Patents Assigned to Space Adminstration
  • Patent number: 11725079
    Abstract: Compositions including a polyimide and one or more thermally conductive fillers, and compaction rollers for an automated fiber placement machine incorporating the compositions are provided. The polyimide may be a polymeric reaction product of a dianhydride and one or more diamines. The one or more diamines may include a fluorine-containing alkyl ether diamine. The one or more thermally conductive fillers may include one or more of a carbon-based filler, boron nitride, a metal, or combinations thereof. The compositions may have a thermal conductivity of from about 0.2 to about 50 Watts per meter Kelvin (Wm?1 K?1).
    Type: Grant
    Filed: July 15, 2021
    Date of Patent: August 15, 2023
    Assignees: THE BOEING COMPANY, United States Government, as Represented by the Administrator of the of the National Aeronautics and Space Adminstration
    Inventors: Sayata Ghose, Marcus Anthony Belcher, John W. Connell
  • Patent number: 10819454
    Abstract: Vortex radiometers (VRs) for cognitive antenna applications and fade prediction techniques are disclosed. A VR may act as an early warning system for communication antennas by of measuring: (1) when a fade causing interference with or complete loss of communication signal will occur; (2) how long the fade will persist; and/or (3) how intense the fade will be. This may be accomplished by measuring atmospheric noise temperature with concentric annular antenna beam patterns.
    Type: Grant
    Filed: November 27, 2019
    Date of Patent: October 27, 2020
    Assignee: United States of America as Represented by the Adminstrator of National Aeronautics and Space Adminstration
    Inventor: Peter J. Schemmel
  • Patent number: 10451156
    Abstract: A robust ground traction (drive) assembly for remotely controlled vehicles, which not only operates smoothly on surfaces that are flat, but also upon surfaces that include rugged terrain, snow, mud, and sand, is provided. The assembly includes a sun gear and a braking gear. The sun gear is configured to cause rotational force to be applied to second planetary gears through a coupling of first planetary gears. The braking gear is configured to cause the assembly (or the second planetary gears) to rotate around the braking gear when an obstacle or braking force is applied.
    Type: Grant
    Filed: May 26, 2017
    Date of Patent: October 22, 2019
    Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space Adminstration
    Inventors: Michael J. Krasowski, Lawrence C. Greer
  • Patent number: 10422706
    Abstract: The present invention is a temperature sensor for cryogenic systems using a fiber optic interrogation system that is capable of a large number of temperature readings across the cryogenic environment at high resolutions. The invention also includes a method of using such a system to measure temperatures in a cryogenic environment and a method of making such a system.
    Type: Grant
    Filed: June 28, 2018
    Date of Patent: September 24, 2019
    Assignee: United States of America as Represented by the Adminstrator of the National Aeronautics and Space Adminstration
    Inventors: Allen R. Parker, Jr., Anthony Piazza, Hon Man Chan, Ryan M Warner
  • Patent number: 9465965
    Abstract: A system for radio frequency identification (RFID) includes an enclosure defining an interior region interior to the enclosure, and a feed for generating an electromagnetic field in the interior region in response to a signal received from an RFID reader via a radio frequency (RF) transmission line and, in response to the electromagnetic field, receiving a signal from an RFID sensor attached to an item in the interior region. The structure of the enclosure may be conductive and may include a metamaterial portion, an electromagnetically absorbing portion, or a wall extending in the interior region. Related apparatuses and methods for performing RFID are provided.
    Type: Grant
    Filed: February 19, 2014
    Date of Patent: October 11, 2016
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Adminstration
    Inventors: Patrick W. Fink, Andrew W. Chu, Gregory Y. Lin, Timothy F. Kennedy, Phong H. Ngo, Dewey T. Brown, Diane Byerly
  • Patent number: 9354134
    Abstract: An In-Situ Load System for calibrating and validating aerodynamic properties of scaled aircraft in ground-based aerospace testing applications includes an assembly having upper and lower components that are pivotably interconnected. A test weight can be connected to the lower component to apply a known force to a force balance. The orientation of the force balance can be varied, and the measured forces from the force balance can be compared to applied loads at various orientations to thereby develop calibration factors.
