Patents Assigned to and Space Administration
  • Patent number: 8628238
    Abstract: A multi-purpose, cylindrical thermal insulation test apparatus is used for testing insulation materials and systems of materials using a liquid boil-off calorimeter system for absolute measurement of the effective thermal conductivity (k-value) and heat flux of a specimen material at a fixed environmental condition (cold-side temperature, warm-side temperature, vacuum pressure level, and residual gas composition). The apparatus includes an inner vessel for receiving a liquid with a normal boiling point below ambient temperature, such as liquid nitrogen, enclosed within a vacuum chamber. A cold mass assembly, including the upper and lower guard chambers and a middle test vessel, is suspended from a lid of the vacuum canister. Each of the three chambers is filled and vented through a single feedthrough. All fluid and instrumentation feedthroughs are mounted and suspended from a top domed lid to allow easy removal of the cold mass.
    Type: Grant
    Filed: June 11, 2010
    Date of Patent: January 14, 2014
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: James E. Fesmire, Adam G. Dokos
  • Publication number: 20140011145
    Abstract: A flame holder system includes a modified torch body and a ceramic flame holder. Catch pin(s) are coupled to and extend radially out from the torch body. The ceramic flame holder has groove(s) formed in its inner wall that correspond in number and positioning to the catch pin(s). Each groove starts at one end of the flame holder and is can be shaped to define at least two 90° elbows. Each groove is sized to receive one catch pin therein when the flame holder is fitted over the end of the torch body. The flame holder is then manipulated until the catch pin(s) butt up against the end of the groove(s).
    Type: Application
    Filed: September 9, 2013
    Publication date: January 9, 2014
    Applicant: U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Henry H. Haskin, Peter Vasquez
  • Patent number: 8623253
    Abstract: Provided are low-melt polyimides and poly(amic acids) (PAAs) for use in repair of electrical wire insulation, flat or ribbon wire harnesses, and flat surfaces comprised of high-performance polymers such as inflatables or solar panels applications. Also provided are methods and devices for repair of electrical insulation.
    Type: Grant
    Filed: February 23, 2011
    Date of Patent: January 7, 2014
    Assignee: The United States of America as Represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Scott T. Jolley, Tracy L. Gibson, Martha K. Williams, Clyde F. Parrish, Steven L. Parks
  • Patent number: 8618933
    Abstract: A monitoring system is disclosed, which includes a base station and at least one sensor unit that is separate from the base station. The at least one sensor unit resides in a dormant state until it is awakened by the triggering of a vibration-sensitive switch. Once awakened, the sensor may take a measurement, and then transmit to the base station the measurement. Once data is transmitted from the sensor to the base station, the sensor may return to its dormant state. There may be various sensors for each base station and the various sensors may optionally measure different quantities, such as current, voltage, single-axis and/or three-axis magnetic fields.
    Type: Grant
    Filed: October 2, 2007
    Date of Patent: December 31, 2013
    Assignee: The United States of America as Represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Scott L. Jensen, George J. Drouant
  • Patent number: 8618762
    Abstract: A tendon tensioning system includes a tendon having a proximal end and a distal end, an actuator, and a motor controller. The actuator may include a drive screw and a motor, and may be coupled with the proximal end of the tendon and configured to apply a tension through the tendon in response to an electrical current. The motor controller may be electrically coupled with the actuator, and configured to provide an electrical current having a first amplitude to the actuator until a stall tension is achieved through the tendon; provide a pulse current to the actuator following the achievement of the stall tension, where the amplitude of the pulse current is greater than the first amplitude, and return the motor to a steady state holding current following the conclusion of the pulse current.
    Type: Grant
    Filed: January 27, 2011
    Date of Patent: December 31, 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: Matthew J. Reiland, Myron A. Diftler
  • Patent number: 8609750
    Abstract: A clay-epoxy nanocomposite may be prepared by dispersing a layered clay in an alkoxy epoxy, such as a polypropylene oxide based epoxide before combining the mixture with an aromatic epoxy to improve the nanocomposite's thermal and mechanical properties.
    Type: Grant
    Filed: June 2, 2010
    Date of Patent: December 17, 2013
    Assignee: The United States of America as Represented by the Administrator of National Aeronautics and Space Administration
    Inventor: Sandi G Miller
  • Patent number: 8608993
    Abstract: A nanocomposite structure and method of fabricating same are provided. The nanocomposite structure is a polymer in an extruded shape with carbon nanotubes (CNTs) longitudinally disposed and dispersed in the extruded shape along a dimension thereof. The polymer is characteristically defined as having a viscosity of at least approximately 100,000 poise at a temperature of 200° C.
