Patents Assigned to and Space Administration
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Patent number: 10465281Abstract: The present invention relates to a high resolution additive manufacturing method, including: creating a rigid shell of a stable material on all surfaces except for a sprue of a three dimensional (3D) polymer part using a chemical vapor deposition (CVD) process which includes: depositing the stable material at a process temperature of 100° C. or less, and operating at, or near, atmospheric pressure; and removing the 3D polymer part by accessing the inside of the rigid shell through the sprue to allow dissolution of the 3D polymer part, thereby leaving a replicated rigid shell of the stable material.Type: GrantFiled: August 15, 2016Date of Patent: November 5, 2019Assignee: U.S.A. as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Vincent T. Bly
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Patent number: 10460714Abstract: 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: GrantFiled: February 6, 2017Date of Patent: October 29, 2019Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventors: Lisa Danielle Koch, Michael G. Jones, Peter J. Bonacuse, Christopher J. Miller, J. Chris Johnston, Maria A. Kuczmarski
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Patent number: 10461621Abstract: An electro hydrodynamic pump apparatus includes a cartridge body member that includes an interior cavity portion and openings on either end of the cartridge body member. A first electrode member is disposed within the interior cavity portion of the cartridge body member. The first electrode member includes a conductive bar member which has a plurality of spaced apart elements extending therefrom. A second electrode member is also disposed within the interior cavity portion of the cartridge body member. The second electrode member also includes a conductive bar with a plurality of spaced apart elements extending therefrom. The elements of the first electrode member are configure to be interspersed with the elements of the second electrode member when the first electrode member and the second electrode member are disposed within the interior cavity portion of the cartridge body member.Type: GrantFiled: December 28, 2015Date of Patent: October 29, 2019Assignee: United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Matthew T. Showalter, Jeffrey R. Didion, Mario S. Martins, Franklin L. Robinson
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Patent number: 10450650Abstract: The present invention relates to a method of manufacturing large area graphene for graphene-based photonics devices such as bolometric graphene detectors, or for use as a saturable absorber in ultra-high bandwidth detectors for producing ultrafast laser pulses. The method includes: growing a first graphene layer on one side of a metal substrate, and a second graphene layer on another side of the metal substrate; coating the first graphene layer with a plurality of resist layers including a low molecular weight polymethylmethacrylate, and a high molecular weight polymethylmethacrylate; removing the second graphene layer and the metal substrate to reveal the first graphene layer; disposing the first graphene layer on an optical substrate; and removing the plurality of resist layers from the first graphene layer to reveal a final graphene layer, which can be used as the basis to manufacture a multilayer graphene structure for graphene detectors.Type: GrantFiled: September 24, 2015Date of Patent: October 22, 2019Assignee: The United States of America as represented by the Admininstrator of the National Aeronautics and Space AdministrationInventors: Mahmooda Sultana, Mary J. Li, Anthony W. Yu
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Patent number: 10450080Abstract: A hybrid propulsion system for an aircraft is provided that includes a turbine engine, a first electric machine assembly connected to the turbine engine, a second electric machine assembly driven by the first electric machine assembly, and multiple third electric machine assemblies driven by the first electric machine assembly, wherein the multiple third electric machines provide a thrust output to propel the aircraft.Type: GrantFiled: March 28, 2016Date of Patent: October 22, 2019Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventor: Raymond F. Beach
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Patent number: 10449804Abstract: A tire includes a plurality of SMA springs. Each SMA spring includes a first end portion, a second end portion, and an arching middle portion. Each SMA spring is interlaced with at least one other SMA spring thereby forming a laced toroidal structure extending about an entire circumference of the tire.Type: GrantFiled: December 6, 2016Date of Patent: October 22, 2019Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventors: Santo A. Padula, II, James Benzing, Vivake M. Asnani
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Patent number: 10444180Abstract: A polymer electrolyte-based sensor is disclosed. The sensor includes a conductive polymer electrolyte film including water-retaining components. The water-retaining components facilitate operational conductivity of the conductive polymer electrolyte film in lower humidity environments than would be possible without the water-retaining components.Type: GrantFiled: July 19, 2012Date of Patent: October 15, 2019Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventors: Gary W Hunter, Jennifer C Xu, Chung-Chiun Liu
