Patents Assigned to Administration
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Patent number: 10306155Abstract: A dual band infrared imaging system self-contained to fit within a small spacecraft is provided. The imaging system uses a detector array cooled by a mini cryocooler, and includes telescope optics and two bandpass filters for fire detection and thermal and evapotranspiration Earth science.Type: GrantFiled: June 28, 2016Date of Patent: May 28, 2019Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Murzban D. Jhabvala, Donald E. Jennings, Compton J. Tucker
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Patent number: 10298060Abstract: An apparatus and method of wirelessly powering an aerospace vehicle while the vehicle is on the ground is provided to solve a problem of supplying electric power for aircraft while idling on taxiways. Present systems typically require fuel-driven auxiliary power units (APU's) to generate electricity. Running APU's to power aircraft while idling requires over 443 million gallons of jet fuel annually at a cost of $1.3 billion dollars. This results in an estimated 4.7 megatons of carbon dioxide emissions annually. At the gate, shore power is provided via hardline connection.Type: GrantFiled: September 14, 2016Date of Patent: May 21, 2019Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Michael R. Wright
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Patent number: 10294099Abstract: 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: GrantFiled: March 7, 2013Date of Patent: May 21, 2019Assignee: The United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventors: Azlin M. Biaggi-Labiosa, Gary W. Hunter
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Patent number: 10293481Abstract: In an embodiment, a relative deflection detector may include at least two structural arcs, and a predetermined number of means for measuring position capable of determining the relative deflection in a first component. The at least two structural arcs may be for example, comprised of a first and second structural arc whereby the first and second structural arcs are attached to the first component at respective first and second predetermined locations and whereby each arc is comprised of a respective sequence of indicators, such as, for example, codes inscribed on the outer circumference of each arc. The first and second structural arcs may be positioned in concentric and coplanar relationship with each other.Type: GrantFiled: December 14, 2016Date of Patent: May 21, 2019Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Roger Rovekamp, Adam H. Parsons, Nicolaus A. Radford, Carolynn J Kanelakos, Peter Neuhaus, Joshua S. Mehling
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Patent number: 10297376Abstract: A bi-stable pin actuator includes a soft magnetic core and having a first central portion and a second central portion spaced apart from the first central portion. The first central portion has a first passage extending there-through and the second portion has a second passage extending there-through which is coaxial with the first passage. A first coil is wound about the first central portion and a second coil is wound about the second central portion. A pair of permanent magnets are located in the space between the first central portion and second central portion and attached to the core. An armature is movably positioned between and spaced apart from the permanent magnets. A pin is attached to the armature and extends into the first passage and second passages such that movement of the armature results in movement of the pin within the first passage and second passage.Type: GrantFiled: September 25, 2017Date of Patent: May 21, 2019Assignee: The United States of America as represented by the Administrator of NASAInventor: Joseph C. Church
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Patent number: 10282841Abstract: Biometric analysis of vascular patterning may be performed in 3D and 2D as an integrative biomarker of complex molecular and mechanical signaling. The vascular patterning may facilitate the coordination of essentially unlimited numbers of bioinformatics dimensions for specific molecular and other co-localizations with spatiotemporal dimensions of vascular morphology. The vascular patterning may also apply geometric principles of translational versus rotational principles for vascular branching to support the transformation of VESGEN 2D to VESGEN 3D.Type: GrantFiled: July 18, 2016Date of Patent: May 7, 2019Assignee: The United States of America as Represented by the Administrator of the NASAInventors: Patricia A. Parsons-Wingerter, Mary B. Vickerman
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Patent number: 10281907Abstract: Methods and systems for controlling a physical system (plant) are disclosed. The plant is modeled as a linear, finite-dimensional system having a state vector, a control input vector, a plant output vector, and a disturbance vector comprising disturbances having known basis functions and unknown amplitudes. An adaptive control law is used with separate adaptive gains for an error vector associated with the plant output vector, and the disturbance vector, plus a fixed gain for a disturbance estimator. The adaptive control law is operable to adjust the control input vector so as to minimize the error vector. The plant includes modes which are not Almost Strictly Positive Real (ASPR).Type: GrantFiled: April 22, 2016Date of Patent: May 7, 2019Assignee: United Stated of America as Represented by the Administrator of the NASAInventors: Susan A. Frost, Mark J. Balas
