Patents Assigned to Administration
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Patent number: 10192970Abstract: A simultaneous ohmic contact to silicon carbide includes a mixture of platinum, titanium, and silicon compounds deposited on a silicon carbide substrate. The silicon carbide substrate includes an n-type surface and a p-type surface.Type: GrantFiled: August 11, 2014Date of Patent: January 29, 2019Assignee: The United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventor: Robert S. Okojie
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Patent number: 10193228Abstract: An antenna includes a first electrical conductor that is shaped to form a spiral between its first and second ends that remain electrically unconnected such that the first electrical conductor so-shaped is maintained as an unconnected single-component open-circuit having inductance and capacitance. In the presence of a time-varying electromagnetic field, the first electrical conductor so-shaped resonates to generate a harmonic electromagnetic field response having a frequency, amplitude and bandwidth. A second electrical conductor includes a loop portion overlapping at least a portion of the spiral. The second electrical conductor is electrically isolated from the first electrical conductor. A radio frequency transceiver capable of transmitting and receiving electromagnetic energy is electrically coupled to the second electrical conductor.Type: GrantFiled: October 22, 2014Date of Patent: January 29, 2019Assignee: The United States of America as represented by the Administrator of NASAInventors: Kenneth L. Dudley, George N. Szatkowski, Chuantong Wang, Laura J. Smith, Larry A. Ticatch, Sandra V. Koppen, Truong X. Nguyen, Jay J. Ely
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Patent number: 10184405Abstract: A process for mitigating or proactively avoiding an aircraft engine icing event may include detecting ice crystals in the atmosphere using one or more sensors on board an aircraft in real time. The process may also include modulating one or more engine operating conditions to proactively change an ice accretion location, to avoid the occurrence of an icing event. The process may further include implementing one or more modulated engine operating conditions in engine controls software, hardware, or both.Type: GrantFiled: March 30, 2017Date of Patent: January 22, 2019Assignee: The United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventors: Joseph P. Veres, Philip C. Jorgenson
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Patent number: 10184839Abstract: The present invention relates to uncooled microbolometers which can be integrated in future thermal instruments engaged in land imaging on future observatories. The present invention includes: (1) developing and characterizing a microstructured VOx thin film, and, (2) fabricating an uncooled microbolometer array over the 8-14 micron spectral band.Type: GrantFiled: August 30, 2017Date of Patent: January 22, 2019Assignee: The United States of America as represented by the Administrator of NASAInventors: Ari D. Brown, Emily M. Barrentine, Shahid Aslam
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Patent number: 10184777Abstract: A system and method for determining a change in a thickness and temperature of a surface of a material are disclosed herein. The system and the method are usable in a thermal protection system of a space vehicle, such as an aeroshell of a space vehicle. The system and method may incorporate micro electric sensors arranged in a ladder network and capacitor strip sensors. Corrosion or ablation causes a change in an electrical property of the sensors. An amount of or rate of the corrosion or the ablation and a temperature of the material is determined based on the change of the electrical property of the sensors.Type: GrantFiled: August 22, 2017Date of Patent: January 22, 2019Assignee: The United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventor: Robert S. Okojie
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Patent number: 10180699Abstract: An apparatus, method, and system for controlling motion in six degrees of freedom is described. The apparatus includes a support structure, a first pedal and a second pedal. A first set of three independent articulating mechanisms is operatively connected to the support structure and the first pedal. The first set of three independent articulating mechanisms, in combination, enable motion of the first pedal in three control axes corresponding to three discrete degrees of freedom. A second set of three independent articulating mechanisms, operatively connected to the second pedal, enable motion, in combination, in three control axes corresponding to a discrete second set of three degrees of freedom. The apparatus may also include first and second sensors configured to detect the motion of the first and second pedals.Type: GrantFiled: July 30, 2014Date of Patent: January 15, 2019Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Stanley G. Love, Lee M. Morin, Mary E. McCabe
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Patent number: 10175273Abstract: A high-voltage power transmission system is used as an extremely large antenna to extract spatiotemporal space, physical, and geological information from geomagnetically induced currents (GIC). A differential magnetometer method is used to measure GIC and involves acquiring line measurements from a first fluxgate magnetometer under a high-voltage transmission line, acquiring natural field measurements from a reference magnetometer nearby but not under the transmission line, subtracting the natural field measurements from the line measurements, and determining the GIC-related Biot-Savart field from the difference. NASA warning and alarm systems can be triggered based on determinations of GIC amplitude levels that exceed a set threshold value.Type: GrantFiled: September 16, 2015Date of Patent: January 8, 2019Assignee: The United States of America as represented by the Administrator of NASAInventors: Antti A. Pulkkinen, Todd M. Bonalsky, Troy Ames, Carl F. Hostetter
