Patents Assigned to Administration
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Patent number: 10255382Abstract: A method for forming an optimized radiation shield design for a component including providing a computer system programmed to generate data files that define a component radiation shield having an optimized design based on pre-stored data defining particular radiation characteristics and user-provided data defining radiation shield design criteria. Radiation shield design criteria are inputted into the computer system which processes the inputted radiation shield design criteria and the pre-stored data defining particular radiation characteristics in order to generate data files defining an optimized design for a component radiation shield. The generated data files defining the optimized design for a component radiation shield are provided to a metallic three-dimensional printing system. The three-dimensional printing system is then activated to form a component radiation shield using a predetermined metal powder and the generated data files that define the optimized component radiation shield design.Type: GrantFiled: August 24, 2017Date of Patent: April 9, 2019Assignee: The United States of America as represented by the Administrator of NASAInventors: Jean-Marie Lauenstein, Steven J. Kenyon, Raymond L. Ladbury, Thomas Jordan
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Patent number: 10249929Abstract: A multimode directional coupler is provided. In some embodiments, the multimode directional coupler is configured to receive a primary signal and a secondary signal at a first port of a primary waveguide. The primary signal is configured to propagate through the primary waveguide and be outputted at a second port of the primary waveguide. The multimode directional coupler also includes a secondary waveguide configured to couple the secondary signal from the primary waveguide with no coupling of the primary signal into the secondary waveguide. The secondary signal is configured to propagate through the secondary waveguide and be outputted from a port of the secondary waveguide.Type: GrantFiled: January 29, 2016Date of Patent: April 2, 2019Assignee: The United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventors: Rainee N Simons, Edwin G Wintucky
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Patent number: 10243412Abstract: A passive beamforming rectenna includes a plurality of antennas, a plurality of terminal port rectifying circuits, and a beamforming network. The beamforming network includes (a) a plurality of antenna ports connecting to the plurality of antennas, and (b) a plurality of terminal ports connecting to the plurality of terminal port rectifying circuits. The beamforming network further includes a microwave lens or any of a variety of other structures. The beamforming rectenna is characterized by a plurality of radiation distribution patterns. Electromagnetic power is received through the plurality of antennas.Type: GrantFiled: August 25, 2016Date of Patent: March 26, 2019Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Patrick W. Fink, Gregory Y. Lin, Timothy F. Kennedy, Phong H. Ngo, Haley C. Boose
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Patent number: 10242439Abstract: Methods and systems for analyzing and processing digital data comprising a plurality of infra-red (IR) video images acquired by a pulse thermography system are used to compute video data from the raw and smoothed video data acquired for the performance of non-destructive evaluation. New video data types computed may include but are not limited to contrast evolution data such as normalized contrast, converted contrast and normalized temperature contrast. Additionally, video data types computed comprise surface temperature, surface temperature rise and temperature simple contrast.Type: GrantFiled: August 16, 2017Date of Patent: March 26, 2019Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Ajay M. Koshti
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Patent number: 10240000Abstract: Novel aromatic polyimides are disclosed with sufficient physical properties to be useful in 3D printing.Type: GrantFiled: September 24, 2014Date of Patent: March 26, 2019Assignees: PolyOne Corporation, The Unted States of America as represented by The Administrator of the National Aeronautics and Space AdministrationsInventors: Roger W. Avakian, Ling Hu, Chun-Hua Chuang
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Patent number: 10243250Abstract: A two-way microwave power divider (the “power divider”) may include an input port and two output ports. The power divider may also include a junction that is configured to split a feedline from the input port into a first transmission line and a second transmission line. One or more resistors may be placed along the first transmission line and the second transmission line to provide isolation between the two output ports.Type: GrantFiled: February 14, 2017Date of Patent: March 26, 2019Assignee: The United States of America, as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Kongpop U-Yen, Nathan Kovarik
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Patent number: 10236166Abstract: A lenslet based integral field spectrograph (IFS) may have a design that makes better use of the detector pixels by placing adjacent spectra next to each other rather than staggering the spectra. Such a design maintains the main compactness and simplicity of prior lenslet array based IFSs, but improves the detector efficiency, which is rather low in conventional lenslet array based IFSs.Type: GrantFiled: June 9, 2017Date of Patent: March 19, 2019Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Qian Gong, David A. Content, Michael W. McElwain, Avram Max Mandell, Tyler D. Groff, Maxime J. Rizzo
