Patents Assigned to The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
  • Patent number: 11815074
    Abstract: Scalable power processing units (PPUs) for Hall-effect thrusters (HETs) and terrestrial systems are disclosed. A technique for current estimation may be employed on each output of parallel isolated discharge supply modules (DSMs) to force proper current/load sharing between the DSMs. A flyback power supply may be used that performs the dual functions of a cathode keeper plasma ignitor and sustainer. The flyback power supply may be tuned for a high no-load direct current (DC) output voltage to achieve cathode keeper ignition rather than requiring a separate ignitor supply, which reduces circuit complexity. To address requirements for higher voltage DC ignition than are achievable with a flyback power supply alone, a supplemental DC ignitor may be placed in parallel with the flyback power supply of some embodiments. Such simplified PPU architectures may provide a high efficiency, low part count, scalable architecture suitable for more compact and lower cost system designs.
    Type: Grant
    Filed: June 26, 2020
    Date of Patent: November 14, 2023
    Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space Administration
    Inventors: Gabriel F. Benavides, Luis R. Pinero, Corey R. Rhodes, Arthur Birchenough
  • Patent number: 11779869
    Abstract: Methods and systems are provided for a multiplexed phase separating inertial filter that is composed of helical through holes generating centrifugal separating forces. In one example, the inertial filter may be a planar porous material with an array of helical channels, each helical channel of the array of helical channels extending from a top surface of the porous material to a bottom surface of the porous material.
    Type: Grant
    Filed: November 19, 2021
    Date of Patent: October 10, 2023
    Assignees: IRPI LLC, The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Mark M. Weislogel, John C. Graf, Nora D. Shapiro, Logan Torres, Rawand M. Rasheed, Ryan Jenson
  • Patent number: 11658398
    Abstract: A phased-array, conformal antenna and a method for forming same are disclosed. The method comprises forming a substantially planar layered antenna structure by fabricating a printed circuit board (PCB) on a substantially planar first substrate, adhering the PCB to a second substantially planar substrate, the second substantially planar substrate comprising an aerogel, adhering a plurality of antenna elements to the substantially planar second substrate to form the phased-array, adhering a protective layer to the one or more antenna elements, and shaping the substantially planar layered antenna structure to form a substantially curved layered antenna structure.
    Type: Grant
    Filed: August 24, 2020
    Date of Patent: May 23, 2023
    Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space Administration
    Inventors: James M. Downey, Bryan L. Schoenholz, Marie T. Piasecki
  • Patent number: 11588628
    Abstract: A space and wave division multiplexing and demultiplexing system and method for quantum key distribution (QKD) using free space laser communications. The system operates to transmit a quantum channel, including a key of QKD, included in a combined laser transmission with a classical channel, including an encrypted message of QKD. The laser transmission can be transmitted through free space to a lens, wherein it is diffracted into two separate diffraction patterns and captured by a double clad optical receiver fiber having an inner core and a concentric outer core. The diffraction pattern of the classical channel is captured by the outer core, while the diffraction pattern of the quantum channel is captured by the inner core, thus allowing separate treatment of each channel.
    Type: Grant
    Filed: March 31, 2021
    Date of Patent: February 21, 2023
    Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space Administration
    Inventor: Adam C. Wroblewski
  • Patent number: 11532296
    Abstract: Broadband acoustic absorbers may be capable providing good absorption performance between 0 and 3,000 Hz, and particularly below 1,000 Hz. Reeds may be incorporated in a single layer, multiple layers, or bundles. Such broadband acoustic absorbers may be applied for acoustic absorption in aircraft, spacecraft, residential and commercial buildings, vehicles, industrial environments, wind tunnels, or any other suitable environment or application where noise reduction is desired.
