Patents Assigned to Administration
  • Patent number: 8691612
    Abstract: Provided is a method of enhancing thermoelectric performance by surrounding crystalline semiconductors with nanoparticles by contacting a bismuth telluride material with a silver salt under a substantially inert atmosphere and a temperature approximately near the silver salt decomposition temperature; and recovering a metallic bismuth decorated material comprising silver telluride crystal grains.
    Type: Grant
    Filed: March 5, 2012
    Date of Patent: April 8, 2014
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Hyun-Jung Kim, Sang Hyouk Choi, Glen C. King, Yeonjoon Park, Kunik Lee
  • Patent number: 8687742
    Abstract: An ensemble detector uses calibrated noise references to produce ensemble sets of data from which properties of non-stationary processes may be extracted. The ensemble detector comprising: a receiver; a switching device coupled to the receiver, the switching device configured to selectively connect each of a plurality of reference noise signals to the receiver; and a gain modulation circuit coupled to the receiver and configured to vary a gain of the receiver based on a forcing signal; whereby the switching device selectively connects each of the plurality of reference noise signals to the receiver to produce an output signal derived from the plurality of reference noise signals and the forcing signal.
    Type: Grant
    Filed: June 7, 2011
    Date of Patent: April 1, 2014
    Assignee: The United Sates of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Paul E. Racette
  • Patent number: 8685576
    Abstract: The present invention relates to an electrically conductive membrane that can be configured to be used in fuel cell systems to act as a hydrophilic water separator internal to the fuel cell, or as a water separator used with water vapor fed electrolysis cells, or as a water separator used with water vapor fed electrolysis cells, or as a capillary structure in a thin head pipe evaporator, or as a hydrophobic gas diffusion layer covering the fuel cell electrode surface in a fuel cell.
    Type: Grant
    Filed: September 25, 2007
    Date of Patent: April 1, 2014
    Assignee: The United States of America as Represented by the Administrator of National Aeronautics and Space Administration
    Inventor: Kenneth Alan Burke
  • Patent number: 8683807
    Abstract: A jet engine exhaust nozzle flow effector is a chevron formed with a radius of curvature with surfaces of the flow effector being defined and opposing one another. At least one shape memory alloy (SMA) member is embedded in the chevron closer to one of the chevron's opposing surfaces and substantially spanning from at least a portion of the chevron's root to the chevron's tip.
    Type: Grant
    Filed: April 28, 2011
    Date of Patent: April 1, 2014
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Travis L. Turner, Roberto J. Cano, Richard J. Silox, Ralph D. Buehrle, Christopher M. Cagle, Randolph H. Cabell, George C. Hilton
  • Patent number: 8685268
    Abstract: Disclosed herein is a textured substrate comprising a base comprising silicon, the base having a plurality of needle like structures depending away from the base, wherein at least one of the needle like structures has a depth of greater than or equal to about 50 micrometers determined perpendicular to the base, and wherein at least one of the needle like structures has a width of less than or equal to about 50 micrometers determined parallel to the base. An anode and a lithium ion battery comprising the textured substrate, and a method of producing the textured substrate are also disclosed.
    Type: Grant
    Filed: May 16, 2013
    Date of Patent: April 1, 2014
    Assignee: The United States of America as Represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Karl Y. Yee, Andrew P. Homyk
  • Patent number: 8679642
    Abstract: A first material with a known maximum temperature of operation is coated with a second material on at least one surface of the first material. The coating has a melting temperature that is greater than the maximum temperature of operation of the first material. The coating is heated to its melting temperature until the coating flows into any cracks in the first material's surface.
    Type: Grant
    Filed: September 26, 2013
    Date of Patent: March 25, 2014
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Stephen W. Smith, John A. Newman, Robert S. Piascik, Edward H. Glaessgen
  • Patent number: 8679300
    Abstract: An integrated production apparatus for production of boron nitride nanotubes via the pressure vapor-condenser method. The apparatus comprises: a pressurized reaction chamber containing a continuously fed boron containing target having a boron target tip, a source of pressurized nitrogen and a moving belt condenser apparatus; a hutch chamber proximate the pressurized reaction chamber containing a target feed system and a laser beam and optics.
    Type: Grant
    Filed: September 22, 2011
    Date of Patent: March 25, 2014
    Assignees: Jefferson Science Associates, LLC, The United States of America as represented by the Administrator of Nasa
    Inventors: Michael W. Smith, Kevin C. Jordan
  • Patent number: 8680749
    Abstract: A novel full piezoelectric multilayer stacked hybrid actuation/transduction system. The system demonstrates significantly-enhanced electromechanical performance by utilizing the cooperative contributions of the electromechanical responses of multilayer stacked negative and positive strain components. Both experimental and theoretical studies indicate that for this system, the displacement is over three times that of a same-sized conventional flextensional actuator/transducer. The system consists of at least 2 layers which include electromechanically active components. The layers are arranged such that when electric power is applied, one layer contracts in a transverse direction while the second layer expands in a transverse direction which is perpendicular to the transverse direction of the first layer. An alternate embodiment includes a third layer.
