Patents Assigned to and Space Administration
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Patent number: 8078309Abstract: Disclosed herein is a method of making a three dimensional mold comprising the steps of providing a mold substrate; exposing the substrate with an electromagnetic radiation source for a period of time sufficient to render the portion of the mold substrate susceptible to a developer to produce a modified mold substrate; and developing the modified mold with one or more developing reagents to remove the portion of the mold substrate rendered susceptible to the developer from the mold substrate, to produce the mold having a desired mold shape, wherein the electromagnetic radiation source has a fixed position, and wherein during the exposing step, the mold substrate is manipulated according to a manipulation algorithm in one or more dimensions relative to the electromagnetic radiation source; and wherein the manipulation algorithm is determined using stochastic optimization computations.Type: GrantFiled: March 31, 2009Date of Patent: December 13, 2011Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Francis B. Eyre, Wolfgang Fink
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Patent number: 8076136Abstract: The present disclosure provides ex vivo-derived mineralized three-dimensional bone constructs. The bone constructs are obtained by culturing osteoblasts and osteoclast precursors under randomized gravity vector conditions. Preferably, the randomized gravity vector conditions are obtained using a low shear stress rotating bioreactor, such as a High Aspect Ratio Vessel (HARV) culture system. The bone constructs of the disclosure have utility in physiological studies of bone formation and bone function, in drug discovery, and in orthopedics.Type: GrantFiled: March 29, 2007Date of Patent: December 13, 2011Assignees: The United States of America as represented by the United States National Aeronautics and Space Administration, University of Houston, Universities Space Research AssociationInventors: Mark S. F. Clarke, Alamelu Sundaresan, Neal R. Pellis
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Publication number: 20110299777Abstract: Disclosed herein are systems, methods, and non-transitory computer-readable storage media for processing image information using a more computationally efficient version of a previously developed HSEG (Hierarchical Segmentation) algorithm. The HSEG algorithm includes iterations intertwining two forms of region growing to produce a set of hierarchically related image segmentations. The first form is a commonly used approach in which regions are grown by merging the most similar spatially adjacent regions. The second form is a unique approach in which regions are grown by also merging spatially non-adjacent regions that are at least as similar as the spatially adjacent regions merged by the first form in the same iteration. The improved HSEG algorithm limits the regions considered for non-adjacent region merging in the second form of operation to regions having at least a minimum number of pixels. This minimum is dynamically controlled to optimize processing efficiency and image segmentation quality.Type: ApplicationFiled: June 1, 2011Publication date: December 8, 2011Applicants: Space AdministrationInventor: James C. Tilton
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Publication number: 20110300523Abstract: Disclosed are methods and apparatuses provided for modifying the effect of an operator controlled input device on an interactive device to encourage the self-regulation of at least one physiological activity by a person different than the operator. The interactive device comprises a display area which depicts images and apparatus for receiving at least one input from the operator controlled input device to thus peiiiiit the operator to control and interact with at least some of the depicted images. One effect modification comprises measurement of the physiological activity of a person different from the operator, while modifying the ability of the operator to control and interact with at least some of the depicted images by modifying the input from the operator controlled input device in response to changes in the measured physiological signal.Type: ApplicationFiled: June 22, 2011Publication date: December 8, 2011Applicant: U. S.A. as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Alan T. Pope, Olafur S. Palsson
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Patent number: 8070105Abstract: An inflatable structure comprises at least two generally toroidal, inflatable modules. When in a deployed mode, the first, inner module has a major diameter less than that of a second, outer module and is positioned within the inner circumference of the outer module such that the first module is nested circumferentially alongside the second module. The inflatable structure, in a non-deployed, non-inflated mode, is of compact configuration and adapted to be transported to a site of deployment. When deployed, the inflatable structure is of substantially increased interior volume. In one embodiment, access between the interior of the first module and the second module is provided by at least one port or structural pass-through. In another embodiment, the inflatable structure includes at least one additional generally toroidal module external of and circumferentially surrounding the second module.Type: GrantFiled: December 14, 2007Date of Patent: December 6, 2011Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Christopher J. Johnson, Jasen L. Raboin, Gary R. Spexarth
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Publication number: 20110295419Abstract: A robotic system includes a robotic mechanism responsive to velocity control signals, and a permissible workspace defined by a convex-polygon boundary. A host machine determines a position of a reference point on the mechanism with respect to the boundary, and includes an algorithm for enforcing the boundary by automatically shaping the velocity control signals as a function of the position, thereby providing smooth and unperturbed operation of the mechanism along the edges and corners of the boundary. The algorithm is suited for application with higher speeds and/or external forces. A host machine includes an algorithm for enforcing the boundary by shaping the velocity control signals as a function of the reference point position, and a hardware module for executing the algorithm. A method for enforcing the convex-polygon boundary is also provided that shapes a velocity control signal via a host machine as a function of the reference point position.Type: ApplicationFiled: May 26, 2010Publication date: December 1, 2011Applicants: The U.S.A. As Represented by the Administrator of the National Aeronautics and Space Administration, GM GLOBAL TECHNOLOGY OPERATIONS, INC.Inventors: Muhammad E. Abdallah, Brian Hargrave, Robert J. Platt, JR.