    Type: Grant
    Filed: February 27, 2014
    Date of Patent: May 31, 2016
    Assignee: THE UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINSTRATION
    Inventors: Sean A. Commo, Keith C. Lynn, Drew Landman, Michael J. Acheson
  • Patent number: 9151639
    Abstract: A two-dimensional inductive position sensing system uses four drive inductors arranged at the vertices of a parallelogram and a sensing inductor positioned within the parallelogram. The sensing inductor is movable within the parallelogram and relative to the drive inductors. A first oscillating current at a first frequency is supplied to a first pair of the drive inductors located at ends of a first diagonal of the parallelogram. A second oscillating current at a second frequency is supplied to a second pair of the drive inductors located at ends of a second diagonal of the parallelogram. As a result, the sensing inductor generates a first output voltage at the first frequency and a second output voltage at the second frequency. A processor determines a position of the sensing inductor relative to the drive inductors using the first output voltage and the second output voltage.
    Type: Grant
    Filed: February 10, 2014
    Date of Patent: October 6, 2015
    Assignee: The United States of America as Represented by the Administrator of the National Aeronautics and Space Adminstration
    Inventors: Robert C. Youngquist, Stanley O. Starr
  • Patent number: 9067794
    Abstract: Disclosed are methods for forming carbon-based fillers as may be utilized in forming highly thermal conductive nanocomposite materials. Formation methods include treatment of an expanded graphite with an alcohol/water mixture followed by further exfoliation of the graphite to form extremely thin carbon nanosheets that are on the order of between about 2 and about 10 nanometers in thickness. Disclosed carbon nanosheets can be functionalized and/or can be incorporated in nanocomposites with extremely high thermal conductivities. Disclosed methods and materials can prove highly valuable in many technological applications including, for instance, in formation of heat management materials for protective clothing and as may be useful in space exploration or in others that require efficient yet light-weight and flexible thermal management solutions.
    Type: Grant
    Filed: August 5, 2009
    Date of Patent: June 30, 2015
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Adminstration
    Inventors: Ya-Ping Sun, John W. Connell, Lucia Monica Veca
  • Publication number: 20150134202
    Abstract: A method of controlling steering of a vehicle through setting wheel angles of a plurality of modular electronic corner assemblies (eModules) is provided. The method includes receiving a driving mode selected from a mode selection menu. A position of a steering input device is determined in a master controller. A velocity of the vehicle is determined, in the master controller, when the determined position of the steering input device is near center. A drive mode request corresponding to the selected driving mode to the plurality of steering controllers is transmitted to the master controller. A required steering angle of each of the plurality of eModules is determined, in the master controller, as a function of the determined position of the steering input device, the determined velocity of the vehicle, and the selected first driving mode. The eModules are set to the respective determined steering angles.
    Type: Application
    Filed: November 8, 2013
    Publication date: May 14, 2015
    Applicants: The U.S.A. As Represented by the Administrator of the National Aeronautics and Space Adminstration, GM GLOBAL TECHNOLOGY OPERATIONS LLC
    Inventors: Andrew D. Dawson, William J. Bluethmann, Chunhao J. Lee, Robert L. Vitale, Raymond Guo, Venkata Prasad Atluri
  • Patent number: 8935107
    Abstract: A compact shock sensing system and method that employ a light sheet generator that can be used either as a solo aerodynamic shock detector or in a combination with a scanning mode shock sensor is disclosed. This shock sensing system and method can be used to detect and track unstable and travelling shocks in high speed aerodynamic flows, such as those found in supersonic inlets.