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Patent number: 10277346Abstract: A high efficiency secondary signal combiner may include a frequency division multiplexer that is configured to receive two or more signals and produce a combined signal. The combined signal may include the two or more signals, and each of the two or more signals may be in different Nyquist zones. The combiner may also include a wideband analog-to-digital converter (ADC) that is configured to frequency shift the combined signal by sub-sampling the two or more signals to produce a sub-sampled signal in a Nyquist zone that is different from the Nyquist zones of the two or more signals.Type: GrantFiled: July 8, 2016Date of Patent: April 30, 2019Assignee: The United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventors: James M. Downey, Bryan L. Schoenholz, Joseph A. Downey
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Patent number: 10273944Abstract: A propellant distributor or anode includes a plenum chamber and a plurality of outlets. The at least one plenum chamber is configured to receive a flow of propellant from an inlet, and the plurality of outlets are configured to distribute the flow of propellant into an inner channel wall and an outer channel wall of a discharge channel.Type: GrantFiled: November 4, 2014Date of Patent: April 30, 2019Assignee: The United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventors: Wensheng Huang, John Yim
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Patent number: 10275548Abstract: Interactive diagnostic modeling evaluator (i-DME) for repairing a diagnostic matrix of a system. The diagnostic modeling evaluator cause steps to be performed comprising: evaluating a first diagnostic performance of a diagnostic unit using supervised data that includes one or more instances of a fault of a system; proposing a repair to the diagnostic unit based on the evaluated diagnostic performance; evaluating a second diagnostic performance of the diagnostic unit having the proposed repair; and upon determining that the second diagnostic performance meets a performance metric criterion, repairing the diagnostic unit according to the proposed repair.Type: GrantFiled: October 7, 2015Date of Patent: April 30, 2019Assignee: The United States of America as Represented by the Administrator of the NASAInventors: Anuradha Kodali, Peter I. Robinson
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Patent number: 10269463Abstract: Systems, methods, and devices of the various embodiments described herein enable an energy conversion system comprising a radioactive element for generating conduction-band electrons in an avalanche cell and generating heat, wherein the conduction-band electrons are provided to an anode to generate avalanche cell power, and the heat is provided to a thermoelectric generator to generate thermoelectric power. In an embodiment, the avalanche cell is irradiated with gamma rays, which excite electrons within the avalanche cell, generating a current. In an additional embodiment, the thermoelectric power and avalanche cell power can comprise a dual power system.Type: GrantFiled: February 3, 2016Date of Patent: April 23, 2019Assignee: The United States of America as represented by the Administrator of NASAInventors: Sang Hyouk Choi, Kunik Lee
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Patent number: 10268213Abstract: A check valve's housing has a valve disposed therein to open or close a flow path from the housing's inlet to its outlet based on a difference between pressures at the inlet and outlet. The valve includes a bellows, a poppet, and a spring. The poppet includes a hollow structure extending through the poppet's plate and terminating in a first open end disposed within the bellows, an annular flange between the second face of the poppet's plate and the housing's outlet, and an open-ended tube extending from the annular flange into the housing's outlet. The spring, disposed within the hollow tubular structure, positions the annular flange to seal the outlet when the pressure difference is less than a predetermined amount and compresses when the difference exceeds the predetermined amount wherein the annular flange is unsealed from the housing's outlet to open the flow path.Type: GrantFiled: October 20, 2017Date of Patent: April 23, 2019Assignee: The United States of America as Represented by the Administrator of NASAInventors: Brad M Addona, James A Richard, Richard J Joye
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Patent number: 10268453Abstract: A method of communicating between one or more modules while executing a plan for a controlled system includes transmitting, by an execution manager, a request to a planner to create a plan in response to receiving a planning goals file. The method also includes transmitting, by the execution manager, the created plan to an adaptive controller for execution of the created plan within a controlled system, and receiving, by the execution manager, state estimates reporting diagnosis information of a controlled system.Type: GrantFiled: March 7, 2016Date of Patent: April 23, 2019Assignee: United States of America as Represented by the Administrator of the NASAInventors: James Ong, Emilio Remolina, Peter I. Robinson