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Patent number: 8069001Abstract: An isotherm sensor tracks space vehicle temperatures by a thermal protection system (TPS) material during vehicle re-entry as a function of time, and surface recession through calibration, calculation, analysis and exposed surface modeling. Sensor design includes: two resistive conductors, wound around a tube, with a first end of each conductor connected to a constant current source, and second ends electrically insulated from each other by a selected material that becomes an electrically conductive char at higher temperatures to thereby complete an electrical circuit. The sensor conductors become shorter as ablation proceeds and reduced resistance in the completed electrical circuit (proportional to conductor length) is continually monitored, using measured end-to-end voltage change or current in the circuit. Thermocouple and/or piezoelectric measurements provide consistency checks on local temperatures.Type: GrantFiled: January 2, 2009Date of Patent: November 29, 2011Assignee: The United States of America as represented by the Administrator of the National Aeronautics & Space Administration (NASA)Inventors: Sergey Gorbunov, Edward R. Martinez, James B. Scott, Tomomi Oishi, Johnny Fu, Joseph G. Mach, Jose B. Santos
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Patent number: 8067478Abstract: Process for preparing polymer-reinforced silica aerogels which comprises a one-pot reaction of at least one alkoxy silane in the presence of effective amounts of a polymer precursor to obtain a silica reaction product, the reaction product is gelled and subsequently subjected to conditions that promotes polymerization of the precursor and then supercritically dried to obtain the polymer-reinforced monolithic silica aerogels.Type: GrantFiled: October 19, 2006Date of Patent: November 29, 2011Assignee: The United States of America as represented by the Administrator of National Aeronautics and Space AdministrationInventors: Mary Ann B. Meador, Lynn A. Capadona
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Patent number: 8063171Abstract: A three dimensional structure fabricated from a self-healing polymeric material, comprising poly(ester amides) obtained from ethylene glycol, azelaic acid and 1,1-aminoundecanoic acid, wherein polymeric material has a melt index above 2.5 g/10 min. as determined by ASTM D1238 at 190° C. and 2.16kg, impact resistance and ductility sufficient to resist cracking and brittle fracture upon impact by a 9 mm bullet fired at a temperature of about 29° C. at subsonic speed in a range from about 800 feet/sec to about 1000 feet/sec. It has been determined that the important factors necessary for self-healing behavior of polymers include sufficient impact strength, control of the degree of crystallinity, low melting point and the ability to instantly melt at impacted area.Type: GrantFiled: January 9, 2009Date of Patent: November 22, 2011Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Daniel J. Klein
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Publication number: 20110278393Abstract: A suspension apparatus for suspending instrumentation from an airborne platform may include a generally longitudinal boom having a payload end and a tail end. Yaw and pitch stabilizers may be disposed at the tail end of the boom. A mast that may be selectively translatable on the boom may connect the boom to a tether line of the airborne platform. The payload may be attached to the payload end of the boom. The mast may be positioned axially along the boom at the center of gravity of the combination of the payload, boom, pitch stabilizer, and yaw stabilizer.Type: ApplicationFiled: May 13, 2010Publication date: November 17, 2011Applicant: National Aeronautics and Space AdministrationInventors: Geoffrey L. Bland, Ted K. Miles
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Patent number: 8060250Abstract: A system and method for controlling tendon-driven manipulators that provide a closed-loop control of joint torques or joint impedances without inducing dynamic coupling between joints. The method includes calculating tendon reference positions or motor commands by projecting a torque error into tendon position space using a single linear operation. The method calculates this torque error using sensed tendon tensions and a reference torque and internal tension. The method can be used to control joint impedance by calculating the reference torque based on a joint position error. The method limits minimum and maximum tendon tensions by projecting the torque error into the tendon tension space and then projecting ii back into joint space.Type: GrantFiled: December 15, 2008Date of Patent: November 15, 2011Assignees: GM Global Technology Operations LLC, The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationsInventors: Matthew J. Reiland, Robert Platt, Charles W. Wampler, II, Muhammad E. Abdallah, Brian Hargrave
