Patents Assigned to Space
  • Patent number: 7127068
    Abstract: Systems and methods to create venue tokens that provide generalized geographic information while preserving location specific data. In one embodiment, a Universal Location Descriptor (ULD) translator converts location data into a geocode that in one embodiment is a binary code. Location information can include a street address, zip code, directional information, destination, velocity information, latitude and/or longitude, etc. The geocode can then be encrypted to generate a token. Relative geographic similarities can be identified by comparing geographic information from the tokens, thereby allowing similarly situated individuals and/or organizations, service providers, etc., to be identified without disclosing specific location identities of those parties seeking such privacy.
    Type: Grant
    Filed: May 23, 2001
    Date of Patent: October 24, 2006
    Assignee: Info Space, Inc.
    Inventors: Vale Sundaravel, Benjamin J. Paul
  • Patent number: 7126553
    Abstract: A deployable antenna and method for using wherein the deployable antenna comprises a collapsible membrane having at least one radiating element for transmitting electromagnetic waves, receiving electromagnetic waves, or both.
    Type: Grant
    Filed: October 2, 2003
    Date of Patent: October 24, 2006
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Patrick W. Fink, Justin A. Dobbins, Greg Y. Lin, Andrew W. Chu, Robert C. Scully
  • Patent number: 7125370
    Abstract: An apparatus and method for exercising whereby the user is supported by various mechanisms in such as way that the user's shoulder area is free to translate and rotate; the user's pelvic area is free to translate and rotate; or in any combination.
    Type: Grant
    Filed: May 12, 2004
    Date of Patent: October 24, 2006
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Grant Schaffner, Jason R. Bentley, James A. Loehr, Daniel P. Gundo
  • Publication number: 20060235136
    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: Application
    Filed: April 12, 2006
    Publication date: October 19, 2006
    Applicant: Administrator of the National Aeronautics and Space Administration
    Inventors: Dennis Working, Emilie Siochi, Cheol Park, Peter Lillehei
  • Publication number: 20060232174
    Abstract: A mobile storage system includes a series of storage units that include wheel assemblies that move on floor-mounted rails. The storage units, wheel assemblies and rails are produced and shipped in disassembled, knockdown kit form, and are assembled on-site in either a lateral high density configuration or a pull-out high density configuration. The user is able to selectively configure the storage units, the wheel assemblies and the rails to provide the desired configuration of the storage system.
    Type: Application
    Filed: March 12, 2004
    Publication date: October 19, 2006
    Applicant: Space Saver Corporation
    Inventors: James Muth, Brian Nemec, Steven Janson, Marvin Runge, Steve Dingle
  • Patent number: 7122071
    Abstract: A gas-liquid separator uses a helical passageway to impart a spiral motion to a fluid passing therethrough. The centrifugal force generated by the spiraling motion urges the liquid component of the fluid radially outward which forces the gas component radially inward. The gas component is then separated through a gas-permeable, liquid-impervious membrane and discharged through a central passageway. A filter material captures target substances contained in the fluid.
    Type: Grant
    Filed: September 25, 2002
    Date of Patent: October 17, 2006
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Steve R. Gonda, Yow-Min D. Tsao, Wenshan Lee
  • Patent number: 7122166
    Abstract: Methods for concentrating hydrogen peroxide solutions have been described. The methods utilize a polymeric membrane separating a hydrogen peroxide solution from a sweep gas or permeate. The membrane is selective to the permeability of water over the permeability of hydrogen peroxide, thereby facilitating the concentration of the hydrogen peroxide solution through the transport of water through the membrane to the permeate. By utilizing methods in accordance with the invention, hydrogen peroxide solutions of up to 85% by volume or higher may be generated at a point of use without storing substantial quantities of the highly-concentrated solutions and without requiring temperatures that would produce explosive mixtures of hydrogen peroxide vapors.
    Type: Grant
    Filed: May 11, 2004
    Date of Patent: October 17, 2006
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Clyde F. Parrish
  • Patent number: 7118094
    Abstract: A cage in which two pulley wheels are mounted with tangent circumferences so that their circumferential cable grooves surround a cable passing between the wheels. The cage freely rotates about an axis that passes between the wheels. The cage axis is normal to the plane of the parallel wheel axes. The cage extends forward of the wheels and forms two curved edges on opposed sides of the cage axis. Each curve has an apex at its forward-most point. A flexible cable passes through the cage, between the wheels, and forward between the curves. Extending the cable substantially away from the plane of the wheels causes it to contact one of the curves. This rotates the cage so that the wheels are aligned with the cable deflection. This switches the cable to one or the other of the wheels, and provides low friction cable operation for any cable direction.
