Patents Assigned to USA as represented by the Administrator of the National Aeronautics and Space Administration
  • Publication number: 20100217063
    Abstract: PCBs are removed from contaminated media using a treatment system including zero-valent metal particles and an organic hydrogen donating solvent. The treatment system may include a weak acid in order to eliminate the need for a coating of catalytic noble metal on the zero-valent metal particles. If catalyzed zero-valent metal particles are used, the treatment system may include an organic hydrogen donating solvent that is a non-water solvent. The treatment system may be provided as a “paste-like” system that is preferably applied to natural media and ex-situ structures to eliminate PCBs.
    Type: Application
    Filed: May 13, 2009
    Publication date: August 26, 2010
    Applicant: USA as Represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Jacqueline W. Quinn, Christian A. Clausen, Cherie L. Geiger, Kathleen B. Brooks
  • Publication number: 20100190026
    Abstract: A composite material includes a structural material and a shape-memory alloy embedded in the structural material. The shape-memory alloy changes crystallographic phase from austenite to martensite in response to a predefined critical macroscopic average strain of the composite material. In a second embodiment, the composite material includes a plurality of particles of a ferromagnetic shape-memory alloy embedded in the structural material. The ferromagnetic shape-memory alloy changes crystallographic phase from austenite to martensite and changes magnetic phase in response to the predefined critical macroscopic average strain of the composite material.
    Type: Application
    Filed: January 11, 2010
    Publication date: July 29, 2010
    Applicant: USA as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Terryl A. Wallace, Stephen W. Smith, Robert S. Piascik, Michael R. Horne, Peter L. Messick, Joel A. Alexa, Edward H. Glaessgen, Benjamin T. Hailer
  • Publication number: 20100146635
    Abstract: A biologically-inspired system and method is provided for self-adapting behavior of swarm-based exploration missions, whereby individual components, for example, spacecraft, in the system can sacrifice themselves for the greater good of the entire system. The swarm-based system can exhibit emergent self-adapting behavior. Each component can be configured to exhibit self-sacrifice behavior based on Autonomic System Specification Language (ASSL).
    Type: Application
    Filed: September 29, 2009
    Publication date: June 10, 2010
    Applicant: USA as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: MICHAEL G. HINCHEY, EMIL I. VASSEV
  • Publication number: 20100135344
    Abstract: A method is provided for controlling second harmonic efficiency of laser beam interactions. A laser system generates two laser beams (e.g., a laser beam with two polarizations) for incidence on a nonlinear crystal having a preferred direction of propagation. Prior to incidence on the crystal, the beams are optically processed based on the crystal's beam separation characteristics to thereby control a position in the crystal along the preferred direction of propagation at which the beams interact.
    Type: Application
    Filed: December 1, 2009
    Publication date: June 3, 2010
    Applicant: USA as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Norman P. Barnes, Brian M. Walsh, Donald J. Reichle
  • Publication number: 20100122901
    Abstract: A system includes a collimated beam source within a vacuum chamber, a condensable barrier gas, cooling material, a pump, and isolation chambers cooled by the cooling material to condense the barrier gas. Pressure levels of each isolation chamber are substantially greater than in the vacuum chamber. Coaxially-aligned orifices connect a working chamber, the isolation chambers, and the vacuum chamber. The pump evacuates uncondensed barrier gas. The barrier gas blocks entry of atmospheric vapor from the working chamber into the isolation chambers, and undergoes supersonic flow expansion upon entering each isolation chamber. A method includes connecting the isolation chambers to the vacuum chamber, directing vapor to a boundary with the working chamber, and supersonically expanding the vapor as it enters the isolation chambers via the orifices. The vapor condenses in each isolation chamber using the cooling material, and uncondensed vapor is pumped out of the isolation chambers via the pump.
    Type: Application
    Filed: May 22, 2009
    Publication date: May 20, 2010
    Applicant: USA as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Leonard M. Weinstein, Karen M. Taminger
  • Publication number: 20100116079
    Abstract: A bidirectional tendon terminator that has particular application for terminating a tendon that actuates a finger in a robotic arm. The tendon terminator includes a cylindrical member having an internal channel through which a single continuous piece of the tendon extends. The internal channel of the tendon terminator includes a widened portion. A ball is placed in the tendon strands, which causes the tendon to expand, and the ball is positioned within the widened portion of the channel. Pulling on the tendon operates to either open or close the finger of the robotic arm depending on which direction the tendon is pulled. In one specific embodiment, the cylinder includes two cylindrical pieces that are coupled together so that the ball can be positioned within the channel and the cylindrical member has an entire circumference of material.
    Type: Application
    Filed: November 12, 2008
    Publication date: May 13, 2010
    Applicants: GM GLOBAL TECHNOLOGY OPERATIONS, INC., The USA as represented by the Administrator of the National Aeronautics & Space Administration
    Inventors: CHRIS A. IHRKE, DOUGLAS MARTIN LINN, LYNDON BRIDGWATER
  • Publication number: 20100118916
    Abstract: A flexible thin metal film thermal sensing system is provided. A thermally-conductive film made from a thermally-insulating material is doped with thermally-conductive material. At least one layer of electrically-conductive metal is deposited directly onto a surface of the thermally-conductive film. One or more devices are coupled to the layer(s) to measure an electrical characteristic associated therewith as an indication of temperature.
