Patents Assigned to The United States of America as represented by the
Administrator of the National Aeronautics and Space
Adminstration
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Patent number: 10451156Abstract: 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: GrantFiled: May 26, 2017Date of Patent: October 22, 2019Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space AdminstrationInventors: Michael J. Krasowski, Lawrence C. Greer
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Patent number: 9465965Abstract: 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: GrantFiled: February 19, 2014Date of Patent: October 11, 2016Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdminstrationInventors: Patrick W. Fink, Andrew W. Chu, Gregory Y. Lin, Timothy F. Kennedy, Phong H. Ngo, Dewey T. Brown, Diane Byerly
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Patent number: 9354134Abstract: 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: GrantFiled: February 27, 2014Date of Patent: May 31, 2016Assignee: THE UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINSTRATIONInventors: Sean A. Commo, Keith C. Lynn, Drew Landman, Michael J. Acheson
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Patent number: 9151639Abstract: 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: GrantFiled: February 10, 2014Date of Patent: October 6, 2015Assignee: The United States of America as Represented by the Administrator of the National Aeronautics and Space AdminstrationInventors: Robert C. Youngquist, Stanley O. Starr
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Patent number: 9067794Abstract: 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: GrantFiled: August 5, 2009Date of Patent: June 30, 2015Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdminstrationInventors: Ya-Ping Sun, John W. Connell, Lucia Monica Veca
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Patent number: 8163243Abstract: 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: GrantFiled: September 7, 2006Date of Patent: April 24, 2012Assignee: The United States of America as represented by the Administrator of National Aeronautics and Space AdminstrationInventor: Kenneth A. Burke
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Patent number: 7890311Abstract: 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: GrantFiled: July 7, 2005Date of Patent: February 15, 2011Assignee: United States of America as represented by the Administrator of the National Aeronautics and Space AdminstrationInventors: Neal E. Hass, Paul A. Schallhorn
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Patent number: 7504921Abstract: 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: GrantFiled: September 29, 2006Date of Patent: March 17, 2009Assignee: United States of America as represented by the Administrator of the National Aeronautics and Space AdminstrationInventor: John M. Vranish
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Patent number: 6810743Abstract: The present invention uses the generation and detection of acoustic guided waves to evaluate the condition of the insulation on electrical wiring. Low order axisymmetric and flexural acoustic modes are generated in the insulated wire and travel partially in the center conductor and partially in the outer insulation. The stiffness of the insulation and the insulation's condition affect the overall wave speed and amplitude of the guided wave. Analysis of the received signal provides information about the age or useful life of the wire insulation. In accordance with the present invention, signal transmission occurs at one location on the electrical wire to be evaluated, and detection occurs at one or more locations along the electrical wire. Additional receivers can be used to improve measurement accuracy. Either the transmission transducer or one or more receiver transducers may be angled at other than 90 degrees to the wire.Type: GrantFiled: August 1, 2002Date of Patent: November 2, 2004Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdminstrationInventors: Eric I. Madaras, Robert F. Anastasi
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Patent number: 6441099Abstract: Phenylethynyl containing reactive additives were prepared from aromatic diamines containing phenylethynyl groups and various ratios of phthalic anhydride and 4-phenylethynylphthalic anhydride in glacial acetic acid to form the imide in one step or in N-methyl-2-pyrrolidinone to form the amide acid intermediate. The reactive additives were mixed in various amounts (10% to 90%) with oligomers containing either terminal or pendent phenylethynyl groups (or both) to reduce the melt viscosity and thereby enhance processability. Upon thermal cure, the additives react and become chemically incorporated into the matrix and effect an increase in crosslink density relative to that of the host resin. This resultant increase in crosslink density has advantageous consequences on the cured resin properties such as higher glass transition temperature and higher modulus as compared to that of the host resin.Type: GrantFiled: November 28, 2000Date of Patent: August 27, 2002Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdminstrationInventors: John W. Connell, Joseph G. Smith, Jr., Paul M. Hergenrother
