Patents Assigned to and Space Administration
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Patent number: 9117948Abstract: A multi junction solar cell is provided and includes multiple semiconducting layers and an interface layer disposed between the multiple semiconducting layers. The interface layer is made from an interface bonding material that has a refractive index such that a ratio of a refractive index of each of the multiple semiconducting layers to the refractive index of the interface bonding material is less than or equal to 1.5.Type: GrantFiled: February 2, 2012Date of Patent: August 25, 2015Assignee: The United States of America as Represented by the Adminstrator of National Aeronautics and Space AdministrationInventor: Geoffrey A Landis
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Patent number: 9108178Abstract: Elongated microcapsules, such as elongated hydrophobic-core and hydrophilic-core microcapsules, may be formed by pulse stirring an emulsion or shearing an emulsion between two surfaces moving at different velocities. The elongated microcapsules may be dispersed in a coating formulation, such as paint.Type: GrantFiled: January 20, 2012Date of Patent: August 18, 2015Assignee: The United States of America as Represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Luz M. Calle, Wenyan N. Li, Jerry W. Buhrow, Stephen A. Perusich, Scott T. Jolley, Tracy L. Gibson, Martha K. Williams
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Patent number: 9102331Abstract: A multi-functional electric module (eModule) is provided for a vehicle having a chassis, a master controller, and a drive wheel having a propulsion-braking module. The eModule includes a steering control assembly, mounting bracket, propulsion control assembly, brake controller, housing, and control arm. The steering control assembly includes a steering motor controlled by steering controllers in response to control signals from the master controller. A mounting feature of the bracket connects to the chassis. The propulsion control assembly and brake controller are in communication with the propulsion-braking module. The control arm connects to the lower portion and contains elements of a suspension system, with the control arm being connectable to the drive wheel via a wheel input/output block. The controllers are responsive to the master controller to control a respective steering, propulsion, and braking function.Type: GrantFiled: September 20, 2013Date of Patent: August 11, 2015Assignees: GM Global Technology Operations LLC, The United States of America As Represented by the Administrator of the National Aeronautics and Space AdministrationInventors: William J. Bluethmann, Thomas M. Waligora, Nathan Fraser-Chanpong, Ryan Reed, Akinjide Akinniyi Akinyode, Ivan Spain, Andrew D. Dawson, Joshua M. Figuered, Eduardo Herrera, Mason M. Markee, Robert L. Vitale, Chunhao J. Lee, Lucien Q. Junkin, Ross Briant Winn, James Jonathan Rogers, Raymond Guo
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Patent number: 9097609Abstract: The present invention is a versatile hermetic seal leak detection apparatus for testing hermetically sealed containers and devices for leaks without the need to create a custom or specially manufactured testing chamber conforming to the dimensions of the specific object under test. The size of the testing chamber may be mechanically adjusted by the novel use of bellows to reduce and optimize the amount of gas space in a test chamber which surrounds the hermetically sealed object under test. The present invention allows the size of the test chamber to be selectively adjusted during testing to provide an optimum test chamber gas space. The present invention may be further adapted to isolate and test specific portions of the hermetically sealed object under test for leaks.Type: GrantFiled: April 30, 2013Date of Patent: August 4, 2015Assignee: The United States of America as Represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Anthony R. Kelley
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Patent number: 9090950Abstract: The present invention provides a process for suppressing abnormal grain growth in friction stir welded aluminum alloys by inserting an intermediate annealing treatment (“IAT”) after the welding step on the article. The IAT may be followed by a solution heat treatment (SHT) on the article under effectively high solution heat treatment conditions. In at least some embodiments, a deformation step is conducted on the article under effective spin-forming deformation conditions or under effective superplastic deformation conditions. The invention further provides a welded article having suppressed abnormal grain growth, prepared by the process above. Preferably the article is characterized with greater than about 90% reduction in area fraction abnormal grain growth in any friction-stir-welded nugget.Type: GrantFiled: October 12, 2011Date of Patent: July 28, 2015Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Stephen J Hales, Harold Dale Claytor, Joel A. Alexa
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Patent number: 9084933Abstract: Method for physiologically modulating videogames and simulations includes utilizing input from a motion-sensing video game system and input from a physiological signal acquisition device. The inputs from the physiological signal sensors are utilized to change the response of a user's avatar to inputs from the motion-sensing sensors. The motion-sensing system comprises a 3D sensor system having full-body 3D motion capture of a user's body. This arrangement encourages health-enhancing physiological self-regulation skills or therapeutic amplification of healthful physiological characteristics. The system provides increased motivation for users to utilize biofeedback as may be desired for treatment of various conditions.Type: GrantFiled: March 15, 2013Date of Patent: July 21, 2015Assignee: The United States of America as represented by the Administrator of the National Aeronatics and Space AdministrationInventors: Alan T. Pope, Chad L. Stephens, Christopher A. Jones
