Patents Assigned to Administration
  • Patent number: 9056900
    Abstract: The present invention provides compositions and methods for treating a coronavirus infection. A method embodiment comprises administering a polypeptide (preferably in a biocompatible pharmaceutical carrier) to a subject suffering from a coronavirus infection. The polypeptide comprises or consists of at least a portion of the fusion initiation region (FIR) of a coronavirus fusion protein. In some embodiments, the polypeptide comprises or consists of a sequence selected from SEQ ID NO: 2, 22, 23, 24, and 25 or an 8 to 40 contiguous amino acid residue portion thereof.
    Type: Grant
    Filed: August 8, 2013
    Date of Patent: June 16, 2015
    Assignees: The Administrators of the Tulane Educational Fund, Autoimmune Technologies, LLC.
    Inventors: Robert F. Garry, Russell B. Wilson
  • Patent number: 9052236
    Abstract: The present invention comprises an approach for calibrating the sensitivity to polarization, optics degradation, spectral and stray light response functions of instruments on orbit. The concept is based on using an accurate ground-based laser system, Ground-to-Space Laser Calibration (GSLC), transmitting laser light to instrument on orbit during nighttime substantially clear-sky conditions. To minimize atmospheric contribution to the calibration uncertainty the calibration cycles should be performed in short time intervals, and all required measurements are designed to be relative. The calibration cycles involve ground operations with laser beam polarization and wavelength changes.
    Type: Grant
    Filed: June 30, 2014
    Date of Patent: June 9, 2015
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Constantine Lukashin, Bruce A. Wielicki
  • Patent number: 9052250
    Abstract: A calibration system and method utilizes acceleration of a mass to generate a force on the mass. An expected value of the force is calculated based on the magnitude and acceleration of the mass. A fixture is utilized to mount the mass to a force balance, and the force balance is calibrated to provide a reading consistent with the expected force determined for a given acceleration. The acceleration can be varied to provide different expected forces, and the force balance can be calibrated for different applied forces. The acceleration may result from linear acceleration of the mass or rotational movement of the mass.
    Type: Grant
    Filed: April 11, 2013
    Date of Patent: June 9, 2015
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Peter A. Parker, Ray D. Rhew, Thomas H. Johnson, Drew Landman
  • Patent number: 9049869
    Abstract: This invention provides a method for improving bread-making properties of bread dough using rice flour as the main material. The invention relates to a dough improving agent for rice flour breads, wherein said agent comprises glutathione and a method for making rice flour breads using the same.
    Type: Grant
    Filed: September 10, 2010
    Date of Patent: June 9, 2015
    Assignee: Incorporated Administrative Agency National Agriculture and Food Research Organization
    Inventor: Hiroyuki Yano
  • Patent number: 9051063
    Abstract: A heat shield for a space vehicle comprises a plurality of phenolic impregnated carbon ablator (PICA) blocks secured to a surface of the space vehicle and arranged in a pattern with gaps therebetween. The heat shield further comprises a plurality of PICA strips disposed in the gaps between the PICA blocks. The PICA strips are mounted edgewise, such that the structural orientation of the PICA strips is substantially perpendicular to the structural orientation of the PICA blocks.
    Type: Grant
    Filed: January 29, 2013
    Date of Patent: June 9, 2015
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Max L. Blosser, Carl C. Poteet, Stan A. Bouslog
  • Publication number: 20150153367
    Abstract: Artificial microvascular network (AMVN) devices are provided and related methods of making and methods of using such devices are provided. The present disclosure generally relates to an AMVN device comprising a substrate including a capillary network configured so as to simulate those actually encountered in the circulation of various humans and animal model systems. In certain aspects, the AMVN devices may be used, e.g., to investigate the effect of storing RBCs under aerobic and anaerobic conditions. However, the use of such AMVN devices is not so limited.
    Type: Application
    Filed: May 22, 2013
    Publication date: June 4, 2015
    Applicants: The Administrators of the Tulane Educational Fund, New Health Sciences, Inc.
