Patents Assigned to and Space Administration
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Publication number: 20100145510Abstract: A torsion spring comprises an inner mounting segment. An outer mounting segment is located concentrically around the inner mounting segment. A plurality of splines extends from the inner mounting segment to the outer mounting segment. At least a portion of each spline extends generally annularly around the inner mounting segment.Type: ApplicationFiled: December 10, 2008Publication date: June 10, 2010Applicants: GM GLOBAL TECHNOLOGY OPERATIONS, INC, The U.S.A As Represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Chris A. Ihrke, Adam H. Parsons, Joshua S. Mehling, Bryan Kristian Griffith
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Patent number: 7732496Abstract: Structurally stable and mechanically strong ceramic oxide aerogels are provided. The aerogels are cross-linked via organic polymer chains that are attached to and extend from surface-bound functional groups provided or present over the internal surfaces of a mesoporous ceramic oxide particle network via appropriate chemical reactions. The functional groups can be hydroxyl groups, which are native to ceramic oxides, or they can be non-hydroxyl functional groups that can be decorated over the internal surfaces of the ceramic oxide network. Methods of preparing such mechanically strong ceramic oxide aerogels also are provided.Type: GrantFiled: November 3, 2005Date of Patent: June 8, 2010Assignees: Ohio Aerospace Institute, The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Nicholas Leventis, Mary Ann B. Meador, James C. Johnston, Eve F. Fabrizio, Ulvi F. Ilhan
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Patent number: 7732998Abstract: A telescoping actuator assembly includes a plurality of cylindrical actuators in a concentric arrangement. Each cylindrical actuator is at least one piezoelectric fiber composite actuator having a plurality of piezoelectric fibers extending parallel to one another and to the concentric arrangement's longitudinal axis. Each cylindrical actuator is coupled to concentrically-adjacent ones of the cylindrical actuators such that the plurality of cylindrical actuators can experience telescopic movement. An electrical energy source coupled to the cylindrical actuators applies actuation energy thereto to generate the telescopic movement.Type: GrantFiled: August 3, 2006Date of Patent: June 8, 2010Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Sidney G. Allison, Qamar A. Shams, Robert L. Fox, Christopher L. Fox, legal representative, Melanie L. Fox Chattin, legal representative
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Patent number: 7732706Abstract: The invention is a novel manufacturing method for making multi-junction solar cell circuits that addresses current problems associated with such circuits by allowing the formation of integral diodes in the cells and allows for a large number of circuits to readily be placed on a single silicon wafer substrate. The standard Ge wafer used as the base for multi-junction solar cells is replaced with a thinner layer of Ge or a II-V semiconductor material on a silicon/silicon dioxide substrate. This allows high-voltage cells with multiple multi-junction circuits to be manufactured on a single wafer, resulting in less array assembly mass and simplified power management.Type: GrantFiled: September 16, 2005Date of Patent: June 8, 2010Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Nick Mardesich
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Publication number: 20100134498Abstract: In a method for domain decomposition for generating unstructured grids, a surface mesh is generated for a spatial domain. A location of a partition plane dividing the domain into two sections is determined. Triangular faces on the surface mesh that intersect the partition plane are identified. A partition grid of tetrahedral cells, dividing the domain into two sub-domains, is generated using a marching process in which a front comprises only faces of new cells which intersect the partition plane. The partition grid is generated until no active faces remain on the front. Triangular faces on each side of the partition plane are collected into two separate subsets. Each subset of triangular faces is renumbered locally and a local/global mapping is created for each sub-domain. A volume grid is generated for each sub-domain. The partition grid and volume grids are then merged using the local-global mapping.Type: ApplicationFiled: June 29, 2009Publication date: June 3, 2010Applicants: Space AdministrationInventors: Shahyar Z. Pirzadeh, Soheila Banihashemi
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Publication number: 20100135344Abstract: A method is provided for controlling second harmonic efficiency of laser beam interactions. A laser system generates two laser beams (e.g., a laser beam with two polarizations) for incidence on a nonlinear crystal having a preferred direction of propagation. Prior to incidence on the crystal, the beams are optically processed based on the crystal's beam separation characteristics to thereby control a position in the crystal along the preferred direction of propagation at which the beams interact.Type: ApplicationFiled: December 1, 2009Publication date: June 3, 2010Applicant: USA as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Norman P. Barnes, Brian M. Walsh, Donald J. Reichle
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Patent number: 7729047Abstract: A method of shifting and fixing an optical frequency of an optical resonator to a desired optical frequency, and an optical resonator made by such a method are provided. The method includes providing an optical resonator having a surface and a refractive index, and obtaining a coating composition having a predetermined concentration of a substance and having a refractive index that is substantially similar to the refractive index of the optical resonator. The coating composition inherently possesses a thickness when it is applied as a coating. The method further includes determining a coating ratio for the surface of the optical resonator and applying the coating composition onto a portion of the surface of the optical resonator based upon the determined coating ratio.Type: GrantFiled: September 14, 2007Date of Patent: June 1, 2010Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Anatoliy A. Savchenkov, Dmitry V. Strekalov, Lute Maleki, Andrey B. Matsko, Vladimir S. Iltchenko, Jan M. Martin
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Patent number: 7723464Abstract: Novel compositions of matter comprise certain derivatives of 9,9-dialkyl fluorene diamine (AFDA). The resultant compositions, whether compositions of matter or monomers that are subsequently incorporated into a polymer, are unique and useful in a variety of applications. Useful applications of AFDA-based material include heavy ion radiation shielding components and components of optical and electronic devices.Type: GrantFiled: February 13, 2007Date of Patent: May 25, 2010Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Donovan M. Delozier, Kent A. Watson, John W. Connell, Joseph G. Smith, Jr.