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Patent number: 9085302Abstract: A modular robotic vehicle includes a chassis, driver input devices, an energy storage system (ESS), a power electronics module (PEM), modular electronic assemblies (eModules) connected to the ESS via the PEM, one or more master controllers, and various embedded controllers. Each eModule includes a drive wheel containing a propulsion-braking module, and a housing containing propulsion and braking control assemblies with respective embedded propulsion and brake controllers, and a mounting bracket covering a steering control assembly with embedded steering controllers. The master controller, which is in communication with each eModule and with the driver input devices, communicates with and independently controls each eModule, by-wire, via the embedded controllers to establish a desired operating mode. Modes may include a two-wheel, four-wheel, diamond, and omni-directional steering modes as well as a park mode.Type: GrantFiled: September 20, 2013Date of Patent: July 21, 2015Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Christopher E. Borroni-Bird, Robert L. Vitale, Chunhao J. Lee, Robert O. Ambrose, William J. Bluethmann, Lucien Q. Junkin, Jonathan J. Lutz, Raymond Guo, Anthony Joseph Lapp, Justin S. Ridley
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Patent number: 9081096Abstract: An apparatus, method, and computer program for a resolution enhanced pseudo-noise coding technique for 3D imaging is provided. In one embodiment, a pattern generator may generate a plurality of unique patterns for a return to zero signal. A plurality of laser diodes may be configured such that each laser diode transmits the return to zero signal to an object. Each of the return to zero signal includes one unique pattern from the plurality of unique patterns to distinguish each of the transmitted return to zero signals from one another.Type: GrantFiled: August 31, 2012Date of Patent: July 14, 2015Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Steven X. Li
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Patent number: 9075749Abstract: An image-based phase retrieval technique has been developed that can be used on board a space based iterative transformation system. Image-based wavefront sensing is computationally demanding due to the floating-point nature of the process. The discrete Fourier transform (DFT) calculation is presented in “diagonal” form. By diagonal we mean that a transformation of basis is introduced by an application of the similarity transform of linear algebra. The current method exploits the diagonal structure of the DFT in a special way, particularly when parts of the calculation do not have to be repeated at each iteration to converge to an acceptable solution in order to focus an image.Type: GrantFiled: March 8, 2011Date of Patent: July 7, 2015Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Bruce H. Dean
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Patent number: 9073623Abstract: The present invention proposes a hardware and software architecture for dynamic modal structural monitoring that uses a robust modal filter to monitor a potentially very large-scale array of sensors in real time, and tolerant of asymmetric sensor noise and sensor failures, to achieve aircraft performance optimization such as minimizing aircraft flutter, drag and maximizing fuel efficiency.Type: GrantFiled: March 13, 2014Date of Patent: July 7, 2015Assignee: The United States of America as Represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Peter M. Suh
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Patent number: 9074066Abstract: Conventional toughening agents are typically rubbery materials or small molecular weight molecules, which mostly sacrifice the intrinsic properties of a matrix such as modulus, strength, and thermal stability as side effects. On the other hand, high modulus inclusions tend to reinforce elastic modulus very efficiently, but not the strength very well. For example, mechanical reinforcement with inorganic inclusions often degrades the composite toughness, encountering a frequent catastrophic brittle failure triggered by minute chips and cracks. Thus, toughening generally conflicts with mechanical reinforcement. Carbon nanotubes have been used as efficient reinforcing agents in various applications due to their combination of extraordinary mechanical, electrical, and thermal properties.Type: GrantFiled: February 22, 2011Date of Patent: July 7, 2015Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Cheol Park, Dennis C. Working, Emilie J. Siochi, Joycelyn S. Harrison
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Patent number: 9075188Abstract: A method of making a mirror from a single crystal blank may include fine grinding top and bottom surfaces of the blank to be parallel. The blank may then be heat treated to near its melting temperature. An optical surface may be created on an optical side of the blank. A protector may be bonded to the optical surface. With the protector in place, the blank may be light weighted by grinding a non-optical surface of the blank using computer controlled grinding. The light weighting may include creating a structure having a substantially minimum mass necessary to maintain distortion of the mirror within a preset limit. A damaged layer of the non-optical surface caused by light weighting may be removed with an isotropic etch and/or repaired by heat treatment. If an oxide layer is present, the entire blank may then be etched using, for example, hydrofluoric acid. A reflecting coating may be deposited on the optical surface.Type: GrantFiled: August 31, 2011Date of Patent: July 7, 2015Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Vincent T. Bly
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Patent number: 9074921Abstract: The invention proposed herein is a system and method for measuring the liquid level in a container that employs an optic fiber sensor which is heated using a simple power source and a wire and making an anemometry measurement. The heater wire is cycled between two levels of heat and the liquid level is obtained by measuring the heat transfer characteristics of the surrounding environment.Type: GrantFiled: January 3, 2013Date of Patent: July 7, 2015Assignee: The United States of America as Represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Allen R. Parker, Jr., W. Lance Richards, Anthony Piazza, Hon Chan Man, John A. Bakalyar
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Patent number: 9076658Abstract: A metal film liftoff process includes applying a polymer layer onto a silicon substrate, applying a germanium layer over the polymer layer to create a bilayer lift off mask, applying a patterned photoresist layer over the germanium layer, removing an exposed portion of the germanium layer, removing the photoresist layer and a portion of the polymer layer to expose a portion of the substrate and create an overhanging structure of the germanium layer, depositing a metal film over the exposed portion of the substrate and the germanium layer, and removing the polymer and germanium layers along with the overlaying metal film.Type: GrantFiled: September 25, 2014Date of Patent: July 7, 2015Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Ari D. Brown, Amil A. Patel
