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:
February 6, 2017
Date of Patent:
October 29, 2019
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, J. Chris Johnston, Maria A. Kuczmarski
Abstract: 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:
Grant
Filed:
September 24, 2015
Date of Patent:
October 22, 2019
Assignee:
The United States of America as represented by the Admininstrator of the National Aeronautics and Space Administration
Inventors:
Mahmooda Sultana, Mary J. Li, Anthony W. Yu
Abstract: 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:
Grant
Filed:
December 6, 2016
Date of Patent:
October 22, 2019
Assignee:
United States of America as Represented by the Administrator of National Aeronautics and Space Administration
Inventors:
Santo A. Padula, II, James Benzing, Vivake M. Asnani
Abstract: 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:
Grant
Filed:
March 28, 2016
Date of Patent:
October 22, 2019
Assignee:
United States of America as Represented by the Administrator of National Aeronautics and Space Administration
Abstract: 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:
Grant
Filed:
April 11, 2016
Date of Patent:
October 15, 2019
Assignee:
United States of America as Represented by the Administrator of National Aeronautics and Space Administration
Inventors:
Mary Ann B. Meador, Felix A. Miranda, Frederick W. Van Keuls
Abstract: 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:
Grant
Filed:
July 19, 2012
Date of Patent:
October 15, 2019
Assignee:
United States of America as Represented by the Administrator of National Aeronautics and Space Administration
Inventors:
Gary W Hunter, Jennifer C Xu, Chung-Chiun Liu
Abstract: 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:
Grant
Filed:
December 8, 2017
Date of Patent:
October 1, 2019
Assignee:
United States of America as Represented by the Administrator of National Aeronautics and Space Administration
Abstract: 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:
Grant
Filed:
May 19, 2017
Date of Patent:
October 1, 2019
Assignee:
United States of America as Represented by the Administrator of National Aeronautics and Space Administration
Inventors:
Santo A. Padula, II, James Benzing, Colln M. Creager
Abstract: 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:
Grant
Filed:
January 20, 2015
Date of Patent:
October 1, 2019
Assignee:
United States of America as Represented by the Administrator of National Aeronautics and Space Administration
Inventors:
Susan Y. Wrbanek, John D. Wrbanek, Gustave C. Fralick
Abstract: 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:
Grant
Filed:
August 25, 2016
Date of Patent:
October 1, 2019
Assignee:
U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
Inventors:
Anthony W. Yu, Michael A. Krainak, Diego Janches, Sarah L. Jones, Branimir Blagojevic
Abstract: 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:
Grant
Filed:
March 9, 2017
Date of Patent:
September 17, 2019
Assignee:
U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
Abstract: 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:
Grant
Filed:
August 17, 2016
Date of Patent:
September 17, 2019
Assignee:
United States of America as Represented by the Administrator of the National Aeronautics and Space Administration
Abstract: 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:
Grant
Filed:
September 22, 2015
Date of Patent:
September 10, 2019
Assignee:
United States of America as represented by the Adminsitrator of the National Aeronautics and Space Administration
Inventors:
Glen F. Steele, Chatwin Lansdowne, Joan P. Zucha, Adam M. Schlesinger
Abstract: 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:
Grant
Filed:
September 18, 2015
Date of Patent:
August 27, 2019
Assignee:
U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
Inventors:
Keith C. Gendreau, Zaven Arzoumanian, Robert G. Baker, Norman Dobson, Richard Koenecke
Abstract: 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:
Grant
Filed:
May 18, 2016
Date of Patent:
August 27, 2019
Assignee:
United States of America as Represented by the Administrator of National Aeronautics and Space Administration
Abstract: 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:
Grant
Filed:
May 16, 2016
Date of Patent:
August 13, 2019
Assignee:
United States of America as Represented by the Administrator of the National Aeronautics and Space Administration
Abstract: Pressure sensors are disclosed that may perform health monitoring in-situ in harsh operating environments. The pressure sensors may be based on a Clapp-type oscillator that includes one or more resistors, one or more inductors, capacitors, a sensor, and a transistor. Such pressure sensors may be particularly well-suited various applications, such as gas turbine engines, oil and gas extraction, vehicle engines, and exhaust monitoring.
Type:
Grant
Filed:
April 11, 2017
Date of Patent:
August 13, 2019
Assignee:
United States of America as Represented by the Administrator of National Aeronautics and Space Administration
Abstract: 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:
Grant
Filed:
August 31, 2016
Date of Patent:
August 13, 2019
Assignee:
United States of America as Represented by the Administrator of National Aeronautics and Space Administration
Abstract: The disclosure is directed to a blackbody calibration target having a textured silicon substrate comprising a base comprising a plurality of needle like structures extending away from the base and having a total emissivity of greater than 99.5% from an electromagnetic radiation source having a wavelength greater than or equal to about 400 nanometers and less than or equal to about 1 mm. The disclosure is further directed to a blackbody calibration target system, and instrument which includes the blackbody calibration target, and a method of calibrating an instrument.
Type:
Grant
Filed:
December 21, 2016
Date of Patent:
August 6, 2019
Assignee:
The United States of America as Represented by the Administrator of the National Aeronautics and Space Administration
Inventors:
William R. Johnson, Karl Y. Yee, Simon J. Hook
Abstract: One or more substitutional elements may be used to reduce the solution treatment temperature and required quench rates for hardening of 60-NITINOL. The advantages of modified NITINOL include that less energy is consumed during the heat treatment process, the material is subjected to less thermal distortion, and less machining is required. Modified NITINOL may have adequate hardness for bearing applications and may display highly elastic behavior.
Type:
Grant
Filed:
February 27, 2014
Date of Patent:
July 30, 2019
Assignee:
The United States of America as Represented by the Administrator of National Aeronautics and Space Administration
Inventors:
Malcolm K. Stanford, Ronald D. Noebe, Christopher DellaCorte, Glen Bigelow, Fransua Thomas