Patents Assigned to Administration
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Patent number: 8702962Abstract: A gas sensor comprises a substrate layer; a pair of interdigitated metal electrodes, said electrodes include upper surfaces, the electrodes selected from the group consisting of Pt, Pd, Au, Ir, Ag, Ru, Rh, In, Os, and their alloys. A first layer of solid electrolyte staying in between electrode fingers and partially on said upper surfaces of said electrodes, said first layer selected from NASICON, LISICON, KSICON and ??-Alumina. A second layer of metal carbonate(s) as an auxiliary electrolyte engaging said upper surfaces of the electrodes and the first solid electrolyte. The metal carbonates selected from the group consisting of the following ions Na+, K+, Li+, Ag+, H+, Pb2+, Sr2+, Ba2+, and any combination thereof.Type: GrantFiled: August 20, 2008Date of Patent: April 22, 2014Assignee: The United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventors: Gary W. Hunter, Jennifer C. Xu
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Patent number: 8704654Abstract: A high temperature communications circuit includes a power conductor for concurrently conducting electrical energy for powering circuit components and transmitting a modulated data signal, and a demodulator for demodulating the data signal and generating a serial bit stream based on the data signal. The demodulator includes an absolute value amplifier for conditionally inverting or conditionally passing a signal applied to the absolute value amplifier. The absolute value amplifier utilizes no diodes to control the conditional inversion or passing of the signal applied to the absolute value amplifier.Type: GrantFiled: June 7, 2007Date of Patent: April 22, 2014Assignee: The United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventors: Michael J. Krasowski, Norman F. Prokop
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Patent number: 8704423Abstract: Embodiments of the invention provide a dielectric elastomer composite material comprising a plurality of elastomer-coated electrodes arranged in an assembly. Embodiments of the invention provide improved force output over prior DEs by producing thinner spacing between electrode surfaces. This is accomplished by coating electrodes directly with uncured elastomer in liquid form and then assembling a finished component (which may be termed an actuator) from coated electrode components.Type: GrantFiled: August 19, 2009Date of Patent: April 22, 2014Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Brian K. Stewart
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Patent number: 8706299Abstract: A robotic system includes a dexterous robot and a controller. The robot includes a plurality of robotic joints, actuators for moving the joints, and sensors for measuring a characteristic of the joints, and for transmitting the characteristics as sensor signals. The controller receives the sensor signals, and is configured for executing instructions from memory, classifying the sensor signals into distinct classes via the state classification module, monitoring a system state of the robot using the classes, and controlling the robot in the execution of alternative work tasks based on the system state. A method for controlling the robot in the above system includes receiving the signals via the controller, classifying the signals using the state classification module, monitoring the present system state of the robot using the classes, and controlling the robot in the execution of alternative work tasks based on the present system state.Type: GrantFiled: August 2, 2011Date of Patent: April 22, 2014Assignees: GM Global Technology Operations LLC, The United States of America as Represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Adam M. Sanders, Robert J. Platt, Jr., Nathaniel Quillin, Frank Noble Permenter, Joseph Pfeiffer
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Patent number: 8703019Abstract: A phosphor which emits light having high brightness, serves as an excellent orange or red phosphor whose light brightness is less decreased when exposed to an excitation source contains a crystal phase having the chemical composition expressed by the general formula [1]: (1?a?b)(Ln?pMII?1?pMIII?MIV?N3).a(MIV?(3n+2)/4NnO).b(AMIV?2N3)??[1] wherein Ln? represents a metal element selected from the group consisting of lanthanoids, Mn, and Ti; MnII? represents a divalent metal element except the Ln? element; MIII? represents a trivalent metal element; MIV? represents a tetravalent metal element; A represents a metal element selected from the group consisting of Li, Na, and K; 0<p?0.2; 0?a, 0?b, a+b>0, 0?n, and 0.002?(3n+2)a/4?0.9.Type: GrantFiled: May 22, 2012Date of Patent: April 22, 2014Assignees: Mitsubishi Chemical Corporation, Independent Administrative Institution National Institute for Materials ScienceInventors: Naoto Hirosaki, Takatoshi Seto, Naoto Kijima
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Patent number: 8703235Abstract: In the method of embodiments of the invention, the metal seeded carbon allotropes are reacted in solution forming zero valent metallic nanowires at the seeded sites. A polymeric passivating reagent, which selects for anisotropic growth is also used in the reaction to facilitate nanowire formation. The resulting structure resembles a porcupine, where carbon allotropes have metallic wires of nanometer dimensions that emanate from the seed sites on the carbon allotrope. These sites are populated by nanowires having approximately the same diameter as the starting nanoparticle diameter.Type: GrantFiled: April 8, 2011Date of Patent: April 22, 2014Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Robin E. Southward, Donavon Mark Delozier, Kent A. Watson, Joseph G. Smith, Sayata Ghose, John W. Connell