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Patent number: 9067325Abstract: A grasp assist system includes a glove and a flexible sleeve. The glove includes a digit such as a finger or thumb, a force sensor configured to measure a grasping force applied to an object by an operator wearing the glove, and adjustable phalange rings positioned with respect to the digit. A saddle is positioned with respect to the finger. A flexible tendon is looped at one end around the saddle. A conduit contains the tendon. A conduit anchor secured within a palm of the glove receives the conduit. The sleeve has pockets containing an actuator assembly connected to another end of the tendon and a controller. The controller is in communication with the force sensor, and calculates a tensile force in response to the measured grasping force. The controller commands the tensile force from the actuator assembly to tension the tendon and thereby move the finger.Type: GrantFiled: February 29, 2012Date of Patent: June 30, 2015Assignees: GM Global Technology Operations LLC, The United States of America As Represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Chris A. Ihrke, Donald R. Davis, Douglas Martin Linn, Bryan Bergelin, Lyndon B. J. Bridgwater, Heather Bibby, Judy Schroeder, Craig Erkkila
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Patent number: 9067319Abstract: A system includes a controller and a serial robot having links that are interconnected by a joint, wherein the robot can grasp a three-dimensional (3D) object in response to a commanded grasp pose. The controller receives input information, including the commanded grasp pose, a first set of information describing the kinematics of the robot, and a second set of information describing the position of the object to be grasped. The controller also calculates, in a two-dimensional (2D) plane, a set of contact points between the serial robot and a surface of the 3D object needed for the serial robot to achieve the commanded grasp pose. A required joint angle is then calculated in the 2D plane between the pair of links using the set of contact points. A control action is then executed with respect to the motion of the serial robot using the required joint angle.Type: GrantFiled: August 11, 2011Date of Patent: June 30, 2015Assignees: GM Global Technology Operations LLC, The United States of America as represented by the Administrator of the National Aeronautics and Space Administrator, Oceaneering Space SystemsInventors: Jianying Shi, Brian Hargrave, Myron A Diftler
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Patent number: 9062712Abstract: Systems and methods for passive thermal management of foil bearing systems are disclosed herein. The flow of the hydrodynamic film across the surface of bearing compliant foils may be disrupted to provide passive cooling and to improve the performance and reliability of the foil bearing system.Type: GrantFiled: February 20, 2013Date of Patent: June 23, 2015Assignee: The United States of America as Represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Robert J. Bruckner
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Patent number: 9065242Abstract: An apparatus and method is provided to enable precision and fast laser frequency tuning. For instance, a fast tunable slave laser may be dynamically offset-locked to a reference laser line using an optical phase-locked loop. The slave laser is heterodyned against a reference laser line to generate a beatnote that is subsequently frequency divided. The phase difference between the divided beatnote and a reference signal may be detected to generate an error signal proportional to the phase difference. The error signal is converted into appropriate feedback signals to phase lock the divided beatnote to the reference signal. The slave laser frequency target may be rapidly changed based on a combination of a dynamically changing frequency of the reference signal, the frequency dividing factor, and an effective polarity of the error signal. Feed-forward signals may be generated to accelerate the slave laser frequency switching through laser tuning ports.Type: GrantFiled: May 17, 2012Date of Patent: June 23, 2015Assignee: The United States of America as represented by the Administrator of the National Aeronautics Space AdministrationInventors: Jeffrey R. Chen, Kenji Numata, Stewart T. Wu, Guangning Yang
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Patent number: 9066028Abstract: Methods and systems for converting an image contrast evolution of an object to a temperature contrast evolution and vice versa are disclosed, including methods for assessing an emissivity of the object; calculating an afterglow heat flux evolution; calculating a measurement region of interest temperature change; calculating a reference region of interest temperature change; calculating a reflection temperature change; calculating the image contrast evolution or the temperature contrast evolution; and converting the image contrast evolution to the temperature contrast evolution or vice versa, respectively.Type: GrantFiled: December 17, 2010Date of Patent: June 23, 2015Assignee: The United States of America as represented by the Administator of the National Aeronautics and Space AdministrationInventor: Ajay M. Koshti
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Patent number: 9052236Abstract: The present invention comprises an approach for calibrating the sensitivity to polarization, optics degradation, spectral and stray light response functions of instruments on orbit. The concept is based on using an accurate ground-based laser system, Ground-to-Space Laser Calibration (GSLC), transmitting laser light to instrument on orbit during nighttime substantially clear-sky conditions. To minimize atmospheric contribution to the calibration uncertainty the calibration cycles should be performed in short time intervals, and all required measurements are designed to be relative. The calibration cycles involve ground operations with laser beam polarization and wavelength changes.Type: GrantFiled: June 30, 2014Date of Patent: June 9, 2015Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Constantine Lukashin, Bruce A. Wielicki