Patents Assigned to USA as represented by the Administrator of the National Aeronautics and Space Administration
  • 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
  • Publication number: 20050119390
    Abstract: Self-metallizing polyimide films are created by doping polyamic acid solutions with metallic ions and solubilizing agents. Upon creating a film, the film is exposed to ultraviolet light for a specific time and then cured. The resulting film has been found to have a metallic surface layer and a metallic subsurface layer (interlayer). The layer separating the metallic layer has a uniform dispersion of small metal particulates within the polymer. The layer below the interlayer has larger metal particulates uniformly distributed within the polymer.
    Type: Application
    Filed: September 23, 2004
    Publication date: June 2, 2005
    Applicant: USA as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Gregory Gaddy, Diane Stoakley, Gilda Miner, Edward Locke, Catharine Fay, German Mills
  • Publication number: 20050017711
    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: April 30, 2004
    Publication date: January 27, 2005
    Applicant: USA as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Stanley Woodard, Bryant Taylor
  • Publication number: 20040156050
    Abstract: An optical path switch divides sample path radiation into a time series of alternating first polarized components and second polarized components. The first polarized components are transmitted along a first optical path and the second polarized components along a second optical path. A first gasless optical filter train filters the first polarized components to isolate at least a first wavelength band thereby generating first filtered radiation. A second gasless optical filter train filters the second polarized components to isolate at least a second wavelength band thereby generating second filtered radiation. A beam combiner combines the first and second filtered radiation to form a combined beam of radiation. A detector is disposed to monitor magnitude of at least a portion of the combined beam alternately at the first wavelength band and the second wavelength band as an indication of the concentration of the substance in the sample path.
    Type: Application
    Filed: June 19, 2003
    Publication date: August 12, 2004
    Applicant: USA as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Glen W. Sachse
  • Publication number: 20040040132
    Abstract: A method for fabricating a piezoelectric macro-fiber composite actuator comprises making a piezoelectric fiber sheet by providing a plurality of wafers of piezoelectric material, bonding the wafers together with an adhesive material to form a stack of alternating layers of piezoelectric material and adhesive material, and cutting through the stack in a direction substantially parallel to the thickness of the stack and across the alternating layers of piezoelectric material and adhesive material to provide at least one piezoelectric fiber sheet having two sides comprising a plurality of piezoelectric fibers in juxtaposition to the adhesive material. The method further comprises bonding two electrically conductive films to the two sides of the piezoelectric fiber sheet. At least one conductive film has first and second conductive patterns formed thereon which are electrically isolated from one another and in electrical contact with the piezoelectric fiber sheet.
    Type: Application
    Filed: September 3, 2003
    Publication date: March 4, 2004
    Applicant: USA as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: W. Keats Wilkie, Robert G. Bryant, Robert L. Fox, Richard F. Hellbaum, James W. High, Antony Jalink, Bruce D. Little, Paul H. Mirick
  • Publication number: 20030173874
    Abstract: An electro-active transducer for sonic applications includes a ferroelectric material sandwiched by first and second electrode patterns to form a piezo-diaphragm coupled to a mounting frame. When the device is used as a sonic actuator, the first and second electrode patterns are configured to introduce an electric field into the ferroelectric material when voltage is applied to the electrode patterns. When the device is used as a sonic sensor, the first and second electrode patterns are configured to introduce an electric field into the ferroelectric material when the ferroelectric material experiences deflection in a direction substantially perpendicular thereto.
    Type: Application
    Filed: March 12, 2003
    Publication date: September 18, 2003
    Applicant: USA as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Robert G. Bryant, Robert L. Fox