921Abstract: A method and apparatus for enhancing and shaping acoustical levitation forces in a single-axis acoustic resonance system wherein specially shaped drivers and reflectors are utilized to enhance the levitation force and better contain fluid substances by means of field shaping.Type: GrantFiled: July 13, 1979Date of Patent: August 26, 1980Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: William A. Oran, LeRoy H. Berge, Donald A. Reiss, Jerry L. Johnson
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Patent number: 4217633Abstract: A monolithie multijunction solar cell is modified by fabricating an integrated circuit inverter on the back of the cell to produce a device capable of generating an alternating current output. In another embodiment, integrated circuit power conditioning electronics is incorporated in a module containing a solar cell power supply.Type: GrantFiled: August 10, 1979Date of Patent: August 12, 1980Assignee: 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: 4215548Abstract: The present invention is directed to a free-piston regenerative hydraulic engine including a displacer piston which is driven pneumatically by a high-pressure or low-pressure gas. Actuation of the displacer piston circulates the working fluid through a heater, a regenerator and a cooler. The present invention includes an inertial mass such as a piston or a hydraulic fluid column to effectively store and supply energy during portions of the cycle. Power is transmitted from the working fluid to a hydraulic fluid across a diaphragm or lightweight piston to achieve a hydraulic power output. The displacer piston of the present invention may be driven pneumatically, hydraulically or electromagnetically. In addition, the displacer piston and the inertial mass of the present invention may be positioned on the same side of the diaphragm member or may be separated by the diaphragm member.Type: GrantFiled: October 12, 1978Date of Patent: August 5, 1980Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Donald G. Beremand
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Patent number: 4215592Abstract: A drive system characterized by a base supporting a pair of pillars arranged in spaced parallelism, a shaft extended between and supported by the pillars for rotation about the longitudinal axis thereof, a worm gear affixed to the shaft and supported thereby in coaxial relation therewith. A bearing housing of a sleeve-like configuration is concentrically related to the shaft and is supported thereby for free rotation with respect thereto. A first and a second normally quiescent drive train, alternatively activatable, is provided for imparting rotation into said bearing housing.Type: GrantFiled: August 4, 1978Date of Patent: August 5, 1980Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: John A. Calvert
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Patent number: 4214902Abstract: An iron alloy is provided which exhibits excellent strength and toughness characteristics at cryogenic temperatures. The alloy consists essentially of about 10 to 16 percent by weight nickel, about 0.1 to 1.0 percent by weight aluminum, and 0 to about 3 percent by weight copper, with the balance being essentially iron. The iron alloy is produced by a process which includes using cold rolling at room temperature and subsequent heat treatment at temperatures ranging from 400.degree. to 650.degree. C., and possesses a fracture toughness ranging from 200 to 230 ksi .sqroot.in. and yield strengths up to 230 ksi.Type: GrantFiled: January 25, 1979Date of Patent: July 29, 1980Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Joseph R. Stephens, Walter R. Witzke
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Patent number: 4214905Abstract: A composite material is described which will provide low friction surfaces for materials in rolling or sliding contact and is self-lubricating and oxidation resistant up to and in excess of about 930.degree. C. The composite is comprised of a metal component which lends strength and elasticity to the structure, a fluoride salt component which provides lubrication and, lastly, a glass component which not only provides oxidation protection to the metal but may also enhance the lubrication qualities of the composite.Type: GrantFiled: January 31, 1977Date of Patent: July 29, 1980Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Harold E. Sliney
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Patent number: 4212477Abstract: A circumferential shaft seal comprising two sealing rings held to a rotating shaft by means of a surrounding elastomeric band. The rings are segmented and are of a rigid sealing material such as carbon or a polymide and graphite fiber composite.Type: GrantFiled: March 31, 1976Date of Patent: July 15, 1980Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Lawrence P. Ludwig
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Patent number: 4211354Abstract: A method is provided for alleviating the stress damage in metallic matrix composites, such as laminated sheet or foil composites, wherein discontinuities are positively introduced into the interface between the layers so as to reduce the thermal stress produced by unequal expansion of the materials making up the composite. Although a plurality of discrete elements could be used to form one of the layers and thus carry out this purpose, the discontinuities are preferably produced by simply drilling holes in the metallic matrix layer or by forming grooves in a grid pattern in this layer.Type: GrantFiled: April 6, 1978Date of Patent: July 8, 1980Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Charles A. Hoffman, John W. Weeton, Norman W. Orth