    Type: Grant
    Filed: March 22, 2011
    Date of Patent: December 17, 2013
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Dennis C. Working, Emilie J. Siochi, Cheol Park, Peter T. Lillehei
  • Patent number: 8605262
    Abstract: A continuous wave Light Detection and Ranging (CW LiDAR) system utilizes two or more laser frequencies and time or range shifted pseudorandom noise (PN) codes to discriminate between the laser frequencies. The performance of these codes can be improved by subtracting out the bias before processing. The CW LiDAR system may be mounted to an artificial satellite orbiting the earth, and the relative strength of the return signal for each frequency can be utilized to determine the concentration of selected gases or other substances in the atmosphere.
    Type: Grant
    Filed: June 23, 2011
    Date of Patent: December 10, 2013
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Joel F. Campbell, Narasimha S. Prasad, Fenton W. Harrison, Michael A. Flood
  • Patent number: 8603285
    Abstract: Disclosed herein is a method of making a mirror support comprising a composite, the composite comprising a plurality of carbon nanotubes, wherein at least two of the plurality of carbon nanotubes are bonded to each other through a bridging moiety bound to each of the two carbon nanotubes, and a laminate comprising the composite.
    Type: Grant
    Filed: March 5, 2010
    Date of Patent: December 10, 2013
    Assignee: The United States of America as Represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Richard L. Baron
  • Patent number: 8593153
    Abstract: A system and method for detecting damage in an electrical wire, including delivering at least one test electrical signal to an outer electrically conductive material in a continuous or non-continuous layer covering an electrically insulative material layer that covers an electrically conductive wire core. Detecting the test electrical signals in the outer conductive material layer to obtain data that is processed to identify damage in the outer electrically conductive material layer.
    Type: Grant
    Filed: July 26, 2010
    Date of Patent: November 26, 2013
    Assignee: The United States of America as Represented by the United States National Aeronautics and Space Administration
    Inventors: Pedro J. Medelius, Tracy L. Gibson, Mark E. Lewis
  • Patent number: 8580546
    Abstract: A method for fabricating a micro-organ device comprises providing a microscale support having one or more microfluidic channels and one or more micro-chambers for housing a micro-organ and printing a micro-organ on the microscale support using a cell suspension in a syringe controlled by a computer-aided tissue engineering system, wherein the cell suspension comprises cells suspended in a solution containing a material that functions as a three-dimensional scaffold. The printing is performed with the computer-aided tissue engineering system according to a particular pattern. The micro-organ device comprises at least one micro-chamber each housing a micro-organ; and at least one microfluidic channel connected to the micro-chamber, wherein the micro-organ comprises cells arranged in a configuration that includes microscale spacing between portions of the cells to facilitate diffusion exchange between the cells and a medium supplied from the at least one microfluidic channel.
    Type: Grant
    Filed: November 29, 2012
    Date of Patent: November 12, 2013
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Steve R. Gonda, Robert C. Chang, Binil Starly, Christopher Culbertson, Heidi L. Holtorf, Wei Sun, Julia Leslie
  • Patent number: 8577519
    Abstract: The present invention is a telemetry system, and more specifically is a rapidly deployed modular telemetry apparatus which utilizes of SDR technology and the FPGA programming capability to reduce the number of hardware components and programming required to deploy a telemetry system.
    Type: Grant
    Filed: March 20, 2012
    Date of Patent: November 5, 2013
    Assignee: The United States of America as Represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Kosta A. Varnavas, William Herbert Sims, III
  • Patent number: 8577639
    Abstract: A calibration assembly for a spectrometer is provided. The assembly includes a spectrometer having n detector elements, where each detector element is assigned a predetermined wavelength value. A first source emitting first radiation is used to calibrate the spectrometer. A device is placed in the path of the first radiation to split the first radiation into a first beam and a second beam. The assembly is configured so that one of the first and second beams travels a path-difference distance longer than the other of the first and second beams. An output signal is generated by the spectrometer when the first and second beams enter the spectrometer. The assembly includes a controller operable for processing the output signal and adapted to calculate correction factors for the respective predetermined wavelength values assigned to each detector element.
    Type: Grant
    Filed: February 19, 2011
    Date of Patent: November 5, 2013
    Assignee: The United States of America as Represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Robert C. Youngquist, Stephen M. Simmons
  • Patent number: 8577120
    Abstract: A method for characterizing an anomaly in a material comprises (a) extracting contrast data; (b) measuring a contrast evolution; (c) filtering the contrast evolution; (d) measuring a peak amplitude of the contrast evolution; (d) determining a diameter and a depth of the anomaly, and (e) repeating the step of determining the diameter and the depth of the anomaly until a change in the estimate of the depth is less than a set value. The step of determining the diameter and the depth of the anomaly comprises estimating the depth using a diameter constant CD equal to one for the first iteration of determining the diameter and the depth; estimating the diameter; and comparing the estimate of the depth of the anomaly after each iteration of estimating to the prior estimate of the depth to calculate the change in the estimate of the depth of the anomaly.