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Publication number: 20100122901Abstract: A system includes a collimated beam source within a vacuum chamber, a condensable barrier gas, cooling material, a pump, and isolation chambers cooled by the cooling material to condense the barrier gas. Pressure levels of each isolation chamber are substantially greater than in the vacuum chamber. Coaxially-aligned orifices connect a working chamber, the isolation chambers, and the vacuum chamber. The pump evacuates uncondensed barrier gas. The barrier gas blocks entry of atmospheric vapor from the working chamber into the isolation chambers, and undergoes supersonic flow expansion upon entering each isolation chamber. A method includes connecting the isolation chambers to the vacuum chamber, directing vapor to a boundary with the working chamber, and supersonically expanding the vapor as it enters the isolation chambers via the orifices. The vapor condenses in each isolation chamber using the cooling material, and uncondensed vapor is pumped out of the isolation chambers via the pump.Type: ApplicationFiled: May 22, 2009Publication date: May 20, 2010Applicant: USA as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Leonard M. Weinstein, Karen M. Taminger
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Patent number: 7718223Abstract: A method for controlling density or tower height of carbon nanotube (CNT) arrays grown in spaced apart first and second regions on a substrate. CNTs having a first density range (or first tower height range) are grown in the first region using a first source temperature range for growth. Subsequently or simultaneously, CNTs having a second density range (or second tower height range), having an average density (or average tower height) in the second region different from the average density (or average tower height) for the first region, are grown in the second region, using supplemental localized heating for the second region. Applications for thermal dissipation and/or dissipation of electrical charge or voltage in an electronic device are discussed.Type: GrantFiled: December 7, 2004Date of Patent: May 18, 2010Assignee: The United States of America as Represented by the Administrator of the National Aeronautics and Space Administration (NASA)Inventors: Lance D. Delzeit, John F. Schipper
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Publication number: 20100116079Abstract: A bidirectional tendon terminator that has particular application for terminating a tendon that actuates a finger in a robotic arm. The tendon terminator includes a cylindrical member having an internal channel through which a single continuous piece of the tendon extends. The internal channel of the tendon terminator includes a widened portion. A ball is placed in the tendon strands, which causes the tendon to expand, and the ball is positioned within the widened portion of the channel. Pulling on the tendon operates to either open or close the finger of the robotic arm depending on which direction the tendon is pulled. In one specific embodiment, the cylinder includes two cylindrical pieces that are coupled together so that the ball can be positioned within the channel and the cylindrical member has an entire circumference of material.Type: ApplicationFiled: November 12, 2008Publication date: May 13, 2010Applicants: GM GLOBAL TECHNOLOGY OPERATIONS, INC., The USA as represented by the Administrator of the National Aeronautics & Space AdministrationInventors: CHRIS A. IHRKE, DOUGLAS MARTIN LINN, LYNDON BRIDGWATER
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Publication number: 20100122117Abstract: A method of validating a probability of detection (POD) testing system using directed design of experiments (DOE) includes recording an input data set of observed hit and miss or analog data for sample components as a function of size of a flaw in the components. The method also includes processing the input data set to generate an output data set having an optimal class width, assigning a case number to the output data set, and generating validation instructions based on the assigned case number. An apparatus includes a host machine for receiving the input data set from the testing system and an algorithm for executing DOE to validate the test system. The algorithm applies DOE to the input data set to determine a data set having an optimal class width, assigns a case number to that data set, and generates validation instructions based on the case number.Type: ApplicationFiled: May 18, 2009Publication date: May 13, 2010Applicants: Space AdministrationInventor: Edward R. Generazio
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Publication number: 20100118916Abstract: A flexible thin metal film thermal sensing system is provided. A thermally-conductive film made from a thermally-insulating material is doped with thermally-conductive material. At least one layer of electrically-conductive metal is deposited directly onto a surface of the thermally-conductive film. One or more devices are coupled to the layer(s) to measure an electrical characteristic associated therewith as an indication of temperature.Type: ApplicationFiled: January 15, 2010Publication date: May 13, 2010Applicant: USA as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Donald L. Thomsen, III
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Patent number: 7715994Abstract: The invention is an improved process for using surface strain data to obtain real-time, operational loads data for complex structures that significantly reduces the time and cost versus current methods.Type: GrantFiled: August 14, 2008Date of Patent: May 11, 2010Assignee: The United States of America as represented by the National Aeronautics and Space AdministrationInventors: William Lance Richards, William L. Ko