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Patent number: 8056423Abstract: A technique that determines the tension in a tendon using a conduit reaction force applied to an end of a conduit through which the tendon is threaded. Any suitable tendon tension sensor can be employed that uses the conduit reaction force for this purpose. In one non-limiting embodiment, the tendon tension sensor includes a cylindrical strain gauge element and a force member mounted to an end of the conduit. The force member includes a cylindrical portion having a bore and a plate portion, where the cylindrical portion is inserted into a bore in the strain gauge element. The tendon is threaded through the strain gauge element and the force member. A strain gauge is mounted to the strain gauge element and measures the reaction force when tension on the tendon causes the strain gauge element to be pushed against the force member.Type: GrantFiled: November 12, 2008Date of Patent: November 15, 2011Assignees: GM Global Technology Operations LLC, The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Muhammad E. Abdallah, Lyndon Bridgwater, Myron A. Diftler, Douglas Martin Linn, Charles W. Wampler, II, Robert Platt
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Patent number: 8060350Abstract: Computational aeroelastic analyses typically use a mathematical model for the structural modes of a flexible structure and a nonlinear aerodynamic model that can generate a plurality of unsteady aerodynamic responses based on the structural modes for conditions defining an aerodynamic condition of the flexible structure. In the present invention, a linear state-space model is generated using a single execution of the nonlinear aerodynamic model for all of the structural modes where a family of orthogonal functions is used as the inputs. Then, static and dynamic aeroelastic solutions are generated using computational interaction between the mathematical model and the linear state-space model for a plurality of periodic points in time.Type: GrantFiled: March 27, 2008Date of Patent: November 15, 2011Assignee: United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Walter A. Silva
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Patent number: 8059273Abstract: A spectrometer system includes an optical assembly for collimating light, a micro-ring grating assembly having a plurality of coaxially-aligned ring gratings, an aperture device defining an aperture circumscribing a target focal point, and a photon detector. An electro-optical layer of the grating assembly may be electrically connected to an energy supply to change the refractive index of the electro-optical layer. Alternately, the gratings may be electrically connected to the energy supply and energized, e.g., with alternating voltages, to change the refractive index. A data recorder may record the predetermined spectral characteristic.Type: GrantFiled: July 2, 2009Date of Patent: November 15, 2011Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Yeonjoon Park, Sang H. Choi, Glen C. King, James R. Elliott
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Patent number: 8057283Abstract: A method of fabricating a whispering gallery mode resonator (WGMR) is provided. The WGMR can be fabricated from a particular material, annealed, and then polished. The WGMR can be repeatedly annealed and then polished. The repeated polishing of the WGMR can be carried out using an abrasive slurry. The abrasive slurry can have a predetermined, constant grain size. Each subsequent polishing of the WGMR can use an abrasive slurry having a grain size that is smaller than the grain size of the abrasive slurry of the previous polishing iteration.Type: GrantFiled: May 13, 2008Date of Patent: November 15, 2011Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Anatoliy A. Savchenkov, Andrey B. Matkso, Vladimir S. Iltchenko, Lute Maleki
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Patent number: 8052860Abstract: A method and system are provided for the shaping and polishing of the surface of a material selected from the group consisting of electrically semi-conductive materials and conductive materials. An electrically non-conductive polishing lap incorporates a conductive electrode such that, when the polishing lap is placed on the material's surface, the electrode is placed in spaced-apart juxtaposition with respect to the material's surface. A liquid electrolyte is disposed between the material's surface and the electrode. The electrolyte has an electrochemical stability constant such that cathodic material deposition on the electrode is not supported when a current flows through the electrode, the electrolyte and the material. As the polishing lap and the material surface experience relative movement, current flows through the electrode based on (i) adherence to Faraday's Law, and (ii) a pre-processing profile of the surface and a desired post-processing profile of the surface.Type: GrantFiled: December 14, 2007Date of Patent: November 8, 2011Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Darell E. Engelhaupt, Mikhail V. Gubarev, William David Jones, Brian D. Ramsey, Carl M. Benson
