Patents Assigned to USA as represented by the Administrator of the National Aeronautics and space
  • Publication number: 20090022977
    Abstract: A dielectric material includes a network of nanosubstrates, such as but not limited to nanotubes, nanosheets, or other nanomaterials or nanostructures, a polymer base material or matrix, and nanoparticles constructed at least partially of an elemental metal. The network has a predetermined nanosubstrate loading percentage by weight with respect to a total weight of the dielectric material, and a preferential or predetermined longitudinal alignment with respect to an orientation of an incident electrical field. A method of forming the dielectric material includes depositing the metal-based nanoparticles onto the nanosubstrates and subsequently mixing these with a polymer matrix. Once mixed, alignment can be achieved by melt extrusion or a similar mechanical shearing process. Alignment of the nanosubstrate may be in horizontal or vertical direction with respect to the orientation of an incident electrical field.
    Type: Application
    Filed: July 16, 2008
    Publication date: January 22, 2009
    Applicant: USA as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Kenneth L. Dudley, Holly A. Elliott, John W. Connell, Joseph G. Smith, Sayata Ghose, Kent A. Watson, Donavon Mark Delozier
  • Publication number: 20080319690
    Abstract: The present invention relates to a method of measuring the temperature of the P-N junction within the light-emitting region of a quasi-continuous-wave or pulsed semiconductor laser diode device. A series of relatively short and low current monitor pulses are applied to the laser diode in the period between the main drive current pulses necessary to cause the semiconductor to lase. At the sufficiently low current level of the monitor pulses, the laser diode device does not lase and behaves similar to an electronic diode. The voltage across the laser diode resulting from each of these low current monitor pulses is measured with a high degree of precision. The junction temperature is then determined from the measured junction voltage using their known linear relationship.
    Type: Application
    Filed: May 9, 2008
    Publication date: December 25, 2008
    Applicant: USA as represented by the Administrator of the National Aeronautics & Space Administration
    Inventors: Byron L. Meadows, Frazin Amzajerdian, Bruce W. Barnes, Nathaniel R. Baker
  • Publication number: 20080292392
    Abstract: A flexure based linear bearing includes top and bottom parallel rigid plates; first and second flexures connecting the top and bottom plates and constraining exactly four degrees of freedom of relative motion of the plates, the four degrees of freedom being X and Y axis translation and rotation about the X and Y axes; and a strut connecting the top and bottom plates and further constraining exactly one degree of freedom of the plates, the one degree of freedom being one of Z axis translation and rotation about the Z axis.
    Type: Application
    Filed: September 25, 2007
    Publication date: November 27, 2008
    Applicant: USA as represented by the Administrator of the National Aeronautics and Space Administrator
    Inventor: George M. Voellmer
  • Publication number: 20080265099
    Abstract: An annular fairing having aerodynamic, thermal, structural and acoustic attributes couples a launch abort motor to a space vehicle having a payload of concern mounted on top of a rocket propulsion system. A first end of the annular fairing is fixedly attached to the launch abort motor while a second end of the annular fairing is attached in a releasable fashion to an aft region of the payload. The annular fairing increases in diameter between its first and second ends.
    Type: Application
    Filed: November 16, 2007
    Publication date: October 30, 2008
    Applicant: USA as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Charles J. Camarda, Stephen J. Scotti, Pieter G. Buning, Steven X. S. Bauer, Walter C. Engelund, David M. Schuster
  • Publication number: 20080184795
    Abstract: A wireless sensing system monitors the level, temperature, magnetic permeability and electrical dielectric constant of a non-gaseous material in a container. An open-circuit electrical conductor is shaped to form a two-dimensional geometric pattern that can store and transfer electrical and magnetic energy. The conductor resonates in the presence of a time-varying magnetic field to generate a harmonic response. The conductor is mounted in an environmentally-sealed housing. A magnetic field response recorder wirelessly transmits the time-varying magnetic field to power the conductor, and wirelessly detects the harmonic response that is an indication of at least one of level of the material in the container, temperature of the material in the container, magnetic permeability of the material in the container, and dielectric constant of the material in the container.
    Type: Application
    Filed: January 17, 2008
    Publication date: August 7, 2008
    Applicant: USA as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Stanley E. Woodard
  • Publication number: 20080061274
    Abstract: The invention provides polymer blends containing polyhydroxyamide and one or more flammable polymers. The polymer blends are flame retardant and have improved durability and heat stability compared to the flammable polymer portion of the blends. Articles containing the polymer blends are also provided.
    Type: Application
    Filed: November 5, 2007
    Publication date: March 13, 2008
    Applicant: USA as Represented by the Administrator of the National Aeronautics and space Adm
    Inventors: Martha Williams, Trent Smith
  • Publication number: 20080046390
    Abstract: Systems, methods and apparatus are provided through which in some embodiments an autonomic unit transmits an otoacoustic signal to counteract a potentially harmful incoming signal.