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Publication number: 20100109818Abstract: A wireless electrical device includes an electrically unconnected electrical conductor and at least one electrically unconnected electrode spaced apart from the electrical conductor. The electrical conductor is shaped for storage of an electric field and a magnetic field. In the presence of a time-varying magnetic field, the electrical conductor so-shaped resonates to generate harmonic electric and magnetic field responses. Each electrode is at a location lying within the magnetic field response so-generated and is constructed such that a linear movement of electric charges is generated in each electrode due to the magnetic field response so-generated.Type: ApplicationFiled: September 30, 2009Publication date: May 6, 2010Applicant: U.S.A. as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Stanley E. Woodard, Bryant Douglas Taylor
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Patent number: 7711509Abstract: A method of calibrating a fluid-level measurement system is provided. A first response of the system is recorded when the system's sensor(s) is (are) not in contact with a fluid of interest. A second response of the system is recorded when the system's sensor(s) is (are) fully immersed in the fluid of interest. Using the first and second responses, a plurality of expected responses of the system's sensor(s) is (are) generated for a corresponding plurality of levels of immersion of the sensor(s) in the fluid of interest.Type: GrantFiled: October 31, 2007Date of Patent: May 4, 2010Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Stanley E. Woodard, Bryant D. Taylor
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Patent number: 7711455Abstract: A low-cost, easily retrofit Propulsion Controlled Aircraft (PCA) system for use on a wide range of commercial and military aircraft consists of an propulsion controlled aircraft computer that reads in aircraft data including aircraft state, pilot commands and other related data, calculates aircraft throttle position for a given maneuver commanded by the pilot, and then displays both current and calculated throttle position on a cockpit display to show the pilot where to move throttles to achieve the commanded maneuver, or is automatically sent digitally to command the engines directly.Type: GrantFiled: August 9, 2006Date of Patent: May 4, 2010Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Bruce R. Cogan
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Publication number: 20100106348Abstract: Systems, methods and apparatus are provided through which in some embodiments an autonomic entity manages a system by generating one or more stay alive signals based on the functioning status and operating state of the system. In some embodiments, an evolvable synthetic neural system is operably coupled to one or more evolvable synthetic neural systems in a hierarchy. The evolvable neural interface receives and generates heartbeat monitor signals and pulse monitor signals that are used to generate a stay alive signal that is used to manage the operations of the synthetic neural system. In another embodiment an asynchronous Alice signal (Autonomic license) requiring valid credentials of an anonymous autonomous agent is initiated. An unsatisfactory Alice exchange may lead to self-destruction of the anonymous autonomous agent for self-protection.Type: ApplicationFiled: October 21, 2009Publication date: April 29, 2010Applicant: U.S.A as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Michael G. Hinchey, Roy Sterritt
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Patent number: 7704622Abstract: This invention relates to a series of organic/inorganic hybrid polymers that are easy to fabricate into dimensionally stable films with good ion-conductivity over a wide range of temperatures for use in a variety of applications. The polymers are prepared by the reaction of amines, preferably diamines and mixtures thereof with monoamines with epoxy-functionalized alkoxysilanes. The products of the reaction are polymerized by hydrolysis of the alkoxysilane groups to produce an organic-containing silica network. Suitable functionality introduced into the amine and alkoxysilane groups produce solid polymeric membranes which conduct ions for use in fuel cells, high-performance solid state batteries, chemical sensors, electrochemical capacitors, electro-chromic windows or displays, analog memory devices and the like.Type: GrantFiled: August 26, 2004Date of Patent: April 27, 2010Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Maryann B. Meador, James D. Kinder
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Patent number: 7704547Abstract: Method and system for combined coarse scale control and fine scale control of growth density of a carbon nanotube (“CNT”) array on a substrate, using a selected electrical field adjacent to a substrate surface for coarse scale density control (by one or more orders of magnitude) and a selected CNT growth temperature range for fine scale density control (by multiplicative factors of less than an order of magnitude) of CNT growth density. Two spaced apart regions on a substrate may have different CNT growth densities and/or may use different feed gases for CNT growth.Type: GrantFiled: June 20, 2006Date of Patent: April 27, 2010Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration (NASA)Inventors: Lance D. Delzeit, John F. Schipper