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Patent number: 4204899Abstract: Cork-resin ablative insulation material is prepared in a form suitable for application to complex curved surfaces by mixing finely divided cork with a B-stage curable thermosetting resin, forming the resulting mixture into a block, B-stage curing the resin-containing block and slicing the block into sheets. The B-stage cured sheet is shaped to conform to the surface being insulated, and further curing is then performed. Curing of the resin only to B-stage before shaping enables application of sheet material to complex curved surfaces and avoids limitations and disadvantages presented in handling of fully cured sheet material.Type: GrantFiled: September 12, 1978Date of Patent: May 27, 1980Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Hill M. Walker, Max H. Sharpe, William G. Simpson
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Patent number: 4199937Abstract: A heat exchanger of increased effectiveness is disclosed. A porous metal matrix is disposed in a metal chamber or between walls through which a heat-transfer fluid is directed. The porous metal matrix has internal bonds and is bonded to the chamber in order to remove all thermal contact resistance within the composite structure. Utilization of the invention in a rocket chamber is disclosed as a specific use. Also disclosed is a method of constructing the heat exchanger.Type: GrantFiled: November 30, 1977Date of Patent: April 29, 1980Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Anthony Fortini, John M. Kazaroff
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Patent number: 4199650Abstract: An electron bombardment argon ion source is used to treat polyimide and fluorinated ethylene propylene polymers to form textured surfaces thereon. This improves the optical and electrical properties so that these polymers can be used in industrial and space applications.Type: GrantFiled: November 7, 1978Date of Patent: April 22, 1980Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Michael J. Mirtich, James S. Sovey
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Patent number: 4198232Abstract: Monotectic alloys having aligned spherical particles or rods of the minor component dispersed in a matrix of the major component are prepared by forming a melt containing predetermined amounts of the major and minor components of a chosen monotectic system, providing in the melt a dopant capable of breaking down the liquid-solid interface for the chosen alloy, and directionally solidifying the melt at a selected temperature gradient and a selected rate of movement of the liquid-solid interface (growth rate). Shaping of the minor component into spheres or rods and the spacing therebetween are controlled by the amount of dopant and the temperature gradient and growth rate values. Specific alloy systems include Al-Bi,Al-Pb and Zn-Bi, using a transition element such as iron.Type: GrantFiled: December 29, 1978Date of Patent: April 15, 1980Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Richard A. Parr, Mary H. Johnston, John C. McClure
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Patent number: 4193827Abstract: Atomic hydrogen, for use as a fuel or as an explosive, is stored in the presence of a strong magnetic field in exfoliated layered compounds such as molybdenum disulfide or an elemental layer material such as graphite. The compound is maintained at liquid temperatures and the atomic hydrogen is collected on the surfaces of the layered compound which are exposed during delamination (exfoliation). The strong magnetic field and the low temperature combine to prevent the atoms of hydrogen from recombining to form molecules.Type: GrantFiled: September 29, 1977Date of Patent: March 18, 1980Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: John A. Woollam
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Patent number: 4192910Abstract: There is disclosed an electricity producing cell of the reduction-oxidation (REDOX) type divided into two compartments by a membrane, each compartment containing a solid inert electrode. A ferrous/ferric couple in a chloride solution serves as a cathode fluid which is circulated through one of the compartments to produce a positive electric potential disposed therein. A chromic/chromous couple in a chloride solution serves as an anode fluid which is circulated through the second compartment to produce a negative potential on an electrode disposed therein. The electrode is an electrically conductive, inert material plated with copper, silver or gold. A thin layer of lead plates onto the copper, silver or gold layer when the cell is being charged, the lead ions being available from lead chloride which has been added to the anode fluid.Type: GrantFiled: November 29, 1978Date of Patent: March 11, 1980Inventors: Robert A. Administrator of the National Aeronautics and Space Administration, with respect to an invention of Frosch, Jose D. Giner, Kathleen J. Cahill