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Patent number: 10446920Abstract: Systems and methods for lightweight, customizable antenna with improved performance and mechanical properties are disclosed. In some aspects, aerogels can be used, for example, as a substrate for antenna fabrication. The reduced weight and expense, as well as the increased ability to adapt antenna designs, permits a systems to mitigate a variety of burdens associated with antennas while providing added benefits.Type: GrantFiled: April 11, 2016Date of Patent: October 15, 2019Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventors: Mary Ann B. Meador, Felix A. Miranda, Frederick W. Van Keuls
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Patent number: 10427461Abstract: A tire having a plurality of shape memory alloy (SMA) radial stiffening elements including a first end portion, a second end portion, and an arching middle portion. Each SMA radial element is secured to the rim of a wheel to form arching elements extending about an entire circumference of the tire.Type: GrantFiled: May 19, 2017Date of Patent: October 1, 2019Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventors: Santo A. Padula, II, James Benzing, Colln M. Creager
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Patent number: 10429243Abstract: The present invention relates an apparatus and method for measuring range-resolved atmospheric sodium temperature profiles using a space-based Lidar instrument, including a diode-pumped Q-switched self-Raman c-cut Nd:YVO4 laser with intra-cavity frequency doubling that could produce multi-watt 589 nm wavelength output. The c-cut Nd:YVO4 laser has a fundamental wavelength that is tunable from 1063-1067 nm. A continuous wave narrow linewidth diode laser is used as an injection seeder to provide single-frequency grating tunable output around 1066 nm. The injection-seeded self-Raman shifted Nd:VO4 laser is tuned across the sodium vapor D2 line at 589 nm. In one embodiment, a space-qualified frequency-doubled 9 Watt at 532 nm wavelength Nd:YVO4 laser, is utilized with a tandem interference filter temperature-stabilized fused-silica-etalon receiver and high-bandwidth photon-counting detectors.Type: GrantFiled: August 25, 2016Date of Patent: October 1, 2019Assignee: U.S.A. as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Anthony W. Yu, Michael A. Krainak, Diego Janches, Sarah L. Jones, Branimir Blagojevic
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Patent number: 10429521Abstract: A small, low power, solid state particle counter may be configured to detect radiation. A scintillator may be doped to emit light in a predetermined energy range when impacted by radiation particles. A photodiode attached to or held against the scintillator may be configured to detect the emitted light in the predetermined energy range and output a current proportional to an amount of the emitted light.Type: GrantFiled: January 20, 2015Date of Patent: October 1, 2019Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventors: Susan Y. Wrbanek, John D. Wrbanek, Gustave C. Fralick
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Patent number: 10433308Abstract: A sensor network may be configured to operate in extreme temperature environments. A sensor may be configured to generate a frequency carrier, and transmit the frequency carrier to a node. The node may be configured to amplitude modulate the frequency carrier, and transmit the amplitude modulated frequency carrier to a receiver.Type: GrantFiled: December 8, 2017Date of Patent: October 1, 2019Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventor: Michael J. Krasowski
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Patent number: 10428181Abstract: Porous cross-linked partially aliphatic polyimide networks are provided. The polyimide networks comprise a polyamic acid oligomer that (i) comprises a repeating unit of a dianhydride and a diamine and terminal functional groups, (ii) has an average degree of polymerization of 10 to 70, (iii) has been cross-linked via a cross-linking agent, comprising three or more cross-linking groups, at a balanced stoichiometry of the cross-linking groups to the terminal functional groups, and (iv) has been chemically imidized to yield the porous cross-linked polyimide network. The polyimide networks are partially aliphatic based on (a) the diamine comprising a first diamine and a second diamine, wherein the first diamine comprises a linear aliphatic backbone chain, and the second diamine does not, and/or (b) the dianhydride comprising a first dianhydride and a second dianhydride, wherein the first dianhydride comprises a linear aliphatic backbone chain, and the second dianhydride does not.Type: GrantFiled: October 11, 2017Date of Patent: October 1, 2019Assignees: OHIO AEROSPACE INSTITUTE, U.S. GOVERNMENT AS REPRESENTED BY THE ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONInventors: Mary Ann B. Meador, Baochau N. Nguyen, Haiquan Guo
