Patents Assigned to and Space Administration
  • Patent number: 8484274
    Abstract: Padding or adding data to a data signal can increase the speed with which a signal processor can process the data. Methods are provided herein that can accurately predict the optimal pad size of a two dimensional array of data, which can be used to increase the processing speed of a signal processor by optimizing run-time for a two-dimensional (2-D) fast Fourier transform (FFT) operation.
    Type: Grant
    Filed: August 27, 2009
    Date of Patent: July 9, 2013
    Assignee: The United States of America represented by the Administrator of the National Aeronautics Space Administration
    Inventors: Bruce H. Dean, David L. Aronstein, Jeffrey S. Smith
  • Patent number: 8483882
    Abstract: A robotic system includes a robot having manipulators for grasping an object using one of a plurality of grasp types during a primary task, and a controller. The controller controls the manipulators during the primary task using a multiple-task control hierarchy, and automatically parameterizes the internal forces of the system for each grasp type in response to an input signal. The primary task is defined at an object-level of control, e.g., using a closed-chain transformation, such that only select degrees of freedom are commanded for the object. A control system for the robotic system has a host machine and algorithm for controlling the manipulators using the above hierarchy. A method for controlling the system includes receiving and processing the input signal using the host machine, including defining the primary task at the object-level of control, e.g., using a closed-chain definition, and parameterizing the internal forces for each of grasp type.
    Type: Grant
    Filed: January 13, 2010
    Date of Patent: July 9, 2013
    Assignees: GM Global Technology Operations LLC, The United States of America as Represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Muhammad E. Abdallah, Robert Platt, Charles W. Wampler, II
  • Patent number: 8480296
    Abstract: A low temperature radiometer includes a main body, a main cavity, an exit cavity, a suspended thermometer, and an attached thermometer. The main cavity is disposed within the main body and is defined through an off-axis parabolic concentrating cone formed of the inner walls of the main body. The exit cavity is disposed within the main body and is defined through a cylindrical inner surface of the main body. The suspended thermometer is suspended within the exit cavity and is disposed to be in communication with radiation entering the main cavity and being diverted to the exit cavity. The attached thermometer is attached to the outer surface of the main body and is in thermal communication and contact with the main body.
    Type: Grant
    Filed: September 16, 2009
    Date of Patent: July 9, 2013
    Assignee: United States of America as represented by the Administrator of the National Aeronautics Space Administration
    Inventors: Michael DiPirro, Thomas P. Hait, James G. Tuttle
  • Patent number: 8476979
    Abstract: One or more embodiments of the present invention pertain to an all solid-state microwave power module. The module includes a plurality of solid-state amplifiers configured to amplify a signal using a low power stage, a medium power stage, and a high power stage. The module also includes a power conditioner configured to activate a voltage sequencer (e.g., bias controller) when power is received from a power source. The voltage sequencer is configured to sequentially apply voltage to a gate of each amplifier and sequentially apply voltage to a drain of each amplifier.
    Type: Grant
    Filed: July 7, 2011
    Date of Patent: July 2, 2013
    Assignee: The United States of America as Represented by the Administrator of National Aeronautics and Space Administration
    Inventors: Rainee N Simons, Edwin G Wintucky
  • Patent number: 8468794
    Abstract: An electric propulsion machine includes an ion thruster having an annular discharge chamber housing an anode having a large surface area. The ion thruster includes flat annular ion optics with a small span to gap ratio. Optionally, a second electric propulsion thruster may be disposed in a cylindrical space disposed within an interior of the annulus.
    Type: Grant
    Filed: September 30, 2010
    Date of Patent: June 25, 2013
    Assignee: The United States of America as Represented by the Administrator of National Aeronautics and Space Administration
    Inventor: Michael J. Patterson
  • Patent number: 8473663
    Abstract: A stackable form-factor Peripheral Component Interconnect (PCI) device can be configured as a host controller or a master/target for use on a PCI assembly. PCI device may comprise a multiple-input switch coupled to a PCI bus, a multiplexor coupled to the switch, and a reconfigurable device coupled to one of the switch and multiplexor. The PCI device is configured to support functionality from power-up, and either control function or add-in card function.