    Type: Grant
    Filed: May 21, 2004
    Date of Patent: October 10, 2006
    Assignee: Space-Age Control, Inc.
    Inventors: Miriam H. McDaniel, Geoffrey D. Simpson
  • Patent number: 7118074
    Abstract: A tether system for providing thrust to or power subsystems of an artificial satellite in a low earth orbit. The tether has three main sections, an insulated section connected to the satellite, a conducting section connected to the insulating section for drawing in and releasing electrons from the space plasma and a non-conducting section for providing a tension to the other sections of the tether. An oxygen resistant coating is applied to the bare wire of the conducting section as well as the insulated wires of the insulated section that prevents breakdown during tether operations in the space plasma. The insulated and bare wire sections also surround a high tensile flexible polymer core to prevent any debris from breaking the tether during use.
    Type: Grant
    Filed: October 17, 2003
    Date of Patent: October 10, 2006
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Charles L. Johnson, Judy L. C. Ballance, Kenneth J. Welzyn, Jason A. Vaughn, Enrico Lorenzini, Peter S. Schuler
  • Patent number: 7116098
    Abstract: A limit and position sensing system includes a sensor assembly and an emitter. The sensor assembly includes first and second electrical conductors arranged in opposing parallel planes. The first electrical conductor is coiled outwardly from either end thereof in a clockwise fashion to form a first coil region and a second coil region. The second electrical conductor forms a single coil with portions of the single coil's rings lying between the first end and second end of the first electrical conductor being parallel to an axis of the first electrical conductor's plane. Ferromagnetic material is aligned with the first and second electrical conductors and spans beyond (a) the first and second ends of the first electrical conductor, and (b) the portions of the rings of the second electrical conductor's single coil that lie between the first end and second end of the first electrical conductor.
    Type: Grant
    Filed: February 16, 2006
    Date of Patent: October 3, 2006
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Dean C. Alhorn, David E. Howard, Dennis A. Smith
  • Patent number: 7114683
    Abstract: The invention presented here relates to a device in a spacecraft comprising a carrier rocket, a satellite and a detachable adapter (4) for connecting a satellite to the carrier rocket, where the adapter (4) comprises a wall structure (14, 15) for supporting the satellite on the carrier rocket, and is fixed at its lower rim to the carrier rocket and is fixed at its upper rim to the satellite. The device is characterised in that the adapter (4) is divided essentially across the longitudinal direction of the spacecraft and that both of the adapter parts (12, 13) are detachably connected to each other. The invention comprises the said adapter design and a method for separating the invented device.
    Type: Grant
    Filed: September 5, 2001
    Date of Patent: October 3, 2006
    Assignee: SAAB Ericsson Space AB
    Inventor: Lars Hall
  • Patent number: 7116568
    Abstract: A Series Connected Buck-Boost Regulator (SCBBR) that switches only a fraction of the input power, resulting in relatively high efficiencies. The SCBBR has multiple operating modes including a buck, a boost, and a current limiting mode, so that an output voltage of the SCBBR ranges from below the source voltage to above the source voltage.
    Type: Grant
    Filed: July 25, 2005
    Date of Patent: October 3, 2006
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Arthur G. Birchenough
  • Patent number: 7113820
    Abstract: Real time cardiac electrical data are received from a patient, manipulated to determine various useful aspects of the ECG signal, and displayed in real time in a useful form on a computer screen or monitor. The monitor displays the high frequency data from the QRS complex in units of microvolts, juxtaposed with a display of conventional ECG data in units of millivolts or microvolts. The high frequency data are analyzed for their root mean square (RMS) voltage values and the discrete RMS values and related parameters are displayed in real time. The high frequency data from the QRS complex are analyzed with imbedded algorithms to determine the presence or absence of reduced amplitude zones, referred to herein as “RAZs”. RAZs are displayed as “go, no-go” signals on the computer monitor. The RMS and related values of the high frequency components are displayed as time varying signals, and the presence or absence of RAZs may be similarly displayed over time.
    Type: Grant
    Filed: July 12, 2001
    Date of Patent: September 26, 2006
    Assignee: The United States of America as represented by the Administration of the National Aeronautics and Space Administration
    Inventors: Todd T. Schlegel, Jude L. DePalma, Saeed Moradi
  • Patent number: 7113265
    Abstract: Method and system for causing a powder sample in a sample holder to undergo at least one of three motions (vibration, rotation and translation) at a selected motion frequency in order to present several views of an individual grain of the sample. One or more measurements of diffraction, fluorescence, spectroscopic interaction, transmission, absorption and/or reflection can be made on the sample, using light in a selected wavelength region.