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Patent number: 10236693Abstract: Some embodiments of the present invention describe a battery including a plurality of master-less controllers. Each controller is operatively connected to a corresponding cell in a string of cells, and each controller is configured to bypass a fraction of current around the corresponding cell when the corresponding cell has a greater charge than one or more other cells in the string of cells.Type: GrantFiled: December 19, 2016Date of Patent: March 19, 2019Assignee: The United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventors: Robert Button, Marcelo C. Gonzalez
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Patent number: 10228465Abstract: An apparatus for improving a pointing capability of an optical pointing system includes a star tracker attitude control system for maintaining an alignment between the optical pointing system and a target, a beam steering mirror controlled by the star tracker attitude control system to direct an optical signal to impinge on the target, a fixed optical assembly configured to direct a portion of the optical signal from the bean steering mirror into a field of view of a star tracker telescope of the star tracker attitude control system, and a detector array for detecting the portion of the optical signal superimposed over a location in a current star scene in the star tracker telescope field of view, where the star tracker attitude control system is configured to operate the beam steering mirror to maintain the optical signal on the target by maintaining the superimposed signal on the location in the star scene.Type: GrantFiled: June 14, 2017Date of Patent: March 12, 2019Assignee: 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: 10227469Abstract: A polyamide aerogel and method of making the same is disclosed. The aerogel includes para-substituted monomers without a cross-linking agent.Type: GrantFiled: August 17, 2016Date of Patent: March 12, 2019Assignee: The United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventors: Jarrod C. Williams, Mary Ann B. Meador
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Patent number: 10227950Abstract: A thermoacoustic engine is provided that uses acoustic energy to operate a piston in a double-acting action. The acoustic energy is amplified as a sound wave travels through the thermoacoustic engine. The amplified acoustic energy is extracted and converted into usable electrical energy.Type: GrantFiled: January 30, 2017Date of Patent: March 12, 2019Assignee: The United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventor: Rodger W. Dyson, Jr.
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Patent number: 10229604Abstract: A software tool assists airline dispatchers and other professionals in management of winter weather events at airports. The flight awareness collaboration tool (FACT) may gather pertinent weather information, air traffic information, airport information, and any other suitable information onto one display screen. FACT can be used by airline dispatchers to manage the airline fleet prior to during the day of a winter weather event, and may have built-in automation tools that can predict the impact of winter weather on airport capacity. FACT may be designed to support collaboration between the airline dispatcher, the air traffic control tower, the airport authority, and de-icing operators on the ground.Type: GrantFiled: June 30, 2017Date of Patent: March 12, 2019Assignee: The United States of America as Represented by the Administrator of the NASAInventors: Richard Hugh Mogford, Cody Allan Evans
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Patent number: 10230216Abstract: A tunable QCL source that utilizes a full bandwidth of a broadband THz QCL, and produces a significantly large number of frequency channels, is provided. The tunable QCL source includes a grating router configured to receive a terahertz frequency from a tunable quantum cascade laser and generate a plurality of terahertz frequencies. The tunable QCL source also includes a waveguide controller configured to receive the plurality of terahertz frequencies from the grating router, and select a desired terahertz frequency from the plurality of terahertz frequencies to be outputted by a waveguide multiplexer.Type: GrantFiled: April 28, 2015Date of Patent: March 12, 2019Assignee: The United States of America as Represented by the Admin of the National Aeronautics and Space AdministrationInventors: Hung D. Nguyen, Rainee N. Simons, Edwin G. Wintucky
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Patent number: 10225114Abstract: A wireless system, and particularly, a multiple-input multiple-output (MIMO) wireless communication system is disclosed. The wireless system includes a plurality of (re)configurable antennas and a rate-two space coding design for a MIMO system. The MIMO wireless communication system generally includes M (re)configurable antennas configured to independently transmit or broadcast wireless electromagnetic signals having a frequency in the microwave and/or optical ranges, a controller configured to control the (re)configurable antennas, and an encoder configured to encode information onto the wireless electromagnetic signals. The information comprises codewords having N symbols, and the codewords are expressed in an N×M matrix having a non-zero determinant and in which at least one symbol is associated with a coefficient configured to maximize diversity, maximize coding gain and/or reduce channel fading in the MIMO wireless communication system. M and N are each independently an integer of at least 2.Type: GrantFiled: October 3, 2016Date of Patent: March 5, 2019Assignees: CSUB Auxillary For Sponsored Programs Administration, The Regents of the University of CaliforniaInventors: Vida Vakilian, Hani Mehrpouyan, Hamid Jafarkhani