    Type: Grant
    Filed: October 8, 2010
    Date of Patent: November 5, 2013
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Ajay M. Koshti
  • Patent number: 8573835
    Abstract: A method and apparatus for the measurement of thermal conductivity combines the following capabilities: 1) measurements of very small specimens; 2) measurements of specimens with thermal conductivity on the same order of that as air; and, 3) the ability to use air as a reference material. Care is taken to ensure that the heat flow through the test specimen is essentially one-dimensional. No attempt is made to use heated guards to minimize the flow of heat from the hot plate to the surroundings. Results indicate that since large correction factors must be applied to account for guard imperfections when specimen dimensions are small, simply measuring and correcting for heat from the heater disc that does not flow into the specimen is preferable.
    Type: Grant
    Filed: June 8, 2012
    Date of Patent: November 5, 2013
    Assignee: The United States of America as Represented by the Administrator of National Aeronautics and Space Administration
    Inventors: Robert A Miller, Maria A Kuczmarski
  • Patent number: 8577504
    Abstract: Disclosed is a system for suppressing vibration and noise mitigation in structures such as blades in turbomachinery. The system includes flexible piezoelectric patches which are secured on or imbedded in turbomachinery blades which, in one embodiment, comprises eight (8) fan blades. The system further includes a capacitor plate coupler and a power transfer apparatus, which may both be arranged into one assembly, that respectively transfer data and power. Each of the capacitive plate coupler and power transfer apparatus is configured so that one part is attached to a fixed member while another part is attached to a rotatable member with an air gap therebetween. The system still further includes a processor that has 16 channels, eight of which serve as sensor channels, and the remaining eight, serving as actuation channels. The processor collects and analyzes the sensor signals and, in turn, outputs corrective signals for vibration/noise suppression of the turbine blades.
    Type: Grant
    Filed: November 24, 2010
    Date of Patent: November 5, 2013
    Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space Administration
    Inventors: Carlos R. Morrison, Andrew J. Provenza, Benjamin B. Choi, Milind A. Bakhle, James B Min, George L. Stefko, John A Kussmann, Alan J Fougere
  • Patent number: 8575577
    Abstract: Neutron optics based on the two-reflection geometries are capable of controlling beams of long wavelength neutrons with low angular divergence. The preferred mirror fabrication technique is a replication process with electroform nickel replication process being preferable. In the preliminary demonstration test an electroform nickel optics gave the neutron current density gain at the focal spot of the mirror at least 8 for neutron wavelengths in the range from 6 to 20 ?. The replication techniques can be also be used to fabricate neutron beam controlling guides.
    Type: Grant
    Filed: June 27, 2012
    Date of Patent: November 5, 2013
    Assignee: The United States of America as Represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Mikhail V. Gubarev, Brian D. Ramsey, Darell E. Engelhaupt
  • Publication number: 20130289945
    Abstract: Embodiments of the invention may provide the ability for infrastructure managers to readily assess current organizational space allocation, to determine overcrowded and/or underutilized facilities, to propose options for improving and/or optimizing space usage in a facility, and to visualize current and proposed utilization. Embodiments of the invention may also provide the ability to reduce operational costs by more efficiently utilizing available space. Embodiments of the invention may comprise optimization algorithms to help redistribute organizational slots based on a variety of user-defined criteria (e.g., lab/technical space constraints, organizational synergy constraints, move minimizations, etc.).
    Type: Application
    Filed: April 27, 2012
    Publication date: October 31, 2013
    Applicant: U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: William B. Ball, Robert L. Gage, Raymond L. Gates
  • Patent number: 8570047
    Abstract: A battery monitoring system utilizes a plurality of transformers interconnected with a battery having a plurality of battery cells. Windings of the transformers are driven with an excitation waveform whereupon signals are responsively detected, which indicate a health of the battery. In one embodiment, excitation windings and sense windings are separately provided for the plurality of transformers such that the excitation waveform is applied to the excitation windings and the signals are detected on the sense windings. In one embodiment, the number of sense windings and/or excitation windings is varied to permit location of underperforming battery cells utilizing a peak voltage detector.
    Type: Grant
    Filed: August 12, 2010
    Date of Patent: October 29, 2013
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Francis J. Davies, Jason R. Graika
  • Patent number: 8561829
    Abstract: A pressure vessel includes a ported fitting having an annular flange formed on an end thereof and a tank that envelopes the annular flange. A crack arresting barrier is bonded to and forming a lining of the tank within the outer surface thereof. The crack arresting barrier includes a cured resin having a post-curing ductility rating of at least approximately 60% through the cured resin, and further includes randomly-oriented fibers positioned in and throughout the cured resin.
    Type: Grant
    Filed: July 9, 2012
    Date of Patent: October 22, 2013
    Assignee: The United States of America as Represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Thomas K. DeLay