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Patent number: 10174198Abstract: Materials based on low melt polyimide, polyurea, or polyurethane chemistry have been developed which exhibit self-healing properties. These high performance polymers can be utilized either by themselves or in combination with microcapsule technology to deliver self-healing properties to electrical wire insulation or in other high performance, thin wall technologies such as inflatable structures.Type: GrantFiled: June 14, 2012Date of Patent: January 8, 2019Assignee: The United States of America as Represented by the Administrator of NASAInventors: Scott T. Jolley, Martha K. Williams, Tracy L. Gibson, Trent M. Smith, Anne J. Caraccio, Wenyan Li
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Patent number: 10166279Abstract: A mutant of an E coli heat-stable toxin (ST) having the following wild-type sequence: NSSNYCCELCCNPACTGCY wherein the mutant comprises a mutation selected from the group consisting of: A14H, A14T and N12T.Type: GrantFiled: February 20, 2014Date of Patent: January 1, 2019Assignees: Bergen Teknologioverføring, The Administrators of the Tulane Educational FundInventors: Pål Puntervoll, Halvor Sommerfelt, John Clements, James P. Nataro, Weiping Zhang, Arne M. Taxt
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Patent number: 10169847Abstract: An air-to-air background-oriented Schlieren system and method for measuring and rendering visible density changes in air that cause a refractive index change by an airborne vehicle. A sensor aircraft equipped with a high-speed visible spectrum camera travels at low airspeed on a predetermined route and on a level altitude over a background having consistent contrast and sunlight reflectivity. The target aircraft, traveling on the same predetermined route but at an altitude between the sensor aircraft and the ground (background) passes beneath the sensor aircraft. The camera on the sensor aircraft captures a series of images including a reference image immediately before the target aircraft enters the image frame followed by several data images as the target aircraft passes through the image frame. The data images are processed to calculate density gradients around the target aircraft. These density gradients include shockwaves, vortices, engine exhaust, and wakes.Type: GrantFiled: August 5, 2016Date of Patent: January 1, 2019Assignee: The United States of America as Represented by the Administrator of NASAInventors: James Thomas Heineck, Daniel William Banks, Edward Treanor Schairer, Paul Stewart Bean, Edward Andrew Haering, Jr., Brett Arnold Pauer, Brittany Joan Martin, David Nils Larson
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Publication number: 20180362363Abstract: An integrated apparatus for chemical precipitation and rapid filtration of water samples. The invention relates to an apparatus for chemical precipitation and filtration of water samples. The integrated apparatus includes a reaction vessel, a lid of reaction vessel, a opening for reagent addition and gas leakage, an aerating tube, a support, a liquid phase remover, a solid phase collector, a control cover of the liquid phase remover, and a control cover of the solid phase collector.Type: ApplicationFiled: April 1, 2016Publication date: December 20, 2018Applicant: Third Institute of Oceanography, State Oceanic AdministrationInventors: Jianhua He, Yiliang Li, Dekun Huang, Feng Lin, Wu Men, Wen Yu, Fangfang Deng, Jing Lin, Fenfen Wang, Jialin Ni, Tao Yu
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Patent number: 10158335Abstract: A Gated CDS Integrator (GCI) may amplify low-level signals without introducing excessive offset and noise. The GCI may also amplify the low level signals with accurate and variable gain. The GCI may include a modulator preceding an amplifier such that offset or noise present in a signal path between the modulator and a demodulator input is translated to a higher out of band frequency, and thereafter reduced by a double sampled discrete time integrator which also reduces thermal noise. The thermal noise may also be reduced by averaging the output of the discrete time integrator.Type: GrantFiled: September 27, 2016Date of Patent: December 18, 2018Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Gerard T. Quilligan, Shahid Aslam
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Publication number: 20180344905Abstract: The disclosure provides drug delivery devices and methods of making and using the drug delivery devices. The devices include single and multi-layer polymer films made by a breath figure technique having therapeutic agents associated therewith. For example, the devices may be a dual layer polymer film wherein the first layer includes a therapeutic agent incorporated into it by spin coating the first agent with a polymer solution and the second agent is incorporated into the second layer by loading the agent into pores of the second layer after it is spin coated onto the first layer. In some cases one layer provides a burst release and the second layer provides a slow release drug delivery profile. The devices may take on the form of a surgical mesh with a slow release therapeutic drug.Type: ApplicationFiled: August 11, 2018Publication date: December 6, 2018Applicant: The Administrators of the Tulane Educational FundInventors: Diane A. BLAKE, Vijay T. John, Ramesh Ayyala, Thiruselvam Ponnusamy