    Type: Grant
    Filed: August 28, 2019
    Date of Patent: December 20, 2022
    Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space Administration
    Inventors: Lisa Danielle Koch, Michael G. Jones, Peter J. Bonacuse, Christopher J. Miller, James Christopher Johnston, Maria A. Kuczmarski
  • Patent number: 11517962
    Abstract: A method for making small diameter NiTi metal alloy components, including balls, comprising providing a metal powder comprising nickel, titanium, and a transition metal, consolidating the metal powder into cylindrical rods, and cutting the cylindrical rods into segments. The segments are then machined into spheres slightly larger than the finished ball size diameter. The spheres are heat treated to solutionize and dissolve all phases and subsequently cooled without the need for rapid quenching due to the influence of the transition metal to suppresses the formation of soft phases in the spheres, wherein such soft phases prevent hardening, to achieve a Rockwell hardness of HRC 58-62. Finally, the hardened spheres are polished until the desired finished ball size diameter and surface finish is achieved.
    Type: Grant
    Filed: June 10, 2021
    Date of Patent: December 6, 2022
    Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space Administration
    Inventors: Christopher DellaCorte, Fransua Thomas, Malcolm K. Stanford
  • Patent number: 11505485
    Abstract: A supercritical water oxidation vortex reactor has a reactor shell configured to contain a pressurized and heated material including water, a burner assembly configured to create a supercritical core region in the material in the reactor shell, the supercritical core region including water above its critical point, an injector assembly configured to inject into the enclosed volume a subcritical wash stream including water below its critical point and an aspirator arranged in the enclosed volume and configured to remove a processed flow including purified water from an upper portion of the supercritical core region. The supercritical water oxidation vortex reactor is configured with an upward helical flow to transfer precipitated ionic compounds out of the supercritical core region, through a transcritical intermediate region, and into the subcritical wash stream where they re-dissolve.
    Type: Grant
    Filed: March 3, 2021
    Date of Patent: November 22, 2022
    Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space Administration
    Inventors: Michael C. Hicks, Uday G. Hegde
  • Patent number: 11506620
    Abstract: A double capsule assembly includes an outer capsule and an inner capsule configured to be positioned within the outer capsule. The inner capsule is configured to have a sample positioned therein. The double capsule assembly is configured to be placed in a solid media assembly to analyze or synthesize the sample.
    Type: Grant
    Filed: July 16, 2019
    Date of Patent: November 22, 2022
    Assignee: United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Kevin Righter
  • Patent number: 11473663
    Abstract: A gear includes a steel rim having an inner circumferential surface a composite gear body attached thereto. The composite gear body includes an opening in a central region thereof. A first continuous fiber composite layer extends from a first point on an outer circumferential edge of the composite gear body to a second point on the outer circumferential edge. A second continuous fiber layer extends from the first point to the second point. The composite gear body also includes a filler layer disposed between the first and second continuous fiber layers, the filler layer extending within an inner region of the composite gear body. The inner region extends radially between the opening and a boundary inward of the inner circumferential surface such that the composite gear body is thicker within the inner region.
    Type: Grant
    Filed: February 22, 2019
    Date of Patent: October 18, 2022
    Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space Administration
    Inventors: Gary D. Roberts, Robert F. Handschuh, Kelsen E. LaBerge, Joel P. Johnston, Sandi G. Miller
  • Patent number: 11406867
    Abstract: A portable system for dynamometry, exercise, and rehabilitation comprises a base, a detachable servomotor assembly, an embedded control system, and a physical human-machine interface for securing a human limb into a stabilized position for use in a repeatable and ambidextrous manner. In another embodiment, the portable system includes a power source and a user interface subsystem for selecting operative modes and input parameters and for real-time processing, display, and storage of the values collected by the system during operation. In another embodiment, a method for determining strength of an isolated muscle group of a human joint is disclosed. The method includes the steps of mounting and securing a detachable servomotor assembly of a portable dynamometer upon a surface and securing the human joint to be tested into a stable position with an adjustable, ambidextrous distal limb attachment assembly for use of the portable dynamometer in a readily repeatable manner.