    Type: Application
    Filed: August 9, 2007
    Publication date: February 21, 2008
    Applicant: USA as represented by the Administrator of the National Aeronautics and Space Ad
    Inventors: Michael G. Hinchey, Roy Sterritt
  • Publication number: 20080013598
    Abstract: Self-Validating Thermocouple (SVT) Systems capable of detecting sensor probe open circuits, short circuits, and unnoticeable faults such as a probe debonding and probe degradation are useful in the measurement of temperatures. SVT Systems provide such capabilities by incorporating a heating or excitation element into the measuring junction of the thermocouple. By heating the measuring junction and observing the decay time for the detected DC voltage signal, it is possible to indicate whether the thermocouple is bonded or debonded. A change in the thermal transfer function of the thermocouple system causes a change in the rise and decay times of the thermocouple output. Incorporation of the excitation element does not interfere with normal thermocouple operation, thus further allowing traditional validation procedures as well.
    Type: Application
    Filed: July 13, 2007
    Publication date: January 17, 2008
    Applicant: USA as Represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Jose M. Perotti, Carlos T. Mata, Josephine B. Santiago, Peter Vokrot, Carlos E. Zavala, Bradley M. Burns
  • Publication number: 20080003103
    Abstract: To control vortices originating at the tips of a rotor's blades rotating through the air at a revolution frequency f, separation control device(s) are actuated to periodically introduce perturbations into the airflow moving over the blades. The periodic introduction of perturbations is controlled in accordance with a periodic modulating frequency of introduction f0 while the frequency of the perturbations so-introduced is designated as fe. Vortex control is achieved when the periodic modulating frequency of introduction f0 satisfies the relationship nf?f0?fe where n is the number of blades.
    Type: Application
    Filed: September 22, 2005
    Publication date: January 3, 2008
    Applicant: USA as represented by the Administrator of the National Aeronautics & Space Administration
    Inventor: David Greenblatt
  • Publication number: 20070287628
    Abstract: A hydrogenation catalyst including a base material coated with a catalytic metal is made using mechanical milling techniques. The hydrogenation catalysts are used as an excellent catalyst for the dehalogenation of contaminated compounds and the remediation of other industrial compounds. Preferably, the hydrogenation catalyst is a bimetallic particle including zero-valent metal particles coated with a catalytic material. The mechanical milling technique is simpler and cheaper than previously used methods for producing hydrogenation catalysts.
    Type: Application
    Filed: May 17, 2007
    Publication date: December 13, 2007
    Applicant: USA as Represented by the Administrator of the National Aeronautics and Space Adm
    Inventors: Jacqueline W. Quinn, Christian A. Clausen, Cherie L. Geiger, Brian S. Aitken
  • Publication number: 20070262835
    Abstract: A microwave waveguide filter comprises an input waveguide section; an output waveguide section; a plurality of resonator sections disposed between the input and output waveguide sections; and a plurality of coupling sections disposed on either side of each of the resonator sections; wherein the input waveguide section, the resonator sections, and the output waveguide section have at least four fold symmetric quadruple ridge cross-sections and the coupling sections have at least four fold symmetric cross-sections.
    Type: Application
    Filed: May 15, 2007
    Publication date: November 15, 2007
    Applicant: USA as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Felice Vanin, Edward Wollack
  • Publication number: 20070091724
    Abstract: An optical assembly is formed by one or more piezoelectric fiber composite actuators having one or more optical fibers coupled thereto. The optical fiber(s) experiences strain when actuation voltage is applied to the actuator(s). Light passing through the optical fiber(s) is wavelength tuned by adjusting the actuation voltage.
    Type: Application
    Filed: May 23, 2006
    Publication date: April 26, 2007
    Applicant: USA as represented by the Administrator of the National Aeronautics & Space Administration
    Inventors: Sidney Allison, Qamar Shams, Robert Fox, Christopher Fox, Melanie Chattin
  • Publication number: 20070074182
    Abstract: Systems, methods and apparatus are provided through which in some embodiments, an agent-oriented specification modeled with MaCMAS, is analyzed, flaws in the agent-oriented specification modeled with MaCMAS are corrected, and an implementation is derived from the corrected agent-oriented specification. Described herein are systems, method and apparatus that produce fully (mathematically) tractable development of agent-oriented specification(s) modeled with methodology fragment for analyzing complex multiagent systems (MaCMAS) and policies for autonomic systems from requirements through to code generation. The systems, method and apparatus described herein are illustrated through an example showing how user formulated policies can be translated into a formal mode which can then be converted to code. The requirements-based programming systems, method and apparatus described herein may provide faster, higher quality development and maintenance of autonomic systems based on user formulation of policies.