    Type: Grant
    Filed: February 18, 2011
    Date of Patent: January 13, 2015
    Assignee: The United States of America as Represented by the Adminstrator of National Aeronautics and Space Adminstration
    Inventors: Grigory Adamovsky, Roger P Tokars
  • Patent number: 8909491
    Abstract: Provided is a method for measuring multi-point interferometric angle changes beginning with an interferometric device capable of measuring at least one main point and at least one reference point. The method includes recording interferometric intensity changes on two or more spots using the main point and the reference point, and determining a sequence having a plurality of peak, local maximas and a plurality of valley, local minimas. The method includes sampling a first, partial sequence and comparing it to a neighboring, partial sequence using a perturbation analysis and additional calculation(s) to compile all phase angle changes for all measured points. Also provided is a computer implemented method to enable nanometer resolution sensitivity in a noisy signal and for characterization of a material in an interferometric device.
    Type: Grant
    Filed: March 5, 2012
    Date of Patent: December 9, 2014
    Assignee: The United States of America as represented by the Adminstrator of the National Aeronautics and Space Adminstration
    Inventors: Yeonjoon Park, Sang Hyouk Choi
  • Patent number: 8875580
    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: Grant
    Filed: December 13, 2011
    Date of Patent: November 4, 2014
    Assignee: The United States of America as represented by the Adminstrator of the National Aeronautics and Space Adminstration
    Inventors: William T. Yost, Karl Elliott Cramer, Daniel F. Perey
  • Patent number: 8266866
    Abstract: A method of assembling an inflatable shell of a structure comprises folding a plurality of shell sections about a set of fold lines and integrating the plurality of shell sections together with one another to form the shell. In another embodiment, an inflatable shell comprises a plurality of shell sections, each shell section having two pairs of fold lines for folding into stowage comprising a first gore section having a plurality of first gore panels layered and collectively folded about at a first set of fold lines. Each layer of the first gore panels and second gore panels are configured such that, once the first gore panel and second gore panel are attached to one another at the respective side edges of each panel, the lines of attachment forming a second set of fold lines for the shell section. A system and method for fabricating gore panels is also disclosed.
    Type: Grant
    Filed: January 9, 2012
    Date of Patent: September 18, 2012
    Assignee: The United States of America as respresented by the Administrator of the National Aeronautics and Space Adminstration
    Inventor: Christopher J. Johnson
  • Patent number: 8170234
    Abstract: Mapping coherent/incoherent acoustic sources as determined from a phased microphone array. A linear configuration of equations and unknowns are formed by accounting for a reciprocal influence of one or more cross-beamforming characteristics thereof at varying grid locations among the plurality of grid locations. An equation derived from the linear configuration of equations and unknowns can then be iteratively determined. The equation can be attained by the solution requirement of a constraint equivalent to the physical assumption that the coherent sources have only in phase coherence. The size of the problem may then be reduced using zoning methods.
    Type: Grant
    Filed: April 24, 2008
    Date of Patent: May 1, 2012
    Assignee: The United States of America by the Administrator of the National Aeronautics and Space Adminstration
    Inventors: Thomas F. Brooks, William M. Humphreys, Jr.
  • Patent number: 8163243
    Abstract: The system that operates in a zero gravity environment and has an integral ozone generating capability is disclosed. The system contributes to the control of metabolic water vapors in the air, and also provided disinfection of any resulting condensate within the system, as well as disinfection of the air stream that flows throughout the disclosed system.
    Type: Grant
    Filed: September 7, 2006
    Date of Patent: April 24, 2012
    Assignee: The United States of America as represented by the Administrator of National Aeronautics and Space Adminstration
    Inventor: Kenneth A. Burke
  • Patent number: 7890311
    Abstract: The flow-through area of a pressure regulator positioned in a branch of a simulated fluid flow network is generated. A target pressure is defined downstream of the pressure regulator. A projected flow-through area is generated as a non-linear function of (i) target pressure, (ii) flow-through area of the pressure regulator for a current time step and a previous time step, and (iii) pressure at the downstream location for the current time step and previous time step. A simulated flow-through area for the next time step is generated as a sum of (i) flow-through area for the current time step, and (ii) a difference between the projected flow-through area and the flow-through area for the current time step multiplied by a user-defined rate control parameter. These steps are repeated for a sequence of time steps until the pressure at the downstream location is approximately equal to the target pressure.