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Patent number: 10147863Abstract: Systems, methods, and devices of the various embodiments provide pyroelectric sandwich thermal energy harvesters. In the various embodiment pyroelectric sandwich thermal energy harvesters, generated electrical energy may be stored in a super-capacitor/battery as soon as it is generated. The various embodiment pyroelectric sandwich thermal energy harvesters may harvest electrical energy from any environment where temperature variations occur. The various embodiment pyroelectric sandwich thermal energy harvesters may be power sources for space equipment and vehicles in space and/or on earth, as well as the for wireless sensor networks, such as health monitoring systems of oil pipes, aircraft, bridges, and buildings.Type: GrantFiled: October 9, 2015Date of Patent: December 4, 2018Assignee: The United States of America as represented by the Administrator of NASAInventors: Tian-Bing Xu, Jin Ho Kang, Emilie J. Siochi, Glen C. King
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Patent number: 10145602Abstract: An active gas-gap heat switch may significantly reduce the time required to transition between the open and closed states, reduce the heat require to warm the getter, and reduce the heat that leaks from the getter to the switch body. A thermal interface at one end of the active gas-gap heat switch may include a plurality of fins. A getter assembly may be hermetically attached to the thermal interface and a containment tube may surround and house the plurality of fins.Type: GrantFiled: September 2, 2015Date of Patent: December 4, 2018Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Peter J. Shirron, Mark O. Kimball
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Patent number: 10148352Abstract: An apparatus for measuring a distance between a first and second terminal includes a frame counter for determining a number of data frames traversing a distance between the first terminal 105 and the second terminal, a frame bit counter for determining a number of data clock bits offset between a transmitted data frame and a concurrently received data frame, a data clock phase detector for determining a phase difference between an RF data clock for the transmitted data frame and an RF data clock for the concurrently received data frame, and an optical carrier phase detector for determining a phase difference between an optical carrier used to transmit the transmitted data frame and an optical carrier for the concurrently received data frame. The distance between the first and second terminal is determined from a round trip transit time T between the first and second terminals.Type: GrantFiled: July 11, 2017Date of Patent: December 4, 2018Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Guangning Yang, Jeffrey R. Chen
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Patent number: 10144535Abstract: The disclosed subject matter relates to a radiation shielding apparatus including a cryogenic vessel and a cryogenic hydrogen radiation shielding material capable of providing a radiation shield, the cryogenic hydrogen radiation shielding material including cryogenic hydrogen.Type: GrantFiled: September 16, 2015Date of Patent: December 4, 2018Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Xiaoyi Li, Shouvanik Mustafi, Alvin J. Boutte
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Patent number: 10147992Abstract: A via-less crossover for use in broadband microwave/mm-wave circuitry, including: a dielectric substrate; a top layer disposed on one side of the substrate and including a microstrip line with an input and an output, two tapered sections placed around the microstrip line along a co-planar waveguide (CPW) central line, one microstrip portion having an input and which connects to one top layer, rectangular stub disposed adjacent to one of the tapered sections, and another microstrip portion having an output and which connects to another top layer, rectangular stub disposed adjacent to the other of the tapered sections; and a ground layer disposed on an opposite side of the substrate and including a bottom layer CPW central line situated in a central cutout and which connects between a bottom layer, rectangular stub on one side and a bottom layer, rectangular stub on the other side situated in ground cutouts, respectively.Type: GrantFiled: June 28, 2016Date of Patent: December 4, 2018Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Kongpop U-Yen, Edward J. Wollack, Marc Castro
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Patent number: 10138005Abstract: Methods and systems may provide for a structure having a plurality of interconnected panels, wherein each panel has a plurality of detection layers separated from one another by one or more non-detection layers. The plurality of detection layers may form a grid of conductive traces. Additionally, a monitor may be coupled to each grid of conductive traces, wherein the monitor is configured to detect damage to the plurality of interconnected panels in response to an electrical property change with respect to one or more of the conductive traces. In one example, the structure is part of an inflatable space platform such as a spacecraft or habitat.Type: GrantFiled: December 29, 2015Date of Patent: November 27, 2018Assignee: The United States of America as Represented by the Administrator of NASAInventors: Tracy L. Gibson, Martha K. Williams, Mark E. Lewis, Luke B. Roberson, Pedro J. Medelius
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Patent number: 10141705Abstract: A diode pumped, solid state laser is provided that can produce over 16 billion, 15 mJ, 10 ns Q-Switched laser pulses with a low measured decay rate. The laser can be integrated into a global biomass measuring instrument, and mounted on the International Space Station (ISS).Type: GrantFiled: January 27, 2016Date of Patent: November 27, 2018Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Paul R. Stysley, Donald B. Coyle