    Inventors: Tatsuro Yoshida, Sergey S. Shevkoplyas, Jennie M. Burns
  • Patent number: 9046418
    Abstract: A spectrometer that includes a grating that disperses light via Fresnel diffraction according to wavelength onto a sensing area that coincides with an optical axis plane of the grating. The sensing area detects the dispersed light and measures the light intensity associated with each wavelength of the light. Because the spectrometer utilizes Fresnel diffraction, it can be miniaturized and packaged as an integrated circuit.
    Type: Grant
    Filed: February 25, 2013
    Date of Patent: June 2, 2015
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Sang Hyouk Choi, Yeonjoon Park
  • Patent number: 9046115
    Abstract: An eddy-current-minimizing flow plug has open flow channels formed between the plug's inlet and outlet. Each open flow channel includes (i) a first portion that originates at the inlet face and converges to a location within the plug that is downstream of the inlet, and (ii) a second portion that originates within the plug and diverges to the outlet. The diverging second portion is approximately twice the length of the converging first portion. The plug is devoid of planar surface regions at its inlet and outlet, and in fluid flow planes of the plug that are perpendicular to the given direction of a fluid flowing therethrough.
    Type: Grant
    Filed: November 9, 2012
    Date of Patent: June 2, 2015
    Assignee: The United States of America as Represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: John Dwight England, Anthony R. Kelley
  • Patent number: 9048759
    Abstract: Embodiments of the disclosure include an apparatus and methods for using a piezoelectric device, that includes an outer flextensional casing, a first cell and a last cell serially coupled to each other and coupled to the outer flextensional casing such that each cell having a flextensional cell structure and each cell receives an input force and provides an output force that is amplified based on the input force. The apparatus further includes a piezoelectric stack coupled to each cell such that the piezoelectric stack of each cell provides piezoelectric energy based on the output force for each cell. Further, the last cell receives an input force that is the output force from the first cell and the last cell provides an output apparatus force In addition, the piezoelectric energy harvested is based on the output apparatus force. Moreover, the apparatus provides displacement based on the output apparatus force.
    Type: Grant
    Filed: November 10, 2011
    Date of Patent: June 2, 2015
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Tian-Bing Xu, Emilie J. Siochi, Lei Zuo, Xiaoning Jiang, Jin Ho Kang
  • Patent number: 9044743
    Abstract: This invention relates generally to a platinized tin oxide-based catalyst. It relates particularly to an improved platinized tin oxide-based catalyst able to decompose nitric oxide to nitrogen and oxygen without the necessity of a reducing gas.
    Type: Grant
    Filed: March 18, 2010
    Date of Patent: June 2, 2015
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: David R. Schryer, Jeffrey D. Jordan, Ates Akyurtlu, Jale Akyurtlu
  • Patent number: 9046426
    Abstract: A modular apparatus for attaching sensors and electronics is disclosed. The modular apparatus includes a square recess including a plurality of cavities and a reference cavity such that a pressure sensor can be connected to the modular apparatus. The modular apparatus also includes at least one voltage input hole and at least one voltage output hole operably connected to each of the plurality of cavities such that voltage can be applied to the pressure sensor and received from the pressure sensor.
    Type: Grant
    Filed: June 15, 2012
    Date of Patent: June 2, 2015
    Assignee: The United States of America as Represented by the Administrator of National Aeronautics and Space Administration
    Inventor: Robert S Okojie
  • Patent number: 9041469
    Abstract: One or more embodiments of the present invention pertain to an all solid-state microwave power module. The module includes a plurality of solid-state amplifiers configured to amplify a signal using a low power stage, a medium power stage, and a high power stage. The module also includes a power conditioner configured to activate a voltage sequencer (e.g., bias controller) when power is received from a power source. The voltage sequencer is configured to sequentially apply voltage to a gate of each amplifier and sequentially apply voltage to a drain of each amplifier.