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Publication number: 20190115869Abstract: A spectrum splitting, transmissive concentrating photovoltaic (tCPV) module is proposed and designed for a hybrid photovoltaic-solar thermal (PV/T) system. The system may be able to fully utilize the full spectrum of incoming sunlight. By utilizing III-V triple junction solar cells with bandgaps of approximately 2.1 eV, 1.7 eV, and 1.4 eV in the module, ultraviolet (UV) and visible light (in-band light) are absorbed and converted to electricity, while infrared (IR) light (out-of-band light) passes through and is captured by a solar thermal receiver and stored as heat. The stored heat energy may be dispatched as electricity or process heat as needed. The tCPV module may have an overall power conversion efficiency exceeding 43.5% for above bandgap (in-band) light under a standard AM1.5D solar spectrum with an average concentration ratio of 400 suns. Passive and/or active cooling methods may be used to keep cells below 110° C.Type: ApplicationFiled: March 28, 2017Publication date: April 18, 2019Applicant: The Administrators of the Tulane Educational FundInventors: Matthew David Escarra, Qi Xy, Yaping Ji, Brian C. Riggs, Adam Ollanik, Kazi M. Islam, Daniel Codd, Vince Romanin, Nicholas David Farrar-Foley
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Patent number: 10259077Abstract: Surface energy of a substrate is changed without the need for any template, mask, or additional coating medium applied to the substrate. At least one beam of energy directly ablates a substrate surface to form a predefined topographical pattern at the surface. Each beam of energy has a width of approximately 25 micrometers and an energy of approximately 1-500 microJoules. Features in the topographical pattern have a width of approximately 1-500 micrometers and a height of approximately 1.4-100 micrometers.Type: GrantFiled: March 24, 2015Date of Patent: April 16, 2019Assignee: The United States of America as represented by the Administrator of NASAInventors: Christopher J. Wohl, Jr., Marcus A. Belcher, John W. Connell, John W. Hopkins
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Patent number: 10259975Abstract: The present invention relates to an easy, scalable method, relying on conventional and unconventional techniques, to incorporate tilt in the fabrication of synthetic polymer-based dry adhesives mimicking the gecko adhesive system. These dry, reversible adhesives demonstrate anisotropic adhesion properties, providing strong adhesion and friction forces when actuated in the gripping direction and an initial repulsive normal force and negligible friction when actuated in the releasing direction.Type: GrantFiled: December 1, 2016Date of Patent: April 16, 2019Assignee: The Administrators of the Tulane Educational FundInventors: Noshir Pesika, Kejia Jin
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Patent number: 10262951Abstract: A novel radiation hardened chip package technology protects microelectronic chips and systems in aviation/space or terrestrial devices against high energy radiation. The proposed technology of a radiation hardened chip package using rare earth elements and mulitlayered structure provides protection against radiation bombardment from alpha and beta particles to neutrons and high energy electromagnetic radiation.Type: GrantFiled: May 16, 2014Date of Patent: April 16, 2019Assignees: National Institute of Aerospace Associates, The United States of America as represented by the Administrator of NASAInventors: Jin Ho Kang, Godfrey Sauti, Cheol Park, Luke Gibbons, Sheila Ann Thibeault, Sharon E. Lowther, Robert G. Bryant
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Patent number: 10254325Abstract: A piezoelectric field disturbance sensing system includes a piezoelectric element for generating mechanical energy when electrically excited and for generating electrical energy when mechanically deformed. A mass is coupled to the piezoelectric element. A signal generator is coupled to the piezoelectric element for applying electrical energy thereto for a fixed period of time. As a result, the piezoelectric element undergoes mechanical deformation and the mass reverberates in response to such mechanical deformation. A charge monitor is coupled to the piezoelectric element for monitoring electrical energy generated thereby during a time period subsequent to the fixed period of time.Type: GrantFiled: April 21, 2015Date of Patent: April 9, 2019Assignee: The United States of America as represented the Administrator of the National Aeronautics and Space AdministrationInventor: Scott Jensen
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Patent number: 10256305Abstract: An electronic device includes a trigonal crystal substrate defining a (0001) C-plane. The substrate may comprise Sapphire or other suitable material. A plurality of rhombohedrally aligned SiGe (111)-oriented crystals are disposed on the (0001) C-plane of the crystal substrate. A first region of material is disposed on the rhombohedrally aligned SiGe layer. The first region comprises an intrinsic or doped Si, Ge, or SiGe layer. The first region can be layered between two secondary regions comprising n+doped SiGe or n+doped Ge, whereby the first region collects electrons from the two secondary regions.Type: GrantFiled: March 3, 2017Date of Patent: April 9, 2019Assignee: The United States of America as represented by the Administrator of NASAInventors: Sang Hyouk Choi, Yeonjoon Park, Glen C. King, Hyun-Jung Kim, Kunik Lee
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Patent number: 10256202Abstract: A durable bond pad structure is described that facilitates highly durable electrical connections to semiconductor microelectronics chips (e.g., silicon carbide (SiC) chips) to enable prolonged operation over very extreme temperature ranges.Type: GrantFiled: January 25, 2018Date of Patent: April 9, 2019Assignee: The United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventors: David J. Spry, Dorothy Lukco, Philip G. Neudeck, Carl W. Chang, Liangyu Chen, Roger D. Meredith, Kelley M. Moses, Charles A. Blaha, Jose M. Gonzalez, Glenn M. Beheim, Kimala L. Laster