    Type: Application
    Filed: September 29, 2006
    Publication date: March 29, 2007
    Applicant: USA as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Michael Hinchey, Joaquin Pena, Roy Sterritt
  • Publication number: 20070013371
    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: June 2, 2006
    Publication date: January 18, 2007
    Applicant: USA as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Stanley Woodard, Bryant Taylor
  • Publication number: 20060197405
    Abstract: A hybrid electromechanical actuator has two different types of electromechanical elements, one that expands in a transverse direction when electric power is applied thereto and one that contracts in a transverse direction when electric power is applied thereto. The two electromechanical elements are (i) disposed in relation to one another such that the transverse directions thereof are parallel to one another, and (ii) mechanically coupled to one another at least at two opposing edges thereof. Electric power is applied simultaneously to the elements.
    Type: Application
    Filed: March 4, 2005
    Publication date: September 7, 2006
    Applicant: USA as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Ji Su, Tian-Bing Xu
  • Publication number: 20060084752
    Abstract: An electroactive sensing or actuating material comprises a composite made from a polymer with polarizable moieties and an effective amount of carbon nanotubes incorporated in the polymer for a predetermined electomechanical operation of the composite when such composite is affected by an external stimulus. In another embodiment, the composite comprises a third component of micro-sized to nano-sized particles of an electroactive ceramic that is also incorporated in the polymer matrix. The method for making the three-phase composite comprises either incorporating the carbon nanotubes in the polymer matrix before incorporation of the particles of ceramic or mixing the carbon nanotubes and particles of ceramic together in a solution before incorporation in the polymer matrix.
    Type: Application
    Filed: March 3, 2005
    Publication date: April 20, 2006
    Applicant: USA as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Zoubeida Ounaies, Cheol Park, Joycelyn Harrison, Nancy Holloway, Gregory Draughon
  • Publication number: 20060062950
    Abstract: A composite laminate material is supported during the roll press processing thereof by an assembly having: first and second perforated films disposed adjacent to first and second opposing surfaces of a mixture of uncured resin and fibers defining the composite laminate material, a gas permeable encasement surrounding the mixture and the first and second films, a gas impervious envelope sealed about the gas permeable encasement, and first and second rigid plates clamped about the gas impervious envelope.
    Type: Application
    Filed: September 23, 2004
    Publication date: March 23, 2006
    Applicant: USA as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Luke Catella
  • Publication number: 20060057361
    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 9, 2005
    Publication date: March 16, 2006
    Applicant: USA as represented by the Administrator of the National Aeronautics & Space Administration
    Inventors: Zoubeida Ounaies, Cheol Park, Joycelyn Harrison, Nancy Holloway, Gregory Draughon
  • Publication number: 20060025686
    Abstract: A method and apparatus for measuring pressure buildup in a body compartment that encases muscular tissue. The method includes assessing the body compartment configuration and identifying the effect of pulsatile components on at least one compartment dimension. This process is used in preventing tissue necrosis, and in decisions of whether to perform surgery on the body compartment for prevention of Compartment Syndrome. An apparatus is used for measuring excess pressure in the body compartment having components for imparting ultrasonic waves such as a transducer, placing the transducer to impart the ultrasonic waves, capturing the reflected imparted ultrasonic waves, and converting them to electrical signals, a pulsed phase-locked loop device for assessing a body compartment configuration and producing an output signal, and means for mathematically manipulating the output signal to thereby categorize pressure build-up in the body compartment from the mathematical manipulations.
    Type: Application
    Filed: August 2, 2004
    Publication date: February 2, 2006
    Applicant: USA as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Toshiaki Ueno, Alan Hargens, William Yost
  • Publication number: 20050209429
    Abstract: Main chain thermotropic liquid crystal esters, ester-imides, and ester-amides were prepared from AA, BB, and AB type monomeric materials and end-capped with phenylacetylene, phenylmaleimide, or nadimide reactive end-groups. The end-capped liquid crystal oligomers are thermotropic and have, preferably, molecular weights in the range of approximately 1000-15,000 grams per mole. The end-capped liquid crystal oligomers have broad liquid crystalline melting ranges and exhibit high melt stability and very low melt viscosities at accessible temperatures. The end-capped liquid crystal oligomers are stable for up to an hour in the melt phase. They are highly processable by a variety of melt process shape forming and blending techniques. Once processed and shaped, the end-capped liquid crystal oligomers were heated to further polymerize and form liquid crystalline thermosets (LCT). The fully cured products are rubbers above their glass transition temperatures.
    Type: Application
    Filed: April 29, 2005
    Publication date: September 22, 2005
    Applicant: USA as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Theodorus Dingemans, Erik Weiser, Terry St. Clair