    Type: Grant
    Filed: January 21, 2011
    Date of Patent: June 25, 2013
    Assignee: United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Kevin M. Somervill, Tak-kwong Ng, Wilfredo Torres-Pomales, Mahyar R. Malekpour
  • Publication number: 20130157079
    Abstract: A first material with a known maximum temperature of operation is coated with a second material on at Least one surface of the first material. The coating has a melting temperature that is greater than the maximum temperature of operation of the first material. The coating is heated to its melting temperature until the coating flows into any cracks in the first material's surface.
    Type: Application
    Filed: December 19, 2012
    Publication date: June 20, 2013
    Applicant: U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
  • Publication number: 20130152727
    Abstract: A touchdown bearing system is provided to safely spin down a magnetically suspended flywheel rotor from full speed when the magnetic suspension system fails. In one embodiment, a plurality of touchdown wheels are mounted on a rigid support ring in a planetary arrangement.
    Type: Application
    Filed: December 14, 2012
    Publication date: June 20, 2013
    Applicant: U.S.A., as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: U.S.A., as represented by the Administrator of the National Aeronautics and Space Administration
  • Patent number: 8466776
    Abstract: A passive wireless tag assembly comprises a plurality of antennas and transmission lines interconnected with circuitry and constructed and arranged in a Van Atta array or configuration to reflect an interrogator signal in the direction from where it came. The circuitry may comprise at least one surface acoustic wave (SAW)-based circuit that functions as a signal reflector and is operatively connected with an information circuit. In another embodiment, at least one delay circuit and/or at least one passive modulation circuit(s) are utilized. In yet another embodiment, antennas connected to SAW-based devices are mounted to at least one of the orthogonal surfaces of a corner reflector.
    Type: Grant
    Filed: July 1, 2010
    Date of Patent: June 18, 2013
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Patrick W. Fink, Timothy F. Kennedy, Gregory Y. Lin
  • Patent number: 8467903
    Abstract: A humanoid robot includes a robotic hand having at least one finger. An actuation system for the robotic finger includes an actuator assembly which is supported by the robot and is spaced apart from the finger. A tendon extends from the actuator assembly to the at least one finger and ends in a tendon terminator. The actuator assembly is operable to actuate the tendon to move the tendon terminator and, thus, the finger.
    Type: Grant
    Filed: September 22, 2009
    Date of Patent: June 18, 2013
    Assignees: GM Global Technology Operations LLC, The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Chris A. Ihrke, David M. Reich, Lyndon Bridgwater, Douglas Martin Linn, Scott R. Askew, Myron A. Diftler, Robert Platt, Brian Hargrave, Michael C. Valvo, Muhammad E. Abdallah, Frank Noble Permenter, Joshua S. Mehling
  • Patent number: 8464750
    Abstract: A magnetostrictive pressure regulating system includes a magnetostrictive valve that incorporates a magnetostrictive actuator with at least one current-carrying coil disposed thereabout. A pressure force sensor, in fluid communication with the fluid exiting the valve, includes (i) a magnetostrictive material, (ii) a magnetic field generator in proximity to the magnetostrictive material for inducing a magnetic field in and surrounding the magnetostrictive material wherein lines of magnetic flux passing through the magnetostrictive material are defined, and (iii) a sensor positioned adjacent to the magnetostrictive material and in the magnetic field for measuring changes in at least one of flux angle and flux density when the magnetostrictive material experiences an applied force that is aligned with the lines of magnetic flux. The pressure of the fluid exiting the valve causes the applied force.
    Type: Grant
    Filed: June 30, 2010
    Date of Patent: June 18, 2013
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: James A. Richard, Herman L. Pickens
  • Publication number: 20130145849
    Abstract: A method and apparatus for evaluating and/or quantifying damage to wire strands of a wire caused during installation of a crimped wire connector, involves launching an ultrasonic wave having known characteristics into a wire at a location that is either the crimp or is adjacent the crimped wire connector, and detecting changes in the characteristics (e.g., amplitude and/or phase shift) of the wave as it is propagates along a length of the wire.