    Type: Grant
    Filed: September 3, 2009
    Date of Patent: March 25, 2014
    Assignees: National Institute of Aerospace Associates, The United States of America as represented by the Administration of NASA
    Inventors: Tian-Bing Xu, Xiaoning Jiang, Ji Su
  • Patent number: 8671551
    Abstract: A process and apparatus for collecting data for nondestructive evaluation of the quality of a crimped wire connector are provided. The process involves providing a crimping tool having an anvil and opposing jaw for crimping a terminal onto a stranded wire, moving the jaw relative to the anvil to close the distance between the jaw and the anvil and thereby compress the terminal against the wire, while transmitting ultrasonic waves that are propagated through the terminal-wire combination and received at a receiving ultrasonic transducer as the jaw is moved relative to the anvil, and detecting and recording the position of the jaw relative to the anvil as a function of time and detecting and recording the amplitude of the ultrasonic wave that is received at the receiving ultrasonic transducer as a function of time as the jaw is moved relative to the anvil.
    Type: Grant
    Filed: February 1, 2012
    Date of Patent: March 18, 2014
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: William T. Yost, Karl E. Cramer, Daniel F. Perey, Keith A. Williams
  • Patent number: 8673649
    Abstract: A wireless chemical sensor includes an electrical conductor and a material separated therefrom by an electric insulator. The electrical conductor is an unconnected open-circuit shaped for storage of an electric field and a magnetic field. In the presence of a time-varying magnetic field, the first electrical conductor resonates to generate harmonic electric and magnetic field responses. The material is positioned at a location lying within at least one of the electric and magnetic field responses so-generated. The material changes in electrical conductivity in the presence of a chemical-of-interest.
    Type: Grant
    Filed: May 11, 2009
    Date of Patent: March 18, 2014
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Stanley E. Woodard, Donald M. Oglesby, Bryant Douglas Taylor
  • Patent number: 8671763
    Abstract: A windscreen is configured for measuring outdoor infrasonic sound. The windscreen includes a container and a microphone. The container defines a chamber. The microphone is disposed in the chamber and can be operatively supported by the floor. The microphone is configured for detecting infrasonic sound. The container is advantageously formed from material that exhibits an acoustic impedance of between 0 and approximately 3150 times the acoustic impedance of air. A reflector plate may be disposed in the container. The reflector plate operatively can support the microphone and provides a doubling effect of infrasonic pressure at the microphone.
    Type: Grant
    Filed: August 5, 2010
    Date of Patent: March 18, 2014
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Allan J. Zuckerwar, Qamar A. Shams
  • Patent number: 8675922
    Abstract: A method of measuring motion blur is disclosed comprising obtaining a moving edge temporal profile r1(k) of an image of a high-contrast moving edge, calculating the masked local contrast m1(k) for r1(k) and the masked local contrast m2(k) for an ideal step edge waveform r2(k) with the same amplitude as r1(k), and calculating the measure or motion blur ? as a difference function, ?=S(?x?k|m1(k)?m2(k)|?)1/?. The masked local contrasts are calculated using a set of convolution kernels scaled to simulate the performance of the human visual system, and ? is measured in units of just-noticeable differences.
    Type: Grant
    Filed: April 11, 2012
    Date of Patent: March 18, 2014
    Assignee: The United States of America as Represented by the Administrator of the National Aeronautics & Space Administration (NASA)
    Inventors: Andrew B. Watson, Albert J. Ahumada
  • Patent number: 8673120
    Abstract: A process for producing boron nitride nanotubes and/or boron-carbon-nitrogen nanotubes of the general formula BxCyNz. The process utilizes a combination of laser light and nitrogen gas flow to support a boron ball target during heating of the boron ball target and production of a boron vapor plume which reacts with nitrogen or nitrogen and carbon to produce boron nitride nanotubes and/or boron-carbon-nitrogen nanotubes of the general formula BxCyNz.
    Type: Grant
    Filed: September 22, 2011
    Date of Patent: March 18, 2014
    Assignees: Jefferson Science Associates, LLC, The United States of America, as Represented by the Administrator of NASA
    Inventors: R. Roy Whitney, Kevin Jordan, Michael W. Smith
  • Patent number: 8674302
    Abstract: Methods for forming sensors using transition edge sensors (TES) and sensors therefrom are described. The method includes forming a plurality of sensor arrays includes at least one TES device. The TES device includes a TES device body, a first superconducting lead contacting a first portion of the TES device body, and a second superconducting lead contacting of a second portion of the TES device body, where the first and second superconducting leads separated on the TES device body by a lead spacing. The lead spacing can be selected to be different for at least two of the plurality of sensor arrays. The method also includes determining a transition temperature for each of the plurality of sensor arrays and generating a signal responsive to detecting a change in the electrical characteristics of one of the plurality of sensor arrays meeting a transition temperature criterion.