    Type: Grant
    Filed: October 24, 2019
    Date of Patent: August 9, 2022
    Assignee: United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Christopher E. Beck, Eduardo Herrera, Austin Lovan, Jairo Sanchez, Andrew S. Donnan, Roger Rovekamp, Briana Luthman, Edward B. Behan, Richard M. Prince, Arthur J. Lekstutis
  • Patent number: 11339463
    Abstract: A local phase transformation strengthened nickel-base superalloy includes at least 8.0 wt % eta phase formers; at least 7.0 wt % of chi phase formers; less than 12 wt % chromium; at least 18 wt % cobalt; and aluminum. A ratio of eta phase formers:aluminum is (3.2-3.4):1. The eta phase formers can include titanium, tantalum, hafnium, and niobium. The chi phase formers include tungsten and molybdenum. When the superalloy is subjected to elevated temperatures, these levels of components promote eta and chi phase formation along superlattice stacking faults, thereby resulting in a local phase transformation at the stacking faults, which strengthens the superalloy and inhibits creep deformation.
    Type: Grant
    Filed: January 31, 2020
    Date of Patent: May 24, 2022
    Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space Administration
    Inventors: Timothy M. Smith, Robert W. Carter
  • Patent number: 11325869
    Abstract: Slurry EBC systems and method for fabricating slurry EBC systems for protecting component substrates and extending the longevity of such components are disclosed. The slurry EBC systems include a bond coat having a temperature capability of up to 1482° C. (2700° F.). Example bond coats include a mullite-based bond coat and a rare earth disilicate-based bond coat.
    Type: Grant
    Filed: October 22, 2018
    Date of Patent: May 10, 2022
    Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space Administration
    Inventors: Kang N. Lee, Deborah L. Waters
  • Patent number: 11303194
    Abstract: A cryogen-free partially-superconducting electric machine of the wound field synchronous type includes a room temperature semi-slotless stator, a superconducting motor rotor, a gap between the rotor and stator, a torque tube which isolates the cryogenic superconducting motor rotor from a central shaft, bearings, an acoustic cryocooler integrated within the motor rotor and torque tube, a heat exchange, a rotary transformer, a vacuum pump, a vacuum enclosure integrated with the stator, and an eddy current/thermal shield. The electric machine can act as a motor or a generator and produces a high specific power and efficiency.
    Type: Grant
    Filed: July 2, 2019
    Date of Patent: April 12, 2022
    Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space Administration
    Inventors: Ralph H. Jansen, Peter E. Kascak, Rodger W. Dyson
  • Patent number: 11201358
    Abstract: A system for measuring a heat response of a cell during a thermal runaway event includes a housing. An insulation is positioned within the housing. A calorimeter is positioned within the insulation and the housing. The calorimeter is configured to have the cell positioned therein. The calorimeter is configured to measure a temperature increase of the cell, one or more components of the calorimeter, or a combination thereof during the thermal runaway event of the cell. A total energy yield of the thermal runaway event is configured to be determined based at least partially upon the temperature increase. A ratio is configured to be determined based at least partially upon the temperature increase. The ratio includes energy released through a casing of the cell during the thermal runaway event vs. energy released through ejecta material from the cell during the thermal runaway event.
    Type: Grant
    Filed: October 30, 2018
    Date of Patent: December 14, 2021
    Assignee: United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Eric C Dimpault-Darcy, John J. Darst, William Q. Walker, Steven L. Rickman, Natalie N. Anderson, Christiaan Khurana, Bruce L. Drolen, Gary Bayles, Zoran Bilc
  • Patent number: 11192780
    Abstract: A microsensor and its method of manufacture are disclosed based on templated metal or metal oxide nanostructures. The microsensor includes an electrode that in one embodiment may be configured as a first sawtooth patterned electrode having a series of first peaks and first valleys and a second electrode that by be configured as a second sawtooth patterned electrode having a series of second peaks and second valleys where the second peaks generally align with the first peaks of the first electrode. A plurality of templated metal or metal oxide nanostructures connect on one side to the first electrode and on another side to the second electrode, where an electrical property of the microsensor changes in response to exposure to an environment to be monitored.