    Type: Application
    Filed: December 13, 2011
    Publication date: June 13, 2013
    Applicant: U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: William T. Yost, Karl Elliott Cramer, Daniel F. Perey
  • Publication number: 20130146905
    Abstract: The present invention provides an electronic apparatus, such as a lighting device comprised of light emitting diodes (LEDs) or a power generating apparatus comprising photovoltaic diodes, which may be created through a printing process, using a semiconductor or other substrate particle ink or suspension and using a lens particle ink or suspension. An exemplary apparatus comprises a base; at least one first conductor; a plurality of substantially spherical or optically resonant diodes coupled to the at least one first conductor; at least one second conductor coupled to the plurality of diodes; and a plurality of substantially spherical lenses suspended in a polymer attached or deposited over the diodes. The lenses and the suspending polymer have different indices of refraction. In some embodiments, the lenses and diodes have a ratio of mean diameters or lengths between about 10:1 and 2:1.
    Type: Application
    Filed: February 9, 2013
    Publication date: June 13, 2013
    Applicants: NTHDEGREE TECHNOLOGIES WORLDWIDE INC., Space Administration
    Inventors: NthDegree Technologies Worldwide Inc., U.S. Government as represented by the Administrator of the National Aeronautics and Space Administration
  • Patent number: 8456393
    Abstract: The present invention provides a method of manufacturing an electronic apparatus, such as a lighting device having light emitting diodes (LEDs) or a power generating device having photovoltaic diodes. The exemplary method includes forming at least one first conductor coupled to a base; coupling a plurality of substrate particles to the at least one first conductor; converting the plurality of substrate particles into a plurality of diodes; forming at least one second conductor coupled to the plurality of spherical diodes; and depositing or attaching a plurality of substantially spherical lenses suspended in a first polymer, with the lenses and the suspending polymer having different indices of refraction. In some embodiments, the lenses and diodes have a ratio of mean diameters or lengths between about 10:1 and 2:1. In various embodiments, the forming, coupling and converting steps are performed by or through a printing process.
    Type: Grant
    Filed: September 15, 2009
    Date of Patent: June 4, 2013
    Assignees: NthDegree Technologies Worldwide Inc, The United States of America as represented by the United States National Aeronautics and Space Administration
    Inventors: William Johnstone Ray, Mark D. Lowenthal, Neil O. Shotton, Richard A. Blanchard, Mark Allan Lewandowski, Kirk A. Fuller, Donald Odell Frazier
  • Patent number: 8456392
    Abstract: The present invention provides a method of manufacturing an electronic apparatus, such as a lighting device having light emitting diodes (LEDs) or a power generating device having photovoltaic diodes. The exemplary method includes forming at least one first conductor coupled to a base; coupling a plurality of substantially spherical substrate particles to the at least one first conductor; converting the substrate particles into a plurality of substantially spherical diodes; forming at least one second conductor coupled to the substantially spherical diodes; and depositing or attaching a plurality of substantially spherical lenses suspended in a first polymer. The lenses and the suspending polymer have different indices of refraction. In some embodiments, the lenses and diodes have a ratio of mean diameters or lengths between about 10:1 and 2:1. In various embodiments, the forming, coupling and converting steps are performed by or through a printing process.
    Type: Grant
    Filed: September 15, 2009
    Date of Patent: June 4, 2013
    Assignees: NthDegree Technologies Worldwide Inc, The United States of America as represented by the National Aeronautics and Space Administration
    Inventors: William Johnstone Ray, Mark D. Lowenthal, Neil O. Shotton, Richard A. Blanchard, Mark Allan Lewandowski, Kirk A. Fuller, Donald Odell Frazier
  • Patent number: 8455926
    Abstract: Systems, methods and apparatus are provided through which in some embodiments a mass spectrometer micro-leak includes a number of channels fabricated by semiconductor processing tools and that includes a number of inlet holes that provide access to the channels.