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Patent number: 8052854Abstract: A gas sensor includes a substrate and a pair of interdigitated metal electrodes selected from the group consisting of Pt, Pd, Au, Ir, Ag, Ru, Rh, In, and Os. The electrodes each include an upper surface. A first solid electrolyte resides between the interdigitated electrodes and partially engages the upper surfaces of the electrodes. The first solid electrolyte is selected from the group consisting of NASICON, LISICON, KSICON, and ??-Alumina (beta prime-prime alumina in which when prepared as an electrolyte is complexed with a mobile ion selected from the group consisting of Na+, K+, Li+, Ag+, H+, Pb2+, Sr2+ or Ba2+). A second electrolyte partially engages the upper surfaces of the electrodes and engages the first solid electrolyte in at least one point. The second electrolyte is selected from the group of compounds consisting of Na+, K+, Li+, Ag+, H+, Pb2+, Sr2+ or Ba2+ ions or combinations thereof.Type: GrantFiled: May 25, 2007Date of Patent: November 8, 2011Assignee: The United States of America as represented by the Administrator of National Aeronautics and Space AdministrationInventors: Gary W. Hunter, Jennifer C. Xu, Chung Chiun Liu, Benjamin J. Ward
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Patent number: 8052324Abstract: A thin film ceramic thermocouple (10) having two ceramic thermocouple (12, 14) that are in contact with each other in at least on point to form a junction, and wherein each element was prepared in a different oxygen/nitrogen/argon plasma. Since each element is prepared under different plasma conditions, they have different electrical conductivity and different charge carrier concentration. The thin film thermocouple (10) can be transparent. A versatile ceramic sensor system having an RTD heat flux sensor can be combined with a thermocouple and a strain sensor to yield a multifunctional ceramic sensor array. The transparent ceramic temperature sensor that could ultimately be used for calibration of optical sensors.Type: GrantFiled: February 4, 2010Date of Patent: November 8, 2011Assignees: Board of Governors for Higher Education, State of Rhode Island and Providence Plantations, National Aeronautics and Space AdministrationInventors: Otto Gregory, Gustave Fralick, John Wrbanek, Tao You
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Patent number: 8052069Abstract: The present invention comprises a high performance, vertical, zero-net mass-flux, synthetic jet actuator for active control of viscous, separated flow on subsonic and supersonic vehicles. The present invention is a vertical piezoelectric hybrid zero-net mass-flux actuator, in which all the walls of the chamber are electrically controlled synergistically to reduce or enlarge the volume of the synthetic jet actuator chamber in three dimensions simultaneously and to reduce or enlarge the diameter of orifice of the synthetic jet actuator simultaneously with the reduction or enlargement of the volume of the chamber. The jet velocity and mass flow rate for the present invention will be several times higher than conventional piezoelectric synthetic jet actuators.Type: GrantFiled: February 26, 2009Date of Patent: November 8, 2011Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Tian-Bing Xu, Xiaoning Jiang, Ji Su
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Patent number: 8047473Abstract: A connecting node comprises a polyhedral structure comprising a plurality of panels joined together at its side edges to form a spherical approximation, wherein at least one of the plurality of panels comprises a faceted surface being constructed with a passage for integrating with one of a plurality of elements comprising a docking port, a hatch, and a window that is attached to the connecting node. A method for manufacturing a connecting node comprises the steps of providing a plurality of panels, connecting the plurality of panels to form a spherical approximation, wherein each edge of each panel of the plurality is joined to another edge of another panel, and constructing at least one of the plurality of panels to include a passage for integrating at least one of a plurality of elements that may be attached to the connecting node.Type: GrantFiled: September 29, 2008Date of Patent: November 1, 2011Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Christopher J. Johnson, Jasen L. Raboin, Gary R. Spexarth