    Type: Application
    Filed: January 15, 2010
    Publication date: May 13, 2010
    Applicant: USA as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Donald L. Thomsen, III
  • Publication number: 20100084618
    Abstract: The present invention is directed to the effective dispersion of carbon nanotubes (CNTs) into polymer matrices. The nanocomposites are prepared using polymer matrices and exhibit a unique combination of properties, most notably, high retention of optical transparency in the visible range (i.e., 400-800 nm), electrical conductivity, and high thermal stability. By appropriate selection of the matrix resin, additional properties such as vacuum ultraviolet radiation resistance, atomic oxygen resistance, high glass transition (Tg) temperatures, and excellent toughness can be attained. The resulting nanocomposites can be used to fabricate or formulate a variety of articles such as coatings on a variety of substrates, films, foams, fibers, threads, adhesives and fiber coated prepreg. The properties of the nanocomposites can be adjusted by selection of the polymer matrix and CNT to fabricate articles that possess high optical transparency and antistatic behavior.
    Type: Application
    Filed: August 25, 2009
    Publication date: April 8, 2010
    Applicant: USA as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: John W. Connell, Joseph G. Smith, JR., Joycelyn S. Harrison, Cheol Park, Kent A. Watson, Zoubeida Ounaies
  • Publication number: 20100078600
    Abstract: The present invention is directed to the effective dispersion of carbon nanotubes (CNTs) into polymer matrices. The nanocomposites are prepared using polymer matrices and exhibit a unique combination of properties, most notably, high retention of optical transparency in the visible range (i.e., 400-800 nm), electrical conductivity, and high thermal stability. By appropriate selection of the matrix resin, additional properties such as vacuum ultraviolet radiation resistance, atomic oxygen resistance, high glass transition (Tg) temperatures, and excellent toughness can be attained. The resulting nanocomposites can be used to fabricate or formulate a variety of articles such as coatings on a variety of substrates, films, foams, fibers, threads, adhesives and fiber coated prepreg. The properties of the nanocomposites can be adjusted by selection of the polymer matrix and CNT to fabricate articles that possess high optical transparency and antistatic behavior.
    Type: Application
    Filed: August 31, 2009
    Publication date: April 1, 2010
    Applicant: USA as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: John W. Connell, Joseph G. Smith, Joycelyn S. Harrison, Cheol Park, Kent A. Watson, Zoubeida Ounaies
  • Publication number: 20100068485
    Abstract: An electroactive material comprises multiple layers of electroactive composite with each layer having unique dielectric, electrical and mechanical properties that define an electromechanical operation thereof when affected by an external stimulus. For example, each layer can be (i) a 2-phase composite made from a polymer with polarizable moieties and an effective amount of carbon nanotubes incorporated in the polymer for a predetermined electomechanical operation, or (ii) a 3-phase composite having the elements of the 2-phase composite and further including a third component of micro-sized to nano-sized particles of an electroactive ceramic incorporated in the polymer matrix.
    Type: Application
    Filed: March 18, 2009
    Publication date: March 18, 2010
    Applicant: USA as represented by the Administrator of the National Aeronautics Space Administration
    Inventors: Zoubeida OUNAIES, Cheol PARK, Joycelyn S. HARRISON, Nancy M. HOLLOWAY, Gregory K. DRAUGHON
  • Publication number: 20100043900
    Abstract: The advanced modified high performance synthetic jet actuator with optimized curvature shape chamber (ASJA-M) is a synthetic jet actuator (SJA) with a lower volume reservoir or chamber. A curved chamber is used, instead of the conventional cylinder chamber, to reduce the dead volume of the jet chamber and increase the efficiency of the synthetic jet actuator. The shape of the curvature corresponds to the maximum displacement (deformation) profile of the electroactive diaphragm. The jet velocity and mass flow rate for the ASJA-M will be several times higher than conventional piezoelectric actuators.
    Type: Application
    Filed: January 16, 2009
    Publication date: February 25, 2010
    Applicant: USA as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Tian-Bing Xu, Ji Su, Xiaoning Jiang
  • Publication number: 20100044069
    Abstract: 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: Application
    Filed: August 19, 2009
    Publication date: February 25, 2010
    Applicant: USA as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Brian K. Stewart
  • Publication number: 20100019153
    Abstract: Acoustic thermography uses a housing configured for thermal, acoustic and infrared radiation shielding. For in-situ applications, the housing has an open side adapted to be sealingly coupled to a surface region of a structure such that an enclosed chamber filled with air is defined. One or more acoustic sources are positioned to direct acoustic waves through the air in the enclosed chamber and towards the surface region. To activate and control each acoustic source, a pulsed signal is applied thereto. An infrared imager focused on the surface region detects a thermal image of the surface region. A data capture device records the thermal image in synchronicity with each pulse of the pulsed signal such that a time series of thermal images is generated. For enhanced sensitivity and/or repeatability, sound and/or vibrations at the surface region can be used in feedback control of the pulsed signal applied to the acoustic sources.