    Type: Grant
    Filed: September 23, 2010
    Date of Patent: June 4, 2013
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Dan N. Harpold, Hasso B. Niemann, Brian G. Jamieson, Bernard A. Lynch
  • Publication number: 20130134438
    Abstract: The present invention provides an electronic apparatus, such as a lighting device comprised of light emitting diodes (LEDs) or a power generating apparatus comprising photovoltaic diodes, which may be created through a printing process, using a semiconductor or other substrate particle ink or suspension and using a lens particle ink or suspension. An exemplary apparatus comprises a base; at least one first conductor; a plurality of diodes coupled to the at least one first conductor; at least one second conductor coupled to the plurality of diodes; and a plurality of lenses suspended in a polymer deposited or attached over the diodes. The lenses and the suspending polymer have different indices of refraction. In some embodiments, the lenses and diodes are substantially spherical, and have a ratio of mean diameters or lengths between about 10:1 and 2:1. The diodes may be LEDs or photovoltaic diodes, and in some embodiments, have a junction formed at least partially as a hemispherical shell or cap.
    Type: Application
    Filed: January 21, 2013
    Publication date: May 30, 2013
    Applicants: U.S. Gov. as represented by the Administrator of the National Aeronautics and Space Administration, NTHDEGREE TECHNOLOGIES WORLDWIDE INC.
    Inventors: NthDegree Technologies Worldwide Inc., U.S. Government as represented by the Administrator of the National Aeronautics and Space Administration
  • Patent number: 8448498
    Abstract: The present invention is a hermetic seal leak detection apparatus, which can be used to test for hermetic seal leaks in instruments and containers. A vacuum tight chamber is created around the unit being tested to minimize gas space outside of the hermetic seal. A vacuum inducing device is then used to increase the gas chamber volume inside the device, so that a slight vacuum is pulled on the unit being tested. The pressure in the unit being tested will stabilize. If the stabilized pressure reads close to a known good seal calibration, there is not a leak in the seal. If the stabilized pressure reads closer to a known bad seal calibration value, there is a leak in the seal. The speed of the plunger can be varied and by evaluating the resulting pressure change rates and final values, the leak rate/size can be accurately calculated.
    Type: Grant
    Filed: August 27, 2010
    Date of Patent: May 28, 2013
    Assignee: United States of America as Represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Anthony R. Kelley
  • Patent number: 8452073
    Abstract: A closed-loop control method for an electron beam freeform fabrication (EBF3) process includes detecting a feature of interest during the process using a sensor(s), continuously evaluating the feature of interest to determine, in real time, a change occurring therein, and automatically modifying control parameters to control the EBF3 process. An apparatus provides closed-loop control method of the process, and includes an electron gun for generating an electron beam, a wire feeder for feeding a wire toward a substrate, wherein the wire is melted and progressively deposited in layers onto the substrate, a sensor(s), and a host machine. The sensor(s) measure the feature of interest during the process, and the host machine continuously evaluates the feature of interest to determine, in real time, a change occurring therein. The host machine automatically modifies control parameters to the EBF3 apparatus to control the EBF3 process in a closed-loop manner.
    Type: Grant
    Filed: March 31, 2010
    Date of Patent: May 28, 2013
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Karen M. Taminger, Robert A. Hafley, Richard E. Martin, William H. Hofmeister
  • Patent number: 8447443
    Abstract: A computerized system and method for peak-seeking-control that uses a unique Kalman filter design to optimize a control loop, in real time, to either maximize or minimize a performance function of a physical object (“plant”). The system and method achieves more accurate and efficient peak-seeking-control by using a time-varying Kalman filter to estimate both the performance function gradient (slope) and Hessian (curvature) based on direct position measurements of the plant, and does not rely upon modeling the plant response to persistent excitation. The system and method can be naturally applied in various applications in which plant performance functions have multiple independent parameters, and it does not depend upon frequency separation to distinguish between system dimensions.
    Type: Grant
    Filed: February 7, 2012
    Date of Patent: May 21, 2013
    Assignees: The United States of America as Represented by the Administrator of the National Aeronautics and Space Administration, The Regents of the University of California
    Inventors: John J Ryan, Jason L Speyer