Patents Represented by Attorney, Agent or Law Firm Robert H. Earp, III
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Patent number: 8310671Abstract: An architecture for spontaneous Raman scattering (SRS) that utilizes a frame-transfer charge-coupled device (CCD) sensor operating in a subframe burst gating mode to realize time-resolved combustion diagnostics is disclosed. The technique permits all-electronic optical gating with microsecond shutter speeds (<5 ?s), without compromising optical throughput or image fidelity. When used in conjunction with a pair of orthogonally-polarized excitation lasers, the technique measures time-resolved vibrational Raman scattering that is minimally contaminated by problematic optical background noise.Type: GrantFiled: September 29, 2010Date of Patent: November 13, 2012Assignee: The United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventors: Quang-Viet Nguyen, David G Fischer, Jun Kojima
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Patent number: 8283172Abstract: A lunar dust simulant containing nanophase iron and a method for making the same. Process (1) comprises a mixture of ferric chloride, fluorinated carbon powder, and glass beads, treating the mixture to produce nanophase iron, wherein the resulting lunar dust simulant contains ?-iron nanoparticles, Fe2O3, and Fe3O4. Process (2) comprises a mixture of a material of mixed-metal oxides that contain iron and carbon black, treating the mixture to produce nanophase iron, wherein the resulting lunar dust simulant contains ?-iron nanoparticles and Fe3O4.Type: GrantFiled: February 24, 2010Date of Patent: October 9, 2012Assignee: The United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventors: Chin-cheh Hung, Jeremiah McNatt
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Patent number: 8264134Abstract: An ultraminiature light source using a double-spiral shaped tungsten filament includes end contact portions which are separated to allow for radial and length-wise unwinding of the spiral. The double-spiral filament is spaced relatively far apart at the end portions thereof so that contact between portions of the filament upon expansion is avoided. The light source is made by fabricating a double-spiral ultraminiature tungsten filament from tungsten foil and housing the filament in a ceramic package having a reflective bottom and a well wherein the filament is suspended. A vacuum furnace brazing process attaches the filament to contacts of the ceramic package. Finally, a cover with a transparent window is attached onto the top of the ceramic package by solder reflow in a second vacuum furnace process to form a complete hermetically sealed package.Type: GrantFiled: June 7, 2010Date of Patent: September 11, 2012Assignee: The United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventors: Margaret L. Tuma, Joseph S. Collura, Henry Helvajian, Michael D. Pocha, Glenn A. Meyer, Charles F. McConaghy, Barry L. Olsen, William W Hansen
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Patent number: 8163243Abstract: The system that operates in a zero gravity environment and has an integral ozone generating capability is disclosed. The system contributes to the control of metabolic water vapors in the air, and also provided disinfection of any resulting condensate within the system, as well as disinfection of the air stream that flows throughout the disclosed system.Type: GrantFiled: September 7, 2006Date of Patent: April 24, 2012Assignee: The United States of America as represented by the Administrator of National Aeronautics and Space AdminstrationInventor: Kenneth A. Burke
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Patent number: 8159669Abstract: A particle detector is provided, the particle detector including a spherical Cherenkov detector, and at least one pair of detector stacks. In an embodiment of the invention, the Cherenkov detector includes a sphere of ultraviolet transparent material, coated by an ultraviolet reflecting material that has at least one open port. The Cherenkov detector further includes at least one photodetector configured to detect ultraviolet light emitted from a particle within the sphere. In an embodiment of the invention, each detector stack includes one or more detectors configured to detect a particle traversing the sphere.Type: GrantFiled: December 20, 2010Date of Patent: April 17, 2012Assignee: The United States of America as represented by the Administrator of National Aeronautics and Space AdministrationInventors: John D. Wrbanek, Gustave C. Fralick, Susan Y. Wrbanek