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Systems, apparatuses, and methods for using durable adhesively bonded joints for sandwich structures
Patent number: 8697216Abstract: Systems, methods, and apparatus for increasing durability of adhesively bonded joints in a sandwich structure. Such systems, methods, and apparatus includes an first face sheet and an second face sheet as well as an insert structure, the insert structure having a first insert face sheet, a second insert face sheet, and an insert core material. In addition, sandwich core material is arranged between the first face sheet and the second face sheet. A primary bondline may be coupled to the face sheet(s) and the splice. Further, systems, methods, and apparatus of the present disclosure advantageously reduce the load, provide a redundant path, reduce structural fatigue, and/or increase fatigue life.Type: GrantFiled: August 5, 2011Date of Patent: April 15, 2014Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Stanley S. Smeltzer, III, Eric C. Lundgren -
Patent number: 8696940Abstract: Metamaterials or artificial negative index materials (NIMs) have generated great attention due to their unique and exotic electromagnetic properties. One exemplary negative dielectric constant material, which is an essential key for creating the NIMs, was developed by doping ions into a polymer, a protonated poly(benzimidazole) (PBI). The doped PBI showed a negative dielectric constant at megahertz (MHz) frequencies due to its reduced plasma frequency and an induction effect. The magnitude of the negative dielectric constant and the resonance frequency were tunable by doping concentration. The highly doped PBI showed larger absolute magnitude of negative dielectric constant at just above its resonance frequency than the less doped PBI.Type: GrantFiled: September 29, 2010Date of Patent: April 15, 2014Assignee: United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Keith L. Gordon, Jin Ho Kang, Cheol Park, Peter T. Lillehei, Joycelyn S. Harrison
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Patent number: 8695430Abstract: Systems and methods that are capable of measuring pressure or temperature based on luminescence are discussed herein. These systems and methods are based on spin-allowed broadband luminescence of sensors with orthorhombic perovskite structures of rare earth aluminates doped with chromium or similar transition metals, such as chromium-doped gadolinium aluminate. Luminescence from these sensors can be measured to determine at least one of temperature or pressure, based on either the intense luminescence of these sensors, even at high temperatures, or low temperature techniques discussed herein.Type: GrantFiled: November 23, 2011Date of Patent: April 15, 2014Assignee: The United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventors: Jeffrey I. Eldridge, Matthew D. Chambers
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Patent number: 8699029Abstract: A method and apparatus for detecting trace gas concentrations in the atmosphere. An absorption signal is provided that includes collected sunlight that has undergone absorption by a trace gas. The absorption signal is mixed with laser light at a nearby frequency to the absorption signal. An amplitude of a resulting RF signal is proportional to the concentration of the trace gas.Type: GrantFiled: July 10, 2012Date of Patent: April 15, 2014Assignee: The United States of America as represented by the Administrator of the National Aeronautics Space AdministrationInventors: Emily W. Steel, Matthew L. McLinden
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Patent number: 8695915Abstract: One or more acoustic liners comprising internal chambers or passageways that absorb energy from a noise source on the aircraft are disclosed. The acoustic liners may be positioned at the ends of flaps of an aircraft wing to provide broadband noise absorption and/or dampen the noise producing unsteady flow features, and to reduce the amount of noise generated due to unsteady flow at the inboard and/or outboard end edges of a flap.Type: GrantFiled: March 12, 2012Date of Patent: April 15, 2014Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Michael G. Jones, Mehdi R. Khorrami, Meelan M. Choudhari, Brian M. Howerton
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Patent number: 8700358Abstract: The invention provides a method of obtaining the FBG data in final form (transforming the raw data into frequency and location data) by taking the raw FBG sensor data and dividing the data into a plurality of segments over time. By transforming the raw data into a plurality of smaller segments, processing time is significantly decreased. Also, by defining the segments over time, only one processing step is required. By employing this method, the refresh rate of FBG sensor systems can be improved from about 1 scan per second to over 20 scans per second.Type: GrantFiled: March 7, 2007Date of Patent: April 15, 2014Assignee: The United States of America as Represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Allen R. Parker, Jr.