    Type: Grant
    Filed: March 20, 2013
    Date of Patent: May 26, 2015
    Assignee: The United States of America as Represented by the Administrator of National Aeronautics and Space Administration
    Inventors: Rainee N. Simons, Edwin G. Wintucky
  • Publication number: 20150141544
    Abstract: Porous cross-linked polyimide networks are provided. The networks comprise an anhydride end-capped polyamic acid oligomer. The oligomer (i) comprises a repeating unit of a dianhydride and a diamine and terminal anhydride groups, (ii) has an average degree of polymerization of 10 to 50, (iii) has been cross-linked via a cross-linking agent, comprising three or more amine groups, at a balanced stoichiometry of the amine groups to the terminal anhydride groups, and (iv) has been chemically imidized to yield the porous cross-linked polyimide network. Also provided are porous cross-linked polyimide aerogels comprising a cross-linked and imidized anhydride end-capped polyamic acid oligomer, wherein the oligomer comprises a repeating unit of a dianhydride and a diamine, and the aerogel has a density of 0.10 to 0.333 g/cm3 and a Young's modulus of 1.7 to 102 MPa. Also provided are thin films comprising aerogels, and methods of making porous cross-linked polyimide networks.
    Type: Application
    Filed: February 1, 2013
    Publication date: May 21, 2015
    Applicants: U.S. Government as represented by the Administrator of the National Aeronautics and Spac, OHIO AEROSPACE INSTITUTE
    Inventors: OHIO AEROSPACE INSTITUTE, U.S. Government as represented by the Administrator of the National Aeronautics and Spa
  • Patent number: 9032785
    Abstract: A system and method of measuring a residence time in a gas-turbine engine is provided, whereby the method includes placing pressure sensors at a combustor entrance and at a turbine exit of the gas-turbine engine and measuring a combustor pressure at the combustor entrance and a turbine exit pressure at the turbine exit. The method further includes computing cross-spectrum functions between a combustor pressure sensor signal from the measured combustor pressure and a turbine exit pressure sensor signal from the measured turbine exit pressure, applying a linear curve fit to the cross-spectrum functions, and computing a post-combustion residence time from the linear curve fit.
    Type: Grant
    Filed: June 27, 2012
    Date of Patent: May 19, 2015
    Assignee: The United States of America as Represented by the Administrator National Aeronautics and Space Administration
    Inventor: Jeffrey H Miles
  • Patent number: 9032723
    Abstract: A shut off valve is configured to shut off flow from the high pressure fluid line to the high pressure accumulator in a series hydraulic hybrid vehicle in order to quickly raise system pressure in the high pressure fluid line and enable additional torque output from the hydraulic motor for vehicle propulsion. A pressure relief valve is further provided to vent excess flow from the high pressure line to the high pressure accumulator as needed to avoid exceeding a maximum desired system pressure in the high pressure fluid line, thereby providing for safe and efficient hydrostatic operation in the vehicle.
    Type: Grant
    Filed: March 9, 2011
    Date of Patent: May 19, 2015
    Assignee: The United States of America, as represented by the Administrator of the U.S. Environmental Protection Agency
    Inventor: David J Haugen
  • Patent number: 9033525
    Abstract: Methods for maximizing a fraction of light energy absorbed in each of three classes of light concentrators (rectangular parallelepipeds, paraboloids and prisms) by choice of incident angle of radiation and of one or more geometrical or physical parameters (absorber thickness, paraboloid dimensions, location of paraboloid focus, prism angles, concentrator material, cladding, prism angles, etc.). Alternatively, the light energy absorbed plus the light energy that escapes through non-total internal reflection within the light concentrator can be minimized.
    Type: Grant
    Filed: May 16, 2013
    Date of Patent: May 19, 2015
    Assignee: The United States of America as Represented by the Administrator of the National Aeronautics & Space Administration (NASA)
    Inventor: Bin Chen
  • Publication number: 20150134199
    Abstract: A vehicle includes a chassis, a modular component, and a central operating system. The modular component is supported by the chassis. The central operating system includes a component control system, a primary master controller, and a secondary master controller. The component control system is configured for controlling the modular component. The primary and secondary master controllers are in operative communication with the component control system. The primary and secondary master controllers are configured to simultaneously transmit commands to the component control system. The component control system is configured to accept commands from the secondary master controller only when a fault occurs in the primary master controller.