    Type: Grant
    Filed: March 17, 2004
    Date of Patent: September 26, 2006
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Philippe C. Sarrazin, David F. Blake
  • Patent number: 7108105
    Abstract: In a cable lift, with a single compartment or shaft (1) for housing a movable cage (2) and an apparatus (3), comprising at least one fixed winch (4) and a counterweight (5), for displacement of the cage (2), the counterweight (5) performs travel movements shorter than those of the cage (2) so that a part (1a) of the shaft (1) is always free to house the winch (4) therein. The latter, in particular, comprises a traction pulley (4c) with its axis (4a) parallel to a wall (1b) of the shaft (1), next to which it is arranged.
    Type: Grant
    Filed: August 1, 2001
    Date of Patent: September 19, 2006
    Assignee: SPACE LIFT S.R.L.
    Inventor: Eros Assirelli
  • Patent number: 7109725
    Abstract: A method and apparatus for testing integrated circuits by subjecting the circuits to an electromagnetic disturbance. A probe is provided, equipped with a horn cover designed to be applied to a printed circuit on which an integrated circuit is mounted. Within this horn cover, a core shield channels the electrical field that is deployed in a zone in which connections from the integrated circuit to the printed circuit that it carries are situated. The effectiveness of the electromagnetic interference injected in the integrated circuit is increased to the point that a true measurement of the resistance of this integrated circuit to the electromagnetic interferences may be carried out.
    Type: Grant
    Filed: December 7, 2005
    Date of Patent: September 19, 2006
    Assignee: European Aeronautic Defence and Space Company Eads France and Eads CCR Groupement d'Interet Economique
    Inventor: Olivier Maurice
  • Patent number: 7109287
    Abstract: Polyimides displaying low color in thin films, atomic oxygen resistance, vacuum ultraviolet radiation resistance, solubility in organic solvents in the imide form, high glass transition (Tg) temperatures, and high thermal stability are provided. The poly(amide acid)s, copoly(amide acid)s, polyimides and copolyimides are prepared by the reaction of stoichiometric ratios of an aromatic dianhydride with diamines which contain phenylphosphine oxide groups in polar aprotic solvents. Controlled molecular weight oligomeric (amide acid)s and imides can be prepared by offsetting the stoichiometry according to the Carothers equation using excess diamine and endcapping with aromatic anhydrides.
    Type: Grant
    Filed: November 8, 2004
    Date of Patent: September 19, 2006
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: John W. Connell, Joseph G. Smith, Jr., Paul M. Hergenrother, Kent A. Watson, Craig M. Thompson
  • Publication number: 20060201133
    Abstract: Pulsed detonation engines (PDEs), or various components thereof, such as the detonation chamber and/or nozzle, can be economically constructed from materials having low thermal stability, such as plastics, composites, and light metals. During operation, the intermittent injection and detonation of reactants produces a motive force (e.g., thrust) over relatively short intervals useful in orbit control and the like. The relatively short intervals of operation prevent temperatures of the PDE components from reaching temperatures that would result in their dimensional failure.
    Type: Application
    Filed: December 9, 2003
    Publication date: September 14, 2006
    Applicants: Science Applications International Corporation, U. S. Army Space and Missile Defense Command
    Inventors: Shmuel Eidelman, Dimitrios Lianos
  • Publication number: 20060201316
    Abstract: The invention relates to a composite structural part comprising pyrotechnic detonating rupture means. According to the invention, in addition to pyrotechnic separation means (16), the structural part (1) also comprises means (27) for absorbing the detonating shock produced by said pyrotechnic separation means (16).
    Type: Application
    Filed: October 11, 2004
    Publication date: September 14, 2006
    Applicant: EADS SPACE TRANSPORTATION SAS
    Inventor: Thomas Kister
  • Patent number: 7106502
    Abstract: A Microscope Imaging System (CMIS) with intelligent controls is disclosed that provides techniques for scanning, identifying, detecting and tracking microscopic changes in selected characteristics or features of various surfaces including, but not limited to, cells, spheres, and manufactured products subject to difficult-to-see imperfections. The practice of the present invention provides applications that include colloidal hard spheres experiments, biological cell detection for patch clamping, cell movement and tracking, as well as defect identification in products, such as semiconductor devices, where surface damage can be significant, but difficult to detect. The CMIS system is a machine vision system, which combines intelligent image processing with remote control capabilities and provides the ability to auto-focus on a microscope sample, automatically scan an image, and perform machine vision analysis on multiple samples simultaneously.
    Type: Grant
    Filed: February 4, 2005
    Date of Patent: September 12, 2006
    Assignee: The United States of America as represented by the Administrator of National Aeronautics and Space Administration
    Inventor: Mark McDowell