    Type: Grant
    Filed: May 28, 2010
    Date of Patent: March 18, 2014
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics Space Administration
    Inventor: John E. Sadleir
  • Patent number: 8672107
    Abstract: A vibration damper includes a rigid base with a mass coupled thereto for linear movement thereon. Springs coupled to the mass compress in response to the linear movement along either of two opposing directions. A converter coupled to the mass converts the linear movement to a corresponding rotational movement. A rotary damper coupled to the converter damps the rotational movement.
    Type: Grant
    Filed: March 8, 2011
    Date of Patent: March 18, 2014
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Thomas G. Ivanco
  • Patent number: 8676382
    Abstract: A robotic system includes a robotic mechanism responsive to velocity control signals, and a permissible workspace defined by a convex-polygon boundary. A host machine determines a position of a reference point on the mechanism with respect to the boundary, and includes an algorithm for enforcing the boundary by automatically shaping the velocity control signals as a function of the position, thereby providing smooth and unperturbed operation of the mechanism along the edges and corners of the boundary. The algorithm is suited for application with higher speeds and/or external forces. A host machine includes an algorithm for enforcing the boundary by shaping the velocity control signals as a function of the reference point position, and a hardware module for executing the algorithm. A method for enforcing the convex-polygon boundary is also provided that shapes a velocity control signal via a host machine as a function of the reference point position.
    Type: Grant
    Filed: May 26, 2010
    Date of Patent: March 18, 2014
    Assignees: GM Global Technology Operations LLC, The United States of America as Represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Muhammad E. Abdallah, Brian Hargrave, Robert J. Platt, Jr.
  • Publication number: 20140071909
    Abstract: Uplink sounding comprising sending one or more representations of a sounding request or a sounding request and configuration information indicator of uplink sounding in a wireless radio communication system is disclosed.
    Type: Application
    Filed: October 29, 2010
    Publication date: March 13, 2014
    Applicant: Huawei Administration Building
    Inventors: Mattias Frenne, Anahid Robert Safavi, Jianghua Liu
  • Patent number: 8669096
    Abstract: Systems and methods for isolating samples are provided. The system comprises a first membrane and a second membrane disposed within an enclosure. First and second reservoirs can also be disposed within the enclosure and adapted to contain one or more reagents therein. A first valve can be disposed within the enclosure and in fluid communication with the first reservoir, the second reservoir, or both. The first valve can also be in fluid communication with the first or second membranes or both. The first valve can be adapted to selectively regulate the flow of the reagents from the first reservoir, through at least one of the first and second membranes, and into the second reservoir.
    Type: Grant
    Filed: May 1, 2012
    Date of Patent: March 11, 2014
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Ye Zhang, Honglu Wu
  • Patent number: 8668168
    Abstract: The present invention is a space vehicle valve system which controls the internal pressure of a space vehicle and the flow rate of purged gases at a given internal pressure and aperture site. A plurality of quasi-unique variable dimension peaked valve structures cover the purge apertures on a space vehicle. Interchangeable sheet guards configured to cover valve apertures on the peaked valve structure contain a pressure-activated surface on the inner surface. Sheet guards move outwardly from the peaked valve structure when in structural contact with a purge gas stream flowing through the apertures on the space vehicle. Changing the properties of the sheet guards changes the response of the sheet guards at a given internal pressure, providing control of the flow rate at a given aperture site.
    Type: Grant
    Filed: December 15, 2011
    Date of Patent: March 11, 2014
    Assignee: The United States of America as Represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Anthony R. Kelley, Jeffrey L. Lindner
  • Patent number: 8668613
    Abstract: A two-speed transmission having an input shaft and an output shaft, the transmission being capable of transitioning between fixed ratios, the high-range ratio being direct 1:1 and the low-range ratio being about 2:1. The transmission is a simple lightweight, yet robust, configuration utilizing only two gear meshes, being comprised of an input gear, a cluster gear, and an output gear. The transmission is controlled with a clutch and a sprag and with the input and output shafts turning in the same direction.
    Type: Grant
    Filed: January 10, 2012
    Date of Patent: March 11, 2014
    Assignee: The United States of America as Represented by the Administrator of National Aeronautics and Space Administration
    Inventors: Mark A Stevens, Robert F Handschuh, David G Lewicki