    Type: Application
    Filed: July 23, 2008
    Publication date: January 28, 2010
    Applicant: USA as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Joseph N. Zalameda, William P. Winfree, William T. Yost
  • Publication number: 20100019811
    Abstract: Systems and methods for rapid Byzantine-fault-tolerant self-stabilizing clock synchronization are provided. The systems and methods are based on a protocol comprising a state machine and a set of monitors that execute once every local oscillator tick. The protocol is independent of specific application specific requirements. The faults are assumed to be arbitrary and/or malicious. All timing measures of variables are based on the node's local clock and thus no central clock or externally generated pulse is used. Instances of the protocol are shown to tolerate bursts of transient failures and deterministically converge with a linear convergence time with respect to the synchronization period as predicted.
    Type: Application
    Filed: April 24, 2009
    Publication date: January 28, 2010
    Applicant: USA as represented by the Administrator of the National Aeronautics & Space Administration
    Inventor: Mahyar R. Malekpour
  • Publication number: 20090315546
    Abstract: A magnetic field response sensor comprises an inductor placed at a fixed separation distance from a conductive surface to address the low RF transmissivity of conductive surfaces. The minimum distance for separation is determined by the sensor response. The inductor should be separated from the conductive surface so that the response amplitude exceeds noise level by a recommended 10 dB. An embodiment for closed cavity measurements comprises a capacitor internal to said cavity and an inductor mounted external to the cavity and at a fixed distance from the cavity's wall. An additional embodiment includes a closed cavity configuration wherein multiple sensors and corresponding antenna are positioned inside the cavity, with the antenna and inductors maintained at a fixed distance from the cavity's wall.
    Type: Application
    Filed: July 31, 2009
    Publication date: December 24, 2009
    Applicant: USA as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Stanley E. Woodard, Bryant Douglas Taylor
  • Publication number: 20090311860
    Abstract: A process for applying blocking contacts on an n-type CdZnTe specimen includes cleaning the CdZnTe specimen; etching the CdZnTe specimen; chemically surface treating the CdZnTe specimen; and depositing blocking metal on at least one of a cathode surface and an anode surface of the CdZnTe specimen.
    Type: Application
    Filed: June 12, 2008
    Publication date: December 17, 2009
    Applicant: USA as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Carl M. Stahle, Bradford H. Parker, Sachidananda R. Babu
  • Publication number: 20090303598
    Abstract: A dynamic optical grating device and associated method for modulating light is provided that is capable of controlling the spectral properties and propagation of light without moving mechanical components by the use of a dynamic electric and/or magnetic field. By changing the electric field and/or magnetic field, the index of refraction, the extinction coefficient, the transmittivity, and the reflectivity of the optical grating device may be controlled in order to control the spectral properties of the light reflected or transmitted by the device.
    Type: Application
    Filed: June 8, 2008
    Publication date: December 10, 2009
    Applicant: USA as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Yeonjoon Park, Sang H. Choi, Glen C. King, Sang-Hyon Chu
  • Publication number: 20090287460
    Abstract: The flow-through area of a pressure regulator positioned in a branch of a simulated fluid flow network is generated. A target pressure is defined downstream of the pressure regulator. A projected flow-through area is generated as a non-linear function of (i) target pressure, (ii) flow-through area of the pressure regulator for a current time step and a previous time step, and (iii) pressure at the downstream location for the current time step and previous time step. A simulated flow-through area for the next time step is generated as a sum of (i) flow-through area for the current time step, and (ii) a difference between the projected flow-through area and the flow-through area for the current time step multiplied by a user-defined rate control parameter. These steps are repeated for a sequence of time steps until the pressure at the downstream location is approximately equal to the target pressure.
    Type: Application
    Filed: July 7, 2005
    Publication date: November 19, 2009
    Applicant: USA as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Neal E. Hass, Paul A. Schallhorn
  • Publication number: 20090231677
    Abstract: An optical assembly includes a zone plate and electro-optic material disposed on one side of the zone plate. The electro-optic material's index of refraction is controlled to adjust the optical properties of the optical assembly.
    Type: Application
    Filed: March 13, 2008
    Publication date: September 17, 2009
    Applicant: USA as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Yeonjoon Park, Sang H. Choi, Glen C. King, James R. Elliott
  • Publication number: 20090233001
    Abstract: A carbon nanotube (CNT) attraction material is deposited on a substrate in the gap region between two electrodes on the substrate. An electric potential is applied to the two electrodes. The CNT attraction material is wetted with a solution defined by a carrier liquid having carbon nanotubes (CNTs) suspended therein. A portion of the CNTs align with the electric field and adhere to the CNT attraction material. The carrier liquid and any CNTs not adhered to the CNT attraction material are then removed.
    Type: Application
    Filed: February 13, 2009
    Publication date: September 17, 2009
    Applicant: USA as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Jan M. Smits, Russell A. Wincheski, JoAnne L. Patry, Anthony Neal Watkins, Jeffrey D. Jordan