    Type: Grant
    Filed: July 7, 2005
    Date of Patent: February 15, 2011
    Assignee: United States of America as represented by the Administrator of the National Aeronautics and Space Adminstration
    Inventors: Neal E. Hass, Paul A. Schallhorn
  • Publication number: 20090277789
    Abstract: A wireless chemical sensor includes an electrical conductor and a dielectric material on the conductor. The conductor is electrically unconnected and is shaped for storage of an electric field and a magnetic field. In the presence of a time-varying magnetic field, the conductor resonates to generate harmonic electric and magnetic field responses, each of which has a frequency associated therewith. The dielectric material is selected such that it experiences changes in dielectric attributes thereof in the presence of a chemical-of-interest. Shifts from the sensor's baseline frequency response indicate that the dielectric material has been exposed to the chemical-of-interest.
    Type: Application
    Filed: May 11, 2009
    Publication date: November 12, 2009
    Applicants: Space Adminstration
    Inventors: Stanley E. Woodard, M. Oglesby Donald, Bryant Douglas Taylor, Qamar A. Shams
  • Publication number: 20090185942
    Abstract: A novel method to prepare an advanced thermoelectric material has hierarchical structures embedded with nanometer-sized voids which are key to enhancement of the thermoelectric performance. Solution-based thin film deposition technique enables preparation of stable film of thermoelectric material and void generator (voigen). A subsequent thermal process creates hierarchical nanovoid structure inside the thermoelectric material. Potential application areas of this advanced thermoelectric material with nanovoid structure are commercial applications (electronics cooling), medical and scientific applications (biological analysis device, medical imaging systems), telecommunications, and defense and military applications (night vision equipments).
    Type: Application
    Filed: December 4, 2008
    Publication date: July 23, 2009
    Applicants: National Institute of Aerospace Associates, Space Adminstration
    Inventors: Sang Hyouk Choi, SR., Yeonjoon Park, Sang-Hyon Chu, James R. Elliott, Glen C. King, Jae-Woo Kim, Peter T. Lillehei, Diane M. Stoakley
  • Patent number: 7507472
    Abstract: An electroactive material comprises multiple layers of electroactive composite with each layer having unique dielectric, electrical and mechanical properties that define an electromechanical operation thereof when affected by an external stimulus. For example, each layer can be (i) a 2-phase composite made from a polymer with polarizable moieties and an effective amount of carbon nanotubes incorporated in the polymer for a predetermined electomechanical operation, or (ii) a 3-phase composite having the elements of the 2-phase composite and further including a third component of micro-sized to nano-sized particles of an electroactive ceramic incorporated in the polymer matrix.
    Type: Grant
    Filed: March 9, 2005
    Date of Patent: March 24, 2009
    Assignee: The United States of America as represented by the Administator of National Aeronatics and Space Adminstration
    Inventors: Zoubeida Ounaies, Cheol Park, Joycelyn S. Harrison, Nancy M. Holloway, Gregory K. Draughon
  • Patent number: 7504921
    Abstract: An actuator for moving a load has a frame forming a race between two surfaces thereof, at least two elements joined together by at least one flexible member, the elements and the at least one flexible member being disposed between the two surfaces of the frame that forms a race, one of the elements further joined to the load by a portion of the at least one flexible member, wherein when an element comes into contact with a surface of the frame it will stick thereto absent a repelling force, and moving means disposed to selectively attract or repel a corresponding element towards or away from one or the other of the two surfaces of the frame that forms the race. The actuator effects movement of the load in a direction towards or away from the elements, by changing a position of at least one of the elements on a surface of the frame that forms the race.
    Type: Grant
    Filed: September 29, 2006
    Date of Patent: March 17, 2009
    Assignee: United States of America as represented by the Administrator of the National Aeronautics and Space Adminstration
    Inventor: John M. Vranish