Patents Assigned to and Space Administration
-
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
-
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
-
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
-
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
-
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
-
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
-
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
-
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
-
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
-
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
-
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
-
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.
-
Patent number: 10196143Abstract: A modular Unmanned Aerial System (UAS) has first and second flight configurations, and includes an Unmanned Aerial Vehicle (UAV) parent module and a plurality of UAV child modules. The parent module may have a fuselage, forward and aft wings connected to the fuselage, and a first plurality of flight propulsion devices. The child modules have a corresponding second plurality of flight propulsion devices. Each child module docks wingtip-to-wingtip with the parent module or an adjacent edge of a child module using the docking mechanisms. The child modules undock and separate from the forward wing and each other, and achieve controlled flight independently of the parent module while in the second flight configuration. A method for controlling the modular UAS is also disclosed.Type: GrantFiled: June 2, 2017Date of Patent: February 5, 2019Assignee: THE UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONInventors: Jesse R. Quinlan, Michael D. Patterson
-
Patent number: 10192970Abstract: A simultaneous ohmic contact to silicon carbide includes a mixture of platinum, titanium, and silicon compounds deposited on a silicon carbide substrate. The silicon carbide substrate includes an n-type surface and a p-type surface.Type: GrantFiled: August 11, 2014Date of Patent: January 29, 2019Assignee: The United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventor: Robert S. Okojie
-
Patent number: 10192173Abstract: Method and systems are disclosed for training state-classifiers for classification of cognitive state. A set of multimodal signals indicating physiological responses of an operator are sampled over a time period. A depiction of operation by the operator during the time period is displayed. In response to user input selecting a cognitive state for a portion of the time period, the one or more state-classifiers are trained. In training the state-classifiers, the set of multimodal signals sampled in the portion of the time period are used as input to the one or more state-classifiers and the selected one of the set of cognitive states is used as a target result to be indicated by the one or more state-classifiers.Type: GrantFiled: April 18, 2017Date of Patent: January 29, 2019Assignee: THE UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONInventors: Chad L. Stephens, Angela R. Harrivel, Alan T. Pope, Lawrence J Prinzel, III
-
Patent number: 10189565Abstract: A modular Unmanned Aerial System (UAS) includes an Unmanned Aerial Vehicle (UAV) parent module and UAV child modules. A main wing extends from a respective fuselage of the modules. The UAS includes docking mechanisms coupled to wingtips of the main wings. The child modules dock with the wingtips of the parent or an adjacent child module. Docking forms a linked-flight configuration, with undocking and separation from the parent or adjacent child module achieving an independent-flight configuration. The modules have booms arranged transverse to the main wings and parallel to the longitudinal axis, as well as front and rear rotors/propellers. The front and rear propellers have axes of rotation that are normal to a plane of the longitudinal axis in a vertical takeoff and landing (VTOL) configuration, with the axis of rotation of the rear propellers parallel to the longitudinal axis in a forward-flight configuration.Type: GrantFiled: November 30, 2017Date of Patent: January 29, 2019Assignee: THE UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONInventors: Michael D. Patterson, Jesse R. Quinlan, William J. Fredericks
-
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
-
Patent number: 10184405Abstract: A process for mitigating or proactively avoiding an aircraft engine icing event may include detecting ice crystals in the atmosphere using one or more sensors on board an aircraft in real time. The process may also include modulating one or more engine operating conditions to proactively change an ice accretion location, to avoid the occurrence of an icing event. The process may further include implementing one or more modulated engine operating conditions in engine controls software, hardware, or both.Type: GrantFiled: March 30, 2017Date of Patent: January 22, 2019Assignee: The United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventors: Joseph P. Veres, Philip C. Jorgenson
-
Patent number: 10184777Abstract: A system and method for determining a change in a thickness and temperature of a surface of a material are disclosed herein. The system and the method are usable in a thermal protection system of a space vehicle, such as an aeroshell of a space vehicle. The system and method may incorporate micro electric sensors arranged in a ladder network and capacitor strip sensors. Corrosion or ablation causes a change in an electrical property of the sensors. An amount of or rate of the corrosion or the ablation and a temperature of the material is determined based on the change of the electrical property of the sensors.Type: GrantFiled: August 22, 2017Date of Patent: January 22, 2019Assignee: The United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventor: Robert S. Okojie
-
Patent number: 10180699Abstract: An apparatus, method, and system for controlling motion in six degrees of freedom is described. The apparatus includes a support structure, a first pedal and a second pedal. A first set of three independent articulating mechanisms is operatively connected to the support structure and the first pedal. The first set of three independent articulating mechanisms, in combination, enable motion of the first pedal in three control axes corresponding to three discrete degrees of freedom. A second set of three independent articulating mechanisms, operatively connected to the second pedal, enable motion, in combination, in three control axes corresponding to a discrete second set of three degrees of freedom. The apparatus may also include first and second sensors configured to detect the motion of the first and second pedals.Type: GrantFiled: July 30, 2014Date of Patent: January 15, 2019Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Stanley G. Love, Lee M. Morin, Mary E. McCabe