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Patent number: 7999173Abstract: A solar panel cleaning device includes a solar panel having a plurality of photovoltaic cells arranged in rows and embedded in the solar panel with space between the rows. A transparent dielectric overlay is affixed to the solar panel. A plurality of electrode pairs each of which includes an upper and a lower electrode are arranged on opposite sides of the transparent dielectric and are affixed thereto. The electrodes may be transparent electrodes which may be arranged without concern for blocking sunlight to the solar panel. The solar panel may be a dielectric and its dielectric properties may be continuously and spatially variable. Alternatively the dielectric used may have dielectric segments which produce different electrical field and which affects the wind “generated.Type: GrantFiled: March 21, 2007Date of Patent: August 16, 2011Assignee: The United States of America as represented by the Administrator of National Aeronautics and Space AdministrationInventor: David E. Ashpis
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Patent number: 7990327Abstract: A method of manufacturing a cellular reflectarray antenna arranged in an m by n matrix of radiating elements for communication with a satellite includes steps of determining a delay ?m,n for each of said m by n matrix of elements of said cellular reflectarray antenna using sub-steps of: determining the longitude and latitude of operation, determining elevation and azimuth angles of the reflectarray with respect to the satellite and converting theta0 (?0) and phi0 (?0), determining ??m,n, the pointing vector correction, for a given inter-element spacing and wavelength, determining ??m,n, the spherical wave front correction factor, for a given radius from the central element and/or from measured data from the feed horn; and, determining a delay ?m,n for each of said m by n matrix of elements as a function of ??m,n and ??m,n.Type: GrantFiled: September 2, 2010Date of Patent: August 2, 2011Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Robert R Romanofsky
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Patent number: 7935601Abstract: A method is disclosed that provides a self-aligned nitrogen-implant particularly suited for a Junction Field Effect Transistor (JFET) semiconductor device preferably comprised of a silicon carbide (SiC). This self-aligned nitrogen-implant allows for the realization of durable and stable electrical functionality of high temperature transistors such as JFETs. The method implements the self-aligned nitrogen-implant having predetermined dimensions, at a particular step in the fabrication process, so that the SiC junction field effect transistors are capable of being electrically operating continuously at 500° C. for over 10,000 hours in an air ambient with less than a 10% change in operational transistor parameters.Type: GrantFiled: September 4, 2009Date of Patent: May 3, 2011Assignee: The United States of America as represented by the Administrator of National Aeronautics and Space AdministrationInventor: Philip G. Neudeck
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Patent number: 7923715Abstract: A nonvolatile nanoionic switch is disclosed. A thin layer of chalcogenide glass engages a substrate and a metal selected from the group of silver and copper photo-dissolved in the chalcogenide glass. A first oxidizable electrode and a second inert electrode engage the chalcogenide glass and are spaced apart from each other forming a gap therebetween. A direct current voltage source is applied with positive polarity applied to the oxidizable electrode and negative polarity applied to the inert electrode which electrodeposits silver or copper across the gap closing the switch. Reversing the polarity of the switch dissolves the electrodeposited metal and returns it to the oxidizable electrode. A capacitor arrangement may be formed with the same structure and process.Type: GrantFiled: December 16, 2008Date of Patent: April 12, 2011Assignee: The United States of America as represented by the Administrator of National Aeronautics and Space AdministrationInventors: James Nessel, Richard Lee
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Patent number: 7876276Abstract: A miniaturized antenna system is characterized non-destructively through the use of a scanner that measures its near-field radiated power performance. When taking measurements, the scanner can be moved linearly along the x, y and z axis, as well as rotationally relative to the antenna. The data obtained from the characterization are processed to determine the far-field properties of the system and to optimize the system. Each antenna is excited using a probe station system while a scanning probe scans the space above the antenna to measure the near field signals. Upon completion of the scan, the near-field patterns are transformed into far-field patterns. Along with taking data, this system also allows for extensive graphing and analysis of both the near-field and far-field data. The details of the probe station as well as the procedures for setting up a test, conducting a test, and analyzing the resulting data are also described.Type: GrantFiled: August 2, 2006Date of Patent: January 25, 2011Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Afroz J. Zaman, Richard Q. Lee, William G. Darby, Philip J. Barr, Kevin M Lambert, Felix A. Miranda