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Patent number: 6321746Abstract: A portable, collapsible hyperbaric chamber. A toroidal inflatable skeleton provides initial structural support for the chamber, allowing the attendant and/or patient to enter the chamber. Oval hatches mate against bulkhead rings, and the hyperbaric chamber is pressurized. The hatches seal against an o-ring, and the internal pressure of the chamber provides the required pressure against the hatch to maintain an airtight seal. In the preferred embodiment, the hyperbaric chamber has an airlock to allow the attendant to enter and exit the patient chamber during treatment. Visual communication is provided through portholes in the patient and/or airlock chamber. Life monitoring and support systems are in communication with the interior of the hyperbaric chamber and/or airlock chamber through conduits and/or sealed feed-through connectors into the hyperbaric chamber.Type: GrantFiled: May 17, 2000Date of Patent: November 27, 2001Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdminstrationInventors: William C Schneider, James P. Locke, Horacio M De La Fuente
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Patent number: 6211822Abstract: The spaceborne Global Positioning System receiver provides navigational solutions and is designed for use in low Earth orbit. The spaceborne GPS receiver can determine the orbital position of a spacecraft using any of the satellites within the GPS constellation. It is a multiple processor system incorporating redundancy by using a microcontroller to handle the closure of tracking loops for acquired GPS satellites, while a separate microprocessor computes the spacecraft navigational solution and handles other tasks within the receiver. The spaceborne GPS receiver can use either microcontroller or the microprocessor to close the satellite tracking loops. The use of microcontroller provides better tracking performance of acquired GPS satellites. The spaceborne GPS receiver utilizes up to seven separate GPS boards, with each board including its own set of correlators, down-converters and front-end components. The spaceborne GPS receiver also includes telemetry and time-marking circuitry.Type: GrantFiled: July 7, 1999Date of Patent: April 3, 2001Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdminstrationsInventors: Lamar F. Dougherty, Frederick A. Niles, Miriam D. Wennersten
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Patent number: 6019926Abstract: Self-metallizing, flexible polyimide films with highly reflective surfaces are prepared by an in situ self-metallization procedure involving thermally initiated reduction of polymer-soluble silver(I) complexes. Polyamic acid solutions are doped with silver(I) acetate and solubilizing agents. Thermally curing the silver(I)-doped resins leads to flexible, metallized films which have reflectivities as high as 100%, abrasion-resistant surfaces, thermal stability and, in some cases, electrical conductivity, rendering them useful for space applications.Type: GrantFiled: February 20, 1998Date of Patent: February 1, 2000Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdminstrationInventors: Robin E. Southward, David W. Thompson, Anne K. St. Clair, Diane M. Stoakley
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Patent number: 6013996Abstract: An improved stop control system and method are provided for a motor having a drive mechanism in which the motor is coupled to a motor controller that controls the speed and position of the drive mechanism using a first signal indicative of a commanded position of the drive mechanism, a second signal indicative of the actual speed of the drive mechanism and a third signal indicative of the actual position of the drive mechanism. The improved system/method uses a first circuit that receives the first and third signal and generates an error signal indicative of a difference therebetween. A second circuit receives the error signal and compares same with a threshold position error. The result of this comparison is used to selectively supply the second signal (i.e., speed) to the motor controller at least whenever the error signal is less than the threshold position error so that the motor controller can use the second signal in conjunction with the third signal to stop the motor.Type: GrantFiled: July 27, 1998Date of Patent: January 11, 2000Assignee: The United States of America as represented by the Administrator of National Aeronautics and Space AdminstrationInventors: David E. Howard, Justino Montenegro
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Patent number: 5969253Abstract: A multilayer object having multiple layers arranged in a stacking direction is evaluated for imperfections such as voids, delaminations and microcracks. First, an acoustic wave is transmitted into the object in the stacking direction via an appropriate transducer/waveguide combination. The wave propagates through the multilayer object and is received by another transducer/waveguide combination preferably located on the same surface as the transmitting combination. The received acoustic wave is correlated with the presence or absence of imperfections by, e.g., generating pulse echo signals indicative of the received acoustic wave, wherein the successive signals form distinct groups over time. The respective peak amplitudes of each group are sampled and curve fit to an exponential curve, wherein a substantial fit of approximately 80-90% indicates an absence of imperfections and a significant deviation indicates the presence of imperfections.Type: GrantFiled: June 9, 1997Date of Patent: October 19, 1999Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdminstrationInventors: Joseph S. Heyman, Md. Nurul Abedin, Kuen J. Sun