    Type: Application
    Filed: November 8, 2013
    Publication date: May 14, 2015
    Applicants: The U.S.A. as Represented by the Administrator of the National Aeronautics and Space Administration, GM GLOBAL TECHNOLOGY OPERATIONS LLC
    Inventors: Nathan Fraser-Chanpong, Ivan Spain, Andrew D. Dawson, William J. Bluethmann, Chunhao J. Lee, Robert L. Vitale, Raymond Guo, Thomas M. Waligora, Akinjide Akinniyi Akinyode, Ryan M. Reed
  • Publication number: 20150134202
    Abstract: A method of controlling steering of a vehicle through setting wheel angles of a plurality of modular electronic corner assemblies (eModules) is provided. The method includes receiving a driving mode selected from a mode selection menu. A position of a steering input device is determined in a master controller. A velocity of the vehicle is determined, in the master controller, when the determined position of the steering input device is near center. A drive mode request corresponding to the selected driving mode to the plurality of steering controllers is transmitted to the master controller. A required steering angle of each of the plurality of eModules is determined, in the master controller, as a function of the determined position of the steering input device, the determined velocity of the vehicle, and the selected first driving mode. The eModules are set to the respective determined steering angles.
    Type: Application
    Filed: November 8, 2013
    Publication date: May 14, 2015
    Applicants: The U.S.A. As Represented by the Administrator of the National Aeronautics and Space Adminstration, GM GLOBAL TECHNOLOGY OPERATIONS LLC
    Inventors: Andrew D. Dawson, William J. Bluethmann, Chunhao J. Lee, Robert L. Vitale, Raymond Guo, Venkata Prasad Atluri
  • Patent number: 9028723
    Abstract: Copper(II) acetate, zinc(II) acetate, and tin(IV) acetate are weighed so that the total amount of metal ions is 2.0×10?4 mol and the molar ratio of ions is Cu:Zn:Sn=2:1:1, and 2.0 cm3 of oleylamine is added to prepare a mixed solution. Apart from this, 1.0 cm3 of oleylamine is added to 2.0×10?4 mol of sulfur powder to prepare a mixed solution. These mixed solutions are separately heated at 60° C. and mixed at room temperature. The pressure in a test tube is reduced, followed by nitrogen filling. The test tube is heated at 240° C. for 30 minutes and then allowed to stand until room temperature. The resultant product is separated into a supernatant and precipitates by centrifugal separation. The separated supernatant is filtered, methanol is added to produce precipitates. The precipitates are dissolved by adding chloroform to prepare a semiconductor nanoparticle solution.
    Type: Grant
    Filed: February 25, 2010
    Date of Patent: May 12, 2015
    Assignees: National University Corporation Nagoya University, Osaka University, Tokyo University of Science Educational Foundation Administrative Organization
    Inventors: Tsukasa Torimoto, Ken-ichi Okazaki, Tatsuya Kameyama, Takaaki Osaki, Susumu Kuwabata, Akihiko Kudo
  • Patent number: 9027265
    Abstract: An excavator includes a mobile chassis with a first bucket drum and a second bucket drum coupled thereto. The first bucket drum and second bucket drum are coupled to the chassis for positioning thereof on the surface at opposing ends of the chassis. Each first scoop on the first bucket drum is a mirror image of one second scoop on the second bucket drum when (i) the first bucket drum and second bucket drum are on the surface adjacent opposing ends of the chassis, and (ii) the first bucket drum is rotated in one direction and the second bucket drum is simultaneously rotated in an opposing direction.
    Type: Grant
    Filed: May 17, 2013
    Date of Patent: May 12, 2015
    Assignee: The United States of America as Represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Robert P. Mueller, Andrew J. Nick, Jason M. Schuler, Jonathan D. Smith