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Patent number: 10414053Abstract: A robotic gripper for rigidly grasping a section of a Marman ring of a satellite, the robotic gripper having an outboard jaw which interfaces to an outer diameter side of the Marman ring, a inboard jaw which interfaces to an inner diameter side of the Marman ring, and a palm which interfaces to a separation surface of the Marman ring. The jaws, when grasping the section of the Marman ring, execute a two-stage motion comprising a first movement toward the opposing jaw in a direction parallel to the palm, and a second movement of drawing the Marman ring down against the palm or other suitable surface in order to fully rigidize the grasp.Type: GrantFiled: March 9, 2017Date of Patent: September 17, 2019Assignee: U.S.A. as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Matthew S. Ashmore
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Patent number: 10414485Abstract: The invention provides an improved propeller blade design by modifying a classic propeller blade design by changing the twist distribution across the propeller blade(s). This is accomplished by increasing the twist of each propeller blade on the inboard portion of the blade compared to a classic propeller design. At a break point, the twist provided across the propeller blade from the break point to the tip of the blade decreases so that the attack angle at the tip of the propeller blade is less than that of a classic propeller blade design.Type: GrantFiled: August 17, 2016Date of Patent: September 17, 2019Assignee: United States of America as Represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Albion H Bowers
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Patent number: 10411740Abstract: A soft decision analyzer system is operable to interconnect soft decision communication equipment and analyze the operation thereof to detect symbol wise alignment between a test data stream and a reference data stream in a variety of operating conditions.Type: GrantFiled: September 22, 2015Date of Patent: September 10, 2019Assignee: United States of America as represented by the Adminsitrator of the National Aeronautics and Space AdministrationInventors: Glen F. Steele, Chatwin Lansdowne, Joan P. Zucha, Adam M. Schlesinger
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Patent number: 10393682Abstract: A multiplexing x-ray fluorescence (MXRF) system and method are provided. The system can include a simple detector that counts x-rays with time resolution. A time-variable applied radiation source is used. The MXRF applied radiation source can produce an excitation spectrum with a peak average energy that grows with time and then recycles. Elemental identification can be achieved by time-correlating x-ray counts detected by the detector, with the time-variable applied radiation field. The system and method provide design flexibility for both commercial and NASA applications.Type: GrantFiled: September 18, 2015Date of Patent: August 27, 2019Assignee: U.S.A. as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Keith C. Gendreau, Zaven Arzoumanian, Robert G. Baker, Norman Dobson, Richard Koenecke
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Patent number: 10396709Abstract: Some embodiments of the present invention describe an apparatus that includes an oscillator, a ramp generator, and an inverter. The apparatus includes an oscillator, an inverter, and a ramp generator. The oscillator is configured to generate a waveform comprising a low time and a high time. The inverter is configured to receive the waveform generated by the oscillator, and invert the waveform. The ramp generator configured to increase a gate control voltage of a transistor connected to a solar cell, and rapidly decrease the gate control voltage of the transistor. During the low time of the waveform, a measurement of a current and a voltage of the solar cell is performed as the current and voltage of the solar cell are transmitted through a first channel and to a second channel.Type: GrantFiled: May 18, 2016Date of Patent: August 27, 2019Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventors: Michael J. Krasowski, Norman F. Prokop
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Patent number: 10378521Abstract: A microthruster system may include a substrate and a source film. The substrate may include a plurality of emitter tips, and a source film deposited on the substrate. The source film may include silver. The microthruster system may also include a solid electrolyte film, which may include chalcogenide film, deposited over the source film. The solid electrolyte film may cause ions of the source film to move to the plurality of emitter tips.Type: GrantFiled: May 16, 2016Date of Patent: August 13, 2019Assignee: United States of America as Represented by the Administrator of the National Aeronautics and Space AdministrationInventor: William C West
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Patent number: 10381455Abstract: A diffusion barrier system may prevent migration of gold, oxygen, or both on a plurality of ohmic contacts. The diffusion barrier system may include a first barrier system or a second barrier system. Each barrier system may include a first metallization layer, a second metallization layer, and a third metallization layer.Type: GrantFiled: August 31, 2016Date of Patent: August 13, 2019Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventor: Robert Okojie