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Patent number: 7872750Abstract: A particle detector is provided, the particle detector including a spherical Cherenkov detector, and at least one pair of detector stacks. In an embodiment of the invention, the Cherenkov detector includes a sphere of ultraviolet transparent material, coated by an ultraviolet reflecting material that has at least one open port. The Cherenkov detector further includes at least one photodetector configured to detect ultraviolet light emitted from a particle within the sphere. In an embodiment of the invention, each detector stack includes one or more detectors configured to detect a particle traversing the sphere.Type: GrantFiled: September 30, 2008Date of Patent: January 18, 2011Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: John D. Wrbanek, Gustave C. Fralick, Susan Y. Wrbanek
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Patent number: 7813406Abstract: An optical pulse stretcher and a mathematical algorithm for the detailed calculation of its design and performance is disclosed. The optical pulse stretcher has a plurality of optical cavities, having multiple optical reflectors such that an optical path length in each of the optical cavities is different. The optical pulse stretcher also has a plurality of beam splitters, each of which intercepts a portion of an input optical beam and diverts the portion into one of the plurality of optical cavities. The input optical beam is stretched and a power of an output beam is reduced after passing through the optical pulse stretcher and the placement of the plurality of optical cavities and beam splitters is optimized through a model that takes into account optical beam divergence and alignment in the pluralities of the optical cavities.Type: GrantFiled: April 13, 2006Date of Patent: October 12, 2010Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Quang-Viet Nguyen, Jun Kojima
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Patent number: 7791552Abstract: A method of manufacturing a cellular reflectarray antenna arranged in an m by n matrix of radiating elements for communication with a satellite includes steps of determining a delay ?m,n for each of said m by n matrix of elements of said cellular reflectarray antenna using sub-steps of: determining the longitude and latitude of operation, determining elevation and azimuth angles of the reflectarray with respect to the satellite and converting theta0 (?0) and phi0 (?0), determining ??m,n, the pointing vector correction, for a given inter-element spacing and wavelength, determining ??m,n, the spherical wave front correction factor, for a given radius from the central element and/or from measured data from the feed horn; and, determining a delay ?m,n for each of said m by n matrix of elements as a function of ??m,n and ??m,n..Type: GrantFiled: October 12, 2007Date of Patent: September 7, 2010Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Robert R Romanofsky
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Patent number: 7749341Abstract: A composition of the invention is a high temperature shape memory alloy having high work output, and is made from (Ni+Pt+Y)xTi(100-x), wherein x is present in a total amount of 49-55 atomic %, Pt is present in a total amount of 10-30 atomic %, Y is one or more of Au, Pd, and Cu and is present in a total amount of 0 to 10 atomic %. The alloy has a matrix phase wherein the total concentration of Ni, Pt, and the one or more of Pd, Au, and Cu is greater than 50 atomic %.Type: GrantFiled: March 6, 2006Date of Patent: July 6, 2010Assignee: The United States of America as represented by the Administrator of National Aeronautics and Space AdministrationInventors: Ronald Dean Noebe, Susan L. Draper, Michael V. Nathal, Edwin A. Crombie
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Patent number: 7704622Abstract: This invention relates to a series of organic/inorganic hybrid polymers that are easy to fabricate into dimensionally stable films with good ion-conductivity over a wide range of temperatures for use in a variety of applications. The polymers are prepared by the reaction of amines, preferably diamines and mixtures thereof with monoamines with epoxy-functionalized alkoxysilanes. The products of the reaction are polymerized by hydrolysis of the alkoxysilane groups to produce an organic-containing silica network. Suitable functionality introduced into the amine and alkoxysilane groups produce solid polymeric membranes which conduct ions for use in fuel cells, high-performance solid state batteries, chemical sensors, electrochemical capacitors, electro-chromic windows or displays, analog memory devices and the like.Type: GrantFiled: August 26, 2004Date of Patent: April 27, 2010Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Maryann B. Meador, James D. Kinder