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Patent number: 5962324Abstract: A process for artificially producing three-dimensional optic tissue has been developed. The optic cells are cultured in a bioreactor at low shear conditions. The tissue forms as normal, functional tissue grows with tissue organization and extracellular matrix formation.Type: GrantFiled: May 13, 1994Date of Patent: October 5, 1999Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdminstrationInventors: Kim C. O'Connor, Glenn F. Spaulding, Thomas J. Goodwin, Laurie A. Aten, Karen M. Francis, Delmar R. Caldwell, Tacey L. Prewett, Wendy S. Fitzgerald
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Patent number: 5665959Abstract: A solid-state focal-plane imaging system comprises an N.times.N array of high gain, low-noise unit cells, each unit cell being connected to a different one of photovoltaic detector diodes, one for each unit cell, interspersed in the array for ultralow level image detection and a plurality of digital counters coupled to the outputs of the unit cell by a multiplexer (either a separate counter for each unit cell or a row of N of counters time shared with N rows of digital counters). Each unit cell includes two self-biasing cascode amplifiers in cascade for a high charge-to-voltage conversion gain (>1 mV/e.sup.-) and an electronic switch to reset input capacitance to a reference potential in order to be able to discriminate detection of an incident photon by the photoelectron (e.sup.-) generated in the detector diode at the input of the first cascode amplifier in order to count incident photons individually in a digital counter connected to the output of the second cascode amplifier.Type: GrantFiled: July 1, 1996Date of Patent: September 9, 1997Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdminstrationInventors: Eric R. Fossum, Bedabrata Pain
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Patent number: 5475878Abstract: A protective helmet assembly (10) comprising a hard ballistic outer shell (12) in a clam shell construction of hinged shell portions (14, 16), the front portion (14) being provided with a window opening (20) and a facial seal (34). A transparent visor (22) and sun visor (24) are pivotally mounted on the shell portion (14) and are positionable to cover the window with a seal (23) between the visor (22) and shell portion (14). Impact absorbing pads (31, 32) of open cell flexible polyimide foam material are attached to the inner surface of the hard shell portions (14, 16) by cooperative fastener strips (35, 36) of hook-and-loop material.Type: GrantFiled: November 4, 1992Date of Patent: December 19, 1995Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdminstrationInventors: Frederic S. Dawn, John D. Eck, Fred R. Weiss
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Patent number: 5302692Abstract: The diamine, 1,3-diamino-5-pentafluorosulfanylbenzene (DASP), was reacted with various dianhydrides to form polyimides containing an SF.sub.5 moiety. These polyimides exhibit high glass transition temperatures, high density, low solubility, and low dielectric properties. These polymers were used to prepare semi-permeable membranes, wire coatings, and films and are useful for electronic, space and piezoelectric applications.Type: GrantFiled: May 27, 1993Date of Patent: April 12, 1994Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdminstrationInventors: Anna K. St. Clair, Terry L. St. Clair
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Patent number: 5281042Abstract: A saddle clamp assembly includes a hollow cylindrical body centered about a longitudinal axis and being diametrically split into semicircular top and bottom sections each having a pair of radially outwardly projecting connection flanges at their opposite ends. A pair of bolts are captively retained on the top section flanges and are threadable into nuts captively retained on the bottom section flanges. A base member is anchored to a central underside portion of the bottom clamp body section and has a pair of connection tabs positioned beneath the bottom clamp body section connection flanges on opposite sides of the clamp axis. A pair of bolts are captively retained on the base member connection tabs and are threadable into a pair of nuts captively retainable on a support structure. The connection tab and connection flanges on each side of the clamp body are axially offset in a manner permitting downward installation/removal tool access to the lower bolts past the connection flanges.Type: GrantFiled: November 17, 1992Date of Patent: January 25, 1994Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdminstrationInventor: Charles R. Belrose