    Type: Grant
    Filed: March 25, 2019
    Date of Patent: December 7, 2021
    Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space Administration
    Inventors: Azlin M. Biaggi-Labiosa, Gary W. Hunter
  • Patent number: 11195072
    Abstract: A method for streaming sensor data from a set of radio-frequency identification (RFID) tags includes determining an initial communication approach to be performed with respect to each RFID tag. The method also includes managing access to the RFID tag by refining the initial communication approach based on records of successes and failures of the initial communication approach. A radio-frequency identification (RFID) system is also disclosed, the system comprising one or more processors and a memory system comprising one or more non-transitory computer-readable media storing instructions that, when executed by at least one of the one or more processors, causes the system to perform operations for streaming sensor data from one or more RFID tags to one or more RFID readers.
    Type: Grant
    Filed: February 27, 2019
    Date of Patent: December 7, 2021
    Assignee: United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Raymond S Wagner, David S Hafermalz, Patrick W. Fink, Chad Zalkin, Ray Seegmiller
  • Patent number: 11183626
    Abstract: A magnetostrictive alternator configured to convert pressure waves into electrical energy is provided. It should be appreciated that the magnetostrictive alternator may be combined in some embodiments with a Stirling engine to produce electrical power. The Stirling engine creates the oscillating pressure wave and the magnetostrictive alternator converts the pressure wave into electricity. In some embodiments, the magnetostrictive alternator may include aerogel material and magnetostrictive material. The aerogel material may be configured to convert a higher amplitude pressure wave into a lower amplitude pressure wave. The magnetostrictive material may be configured to generate an oscillating magnetic field when the magnetostrictive material is compressed by the lower amplitude pressure wave.
    Type: Grant
    Filed: December 13, 2017
    Date of Patent: November 23, 2021
    Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space Administration
    Inventors: Rodger W. Dyson, Geoffrey A. Bruder
  • Patent number: 11174850
    Abstract: A plurality of shape memory alloy tubes (SMTs) of one or more shape memory alloy (SMA) types is configured as an element in a rotary actuator system in a nested manner. In various configurations, the nested SMTs provide one or more modes of multiplication (torque output or angular displacement), rotation reversibility and bias loading. The innovation provides for leveraging the modes for reductions in the rotary actuator system size, weight, or complexity or combinations thereof, or providing improved and more stable actuation capabilities in a given envelope.
    Type: Grant
    Filed: January 24, 2020
    Date of Patent: November 16, 2021
    Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space Administration
    Inventors: Othmane Benafan, Phillip B. Abel, Steven W. Bauman, Darrell J. Gaydosh, Paul A. Solano
  • Patent number: 11129546
    Abstract: A portable unit for metabolic analysis includes a manifold in fluid communication with a mouth of a test subject. A conduit extends from the manifold and defines a flow channel through which the breaths of the test subject travels. A carbon dioxide sensor is attached to the conduit. The carbon dioxide sensor includes an intermediate support housing enclosing a volume disposed along the flow channel to define a first part of the flow channel, an inner support housing attached to a first side of the intermediate support housing, a plurality of IR LEDs mounted to an interior surface of the inner support housing, an outer support housing attached to a second side of the intermediate support housing, and a photodetector attached to the outer support housing. The photodetector faces the flow channel and receives IR radiation emitted by the plurality of LEDs.
    Type: Grant
    Filed: August 6, 2018
    Date of Patent: September 28, 2021
    Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space Administration
    Inventors: Daniel L. Dietrich, Jeffrey R. Juergens, Mark E. Lewis, Nancy C. Piltch, Michael J. Lichter, Russel W. Valentine, Dale M. Diedrick, Richard D Pettegrew, Peter M. Struk
  • Patent number: 11131294
    Abstract: A scalable plurality of shape memory alloy (SMA) elements are configured to provide a continuous rotation actuator system. The plurality of SMA elements are coupled to a Ring Gear element, as well as to a Sun Gear element and a provision for thermal cycle return assist of the SMA elements. A plurality of Transmission elements provide for controlled rotary actuation in a desired direction with lock capability that provides for continuous rotary motion even as the SMA elements undergo reciprocating rotary action during their thermal cycling without running into system component rotation limits. The innovation distinguishes over other innovative approaches by way of at least the Ring Gear element, the manner of lock control, and the return assist element.
    Type: Grant
    Filed: January 24, 2020
    Date of Patent: September 28, 2021
    Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space Administration
    Inventors: Steven W. Bauman, Othmane Benafan