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Patent number: 10197165Abstract: A method is provided for installing a valve seat in the hole of a valve element. The valve seat is fabricated from a seal material having a freezing temperature. The seal material is stretched such that a portion thereof has a reduced diameter that is less than the diameter of the valve element's hole. The stretched portion of the seal material is immersed in a first environment having a temperature that is less than the freezing temperature of the seal material to thereby freeze the stretched portion and fix its reduced diameter. The stretched and frozen portion is then placed in the valve element's hole with the combination then being placed in a second environment having a temperature that is greater than the freezing temperature of the seal material.Type: GrantFiled: February 3, 2016Date of Patent: February 5, 2019Assignee: The United States of America as Represented by the Administrator of NASAInventors: James A. Richard, Brad M. Addona
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Patent number: 10196125Abstract: A stretchable mesh material extends across the opening of a cavity of the landing gear of an aircraft when the landing gear is in the deployed position. The mesh material alters the flow of air across the opening of the landing gear cavity and significantly reduces the amount of noise produced by the wheel well at low-to-mid frequencies.Type: GrantFiled: May 15, 2017Date of Patent: February 5, 2019Assignee: The United States of America as represented by the Administrator of NASAInventor: Mehdi R. Khorrami
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Patent number: 10196603Abstract: A method of manufacturing and/or using a scaffold assembly for stem cell culture and tissue engineering applications is disclosed. The scaffold at least partially mimics a native biological environment by providing biochemical, topographical, mechanical and electrical cues by using an electroactive material. The assembly includes at least one layer of substantially aligned, electrospun polymer fiber having an operative connection for individual voltage application. A method of cell tissue engineering and/or stem cell differentiation that uses the assembly seeded with a sample of cells suspended in cell culture media, incubates and applies voltage to one or more layers, and thus produces cells and/or a tissue construct.Type: GrantFiled: August 3, 2017Date of Patent: February 5, 2019Assignee: The United States of America as represented by the Administrator of NASAInventors: Lisa A. Scott Carnell, Emilie J. Siochi, Nancy M. Holloway, Kam W. Leong, Karina Kulangara
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Patent number: 10195749Abstract: A tension stiffened and tendon actuated manipulator is provided performing robotic-like movements when acquiring a payload. The manipulator design can be adapted for use in-space, lunar or other planetary installations as it is readily configurable for acquiring and precisely manipulating a payload in both a zero-g environment and in an environment with a gravity field. The manipulator includes a plurality of link arms, a hinge connecting adjacent link arms together to allow the adjacent link arms to rotate relative to each other and a cable actuation and tensioning system provided between adjacent link arms. The cable actuation and tensioning system includes a spreader arm and a plurality of driven and non-driven elements attached to the link arms and the spreader arm. At least one cable is routed around the driven and non-driven elements for actuating the hinge.Type: GrantFiled: October 26, 2015Date of Patent: February 5, 2019Assignee: The United States of America as represented by the Administrator of NASAInventors: William R. Doggett, John T. Dorsey, George G. Ganoe, Bruce D. King, Thomas C. Jones, Charles D. Mercer, Cole K. Corbin
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Patent number: 10189700Abstract: An integrated circuit (IC) chip with a self-contained fluid sensor and method of making the chip. The sensor is in a conduit formed between a semiconductor substrate and a non-conductive cap with fluid entry and exit points through the cap. The conduit may be entirely in the cap, in the substrate or in both. The conduit includes encased temperature sensors at both ends and a central encased heater. The temperature sensors may each include multiple encased diodes and the heater may include multiple encased resistors.Type: GrantFiled: September 28, 2016Date of Patent: January 29, 2019Assignee: The United States of America as represented by the Administrator of NASAInventors: George Manos, Manuel A. Balvin, Michael P. Callahan
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Patent number: 10191163Abstract: A method of mapping pixel locations of a detector array includes measuring a location on the detector array, initiating a frame readout of the detector array, measuring a location of one or more metrology targets on the detector array, analyzing the frame readout to identify a pixel at the location on the detector array, and defining a location of the identified pixel with respect to the location of the one or more metrology targets. Subsequent measurement of the metrology targets alone by another metrology system allows one to infer the six degree of freedom alignment of the detector array in space.Type: GrantFiled: June 8, 2016Date of Patent: January 29, 2019Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Phillip Coulter, Raymond Ohl, Timothy Madison