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Patent number: 7688117Abstract: A circuit topography is presented which is used to create usable digital logic gates using N (negatively doped) channel Junction Field Effect Transistors (JFETs) and load resistors, level shifting resistors, and supply rails whose values are based on the direct current (DC) parametric distributions of those JFETs. This method has direct application to the current state of the art in high temperature, for example 300° C. to 500° C. and higher, silicon carbide (SiC) device production. The ability to produce inverting and combinatorial logic enables the production of pulse and edge triggered latches. This scale of logic synthesis would bring digital logic and state machine capabilities to devices operating in extremely hot environments, such as the surface of Venus, near hydrothermal vents, within nuclear reactors (SiC is inherently radiation hardened), and within internal combustion engines.Type: GrantFiled: April 21, 2008Date of Patent: March 30, 2010Assignee: The United States of America as represented by the Administrator of National Aeronautics and Space AdministrationInventor: Michael J. Krasowski
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Patent number: 7624566Abstract: A Hall effect plasma accelerator includes inner and outer electromagnets, circumferentially surrounding the inner electromagnet along a thruster centerline axis and separated therefrom, inner and outer magnetic conductors, in physical connection with their respective inner and outer electromagnets, with the inner magnetic conductor having a mostly circular shape and the outer magnetic conductor having a mostly annular shape, a discharge chamber, located between the inner and outer magnetic conductors, a magnetically conducting back plate, in magnetic contact with the inner and outer magnetic conductors, and a combined anode electrode/gaseous propellant distributor, located at a bottom portion of the discharge chamber. The inner and outer electromagnets, the inner and outer magnetic conductors and the magnetically conducting back plate form a magnetic circuit that produces a magnetic field that is largely axial and radially symmetric with respect to the thruster centerline.Type: GrantFiled: January 18, 2005Date of Patent: December 1, 2009Assignee: The United States of America as represented by the Administrator of National Aeronautics and Space AdministrationInventors: David H. Manzella, David T. Jacobson, Robert S. Jankovsky, Richard Hofer, Peter Peterson
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Container and method for preventing leakage therefrom through isolating deformation in the container
Patent number: 6793088Abstract: A container and method for preventing leakage therefrom through isolating deformation in the container caused by external forces. The container comprises a container wall having an opening therein, the opening capable of receiving a closure bushing with a sealing member wedged between the closure bushing and the container wall, and a weakened portion of the container wall not in wedged engagement with the sealing member capable of bending in response to an external force so as not to deform the portion of the container wall in wedged engagement with the sealing member.Type: GrantFiled: February 8, 2002Date of Patent: September 21, 2004Assignee: Rieke CorporationInventor: Gary M. Baughman -
Patent number: 6722686Abstract: A device for closing the socket of a trailer hitch, generally called a coupler lock, generally comprises a locking bar and a base having a plug member, a locking bar-receiving aperture, and an integral locking means for lockingly engaging the locking bar within aperture. When the coupler lock is attached to a trailer coupler, the trailer hitch socket is not accessible without removing the coupler lock with the appropriate key. Thus, theft of an unattended trailer is deterred due to the difficulty in attempting to remove the locking device. Providing a coupler lock having an integral locking mechanism better deters the tampering with or removal of the locking mechanism to remove the coupler lock from the trailer hitch as is possible in the art.Type: GrantFiled: May 1, 2002Date of Patent: April 20, 2004Assignee: Cequent Trailer Products, Inc.Inventor: Tim Vander Koy
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Patent number: RE43880Abstract: This invention relates to the composition and a solvent-free process for preparing novel imide oligomers and polymers specifically formulated with effective amounts of a dianhydride such as 2,3,3?,4-biphenyltetra carboxylic dianydride (a-BPDA), at least one aromatic diamine and an endcapped of 4-phenylethynylphthalic anhydride (PEPA) or nadic anhydride to produce imide oligomers that possess a low-melt viscosity of 1-60 poise at 260-280° C. When the imide oligomer melt is cured at about 371° C. in a press or autoclave under 100-500 psi, the melt resulted in a thermoset polyimide having a glass transition temperature (Tg) equal to and above 310° C. A novel feature of this process is that the monomers; namely the dianhydrides, diamines and the endcaps, are melt processable to form imide oligomers at temperatures ranging between 232-280° C. (450-535° F.) without any solvent.Type: GrantFiled: May 8, 2006Date of Patent: December 25, 2012Assignee: The United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventor: Chun-Hua Chuang