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Patent number: 8695925Abstract: A system is provided for reducing aeroacoustic noise generated by an aircraft having wings equipped with trailing-edge flaps. The system includes a plurality of elastically deformable structures. Each structure is coupled to and along one of the side edges of one of the trailing-edge flaps, and is coupled to a portion of one of the wings that is adjacent to the one of the side edges. The structures elastically deform when the trailing-edge flaps are deployed away from the wings.Type: GrantFiled: December 15, 2011Date of Patent: April 15, 2014Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Mehdi R. Khorrami, David P. Lockard, James B. Moore, Ji Su, Travis L. Turner, John C. Lin, Karen M. Taminger, Seun K. Kahng, Scott A. Verden
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Patent number: 8697313Abstract: The invention is a novel solid oxide fuel cell (SOFC) stack comprising individual bi-electrode supported fuel cells in which a thin electrolyte is supported between electrodes of essentially equal thickness. Individual cell units are made from graded pore ceramic tape that has been created by the freeze cast method followed by freeze drying. Each piece of graded pore tape later becomes a graded pore electrode scaffold that subsequent to sintering, is made into either an anode or a cathode by means of appropriate solution and thermal treatment means. Each cell unit is assembled by depositing of a thin coating of ion conducting ceramic material upon the side of each of two pieces of tape surface having the smallest pore openings, and then mating the coated surfaces to create an unsintered electrode scaffold pair sandwiching an electrolyte layer.Type: GrantFiled: August 20, 2010Date of Patent: April 15, 2014Assignee: The United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventors: Thomas L. Cable, Stephen W Sofie
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Patent number: 8695420Abstract: A liquid level sensing system includes waveguides disposed in a liquid and distributed along a path with a gap between adjacent waveguides. A source introduces electromagnetic energy into the waveguides at a first end of the path. A portion of the electromagnetic energy exits the waveguides at a second end of the path. A detector measures the portion of the electromagnetic energy exiting the second end of the path.Type: GrantFiled: June 30, 2010Date of Patent: April 15, 2014Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Valentin Korman, John T. Wiley, Amanda G. Duffell
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Patent number: 8694183Abstract: The present invention is a Partial Automated Alignment and Integration System (PAAIS) used to automate the alignment and integration of space vehicle components. A PAAIS includes ground support apparatuses, a track assembly with a plurality of energy-emitting components and an energy-receiving component containing a plurality of energy-receiving surfaces. Communication components and processors allow communication and feedback through PAAIS.Type: GrantFiled: December 6, 2011Date of Patent: April 8, 2014Assignee: The United States of America as Represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Gary Wayne Kelley
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Patent number: 8694963Abstract: Systems, methods and apparatus are provided through which an evolutionary system is managed and viewed as a software product line. In some embodiments, the core architecture is a relatively unchanging part of the system, and each version of the system is viewed as a product from the product line. Each software product is generated from the core architecture with some agent-based additions. The result may be a multi-agent system software product line.Type: GrantFiled: November 29, 2011Date of Patent: April 8, 2014Assignee: The United States as represented by the Administrator of the National Aeronautics Space AdministrationInventors: Michael G. Hinchey, James L. Rash, Joaquin Pena
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Patent number: 8692562Abstract: A wireless in-plane strain and displacement sensor includes an electrical conductor fixedly coupled to a substrate subject to strain conditions. The electrical conductor is shaped between its ends for storage of an electric field and a magnetic field, and remains electrically unconnected to define an unconnected open-circuit having inductance and capacitance. In the presence of a time-varying magnetic field, the electrical conductor so-shaped resonates to generate harmonic electric and magnetic field responses. The sensor also includes at least one electrically unconnected electrode having an end and a free portion extending from the end thereof. The end of each electrode is fixedly coupled to the substrate and the free portion thereof remains unencumbered and spaced apart from a portion of the electrical conductor so-shaped. More specifically, at least some of the free portion is disposed at a location lying within the magnetic field response generated by the electrical conductor.Type: GrantFiled: August 1, 2011Date of Patent: April 8, 2014Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Marie Woodard
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Patent number: 8693828Abstract: A waveguide structure for a dual polarization waveguide includes a first flange member, a second flange member, and a waveguide member disposed in each of the first flange member and second flange member. The first flange member and the second flange member are configured to be coupled together in a spaced-apart relationship separated by a gap. The first flange member has a substantially smooth surface, and the second flange member has an array of two-dimensional pillar structures formed therein.Type: GrantFiled: May 10, 2011Date of Patent: April 8, 2014Assignee: The United States of America as represented by the Administrator of the National Aeronautics Space AdministrationInventors: Edward J. Wollack, Kongpop U-Yen, David T. Chuss
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Patent number: 8693002Abstract: A Fourier transform spectrometer (FTS) data acquisition system includes an FTS spectrometer that receives a spectral signal and a laser signal. The system further includes a wideband detector, which is in communication with the FTS spectrometer and receives the spectral signal and laser signal from the FTS spectrometer. The wideband detector produces a composite signal comprising the laser signal and the spectral signal. The system further comprises a converter in communication with the wideband detector to receive and digitize the composite signal. The system further includes a signal processing unit that receives the composite signal from the converter. The signal processing unit further filters the laser signal and the spectral signal from the composite signal and demodulates the laser signal, to produce velocity corrected spectral data.Type: GrantFiled: December 21, 2010Date of Patent: April 8, 2014Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Joel F. Campbell