Patents Assigned to Space
  • Patent number: 7040804
    Abstract: Two conductive solid materials with their respective different compositions are joined in parallel with a gravity direction thereof, and then, heated and melted under static magnetic field orthogonal to the gravity direction to form two conductive melts with their respective different compositions. Then, the conductive melts are maintained for a predetermined period of time under the static magnetic field, and cooled and solidified.
    Type: Grant
    Filed: June 30, 2003
    Date of Patent: May 9, 2006
    Assignee: The Institute of Space and Astronautical Science
    Inventors: Yuko Inatomi, Kazuhiko Kuribayashi
  • Patent number: 7040319
    Abstract: Method and apparatus are disclosed for monitoring an oxygen partial pressure in an air mask and providing a tactile warning to the user. The oxygen partial pressure in the air mask is detected using an electrochemical sensor, the output signal from which is provided to a comparator. The comparator compares the output signal with a preset reference value or range of values representing acceptable oxygen partial pressures. If the output signal is different than the reference value or outside the range of values, the air mask is vibrated by a vibrating motor to alert the user to a potentially hypoxic condition.
    Type: Grant
    Filed: February 22, 2002
    Date of Patent: May 9, 2006
    Assignee: The United States of America as represented by the National Aeronautics and Space Administration
    Inventors: Mark E. Kelly, Donald R. Pettit
  • Patent number: 7042008
    Abstract: An image sensor has a CdTe plate, a plurality of hole-type electrodes, and a voltage-applying unit. The hole-type electrodes are arranged at predetermined intervals in the direction of thickness. The voltage-applying unit applies a voltage to the hole-type electrodes. One of the electrodes is not adjacent to any other electrode and is used as an anode. The remaining electrodes are used as cathodes. A sensor-element array is provided on the detecting surface of the image sensor. The array comprises a plurality of sensor elements arranged in the form of a matrix. Each sensor element comprises an anode, a plurality of cathodes, and CdTe lying between the anode and the cathodes.
    Type: Grant
    Filed: August 8, 2003
    Date of Patent: May 9, 2006
    Assignees: Mitsubishi Heavy Industries, Ltd., Japan as represented by the Director-General of the Institute of Space and Astronautical Science
    Inventors: Yoshikatsu Kuroda, Tadayuki Takahashi, Yasushi Mizuno
  • Patent number: 7042199
    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 28, 2003
    Date of Patent: May 9, 2006
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Arthur G. Birchenough
  • Publication number: 20060090453
    Abstract: An injection head for a liquid-propelled rocket engine has a plurality of first and second injection bores for injecting jets of first and second propellant constituents, respectively, into the combustion chamber of a rocket engine, with mutual mixing of propellant constituents. The first injection bores are provided for injecting jets of the first propellant constituent with a high impulse, and the second injection bores are provided for injecting propellant jets of the second propellant constituent with a low impulse. In addition, the first and second injection bores are mutually arranged such that an admixing of the second propellant constituent to the first propellant constituent takes place under an ejector effect of the propellant jets of the first propellant constituent leaving the first injection bores.
    Type: Application
    Filed: November 4, 2004
    Publication date: May 4, 2006
    Applicant: EADS Space Transportation GmbH
    Inventors: Wolfgang Mueller, Christoph Tscherwitschke
  • Patent number: 7037946
    Abstract: A zero-valent metal emulsion is used to dehalogenate solvents, such as pooled dense non-aqueous phase liquids (DNAPLs), including trichloroethylene (TCE). The zero-valent metal emulsion contains zero-valent metal particles, a surfactant, oil and water. The preferred zero-valent metal particles are nanoscale and microscale zero-valent iron particles.
    Type: Grant
    Filed: October 31, 2003
    Date of Patent: May 2, 2006
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Debra R. Reinhart, Christian Clausen, Cherie L. Geiger, Jacqueline Quinn, Kathleen Brooks
  • Patent number: 7038358
    Abstract: An electro-active transducer includes a ferroelectric material sandwiched by first and second electrode patterns. When the device is used as an actuator, the first and second electrode patterns are configured to introduce an electric field into the ferroelectric material when voltage is applied to the electrode patterns. When the device is used as a sensor, the first and second electrode patterns are configured to introduce an electric field into the ferroelectric material when the ferroelectric material experiences deflection in a direction substantially perpendicular thereto. In each case, the electrode patterns are designed to cause the electric field to: i) originate at a region of the ferroelectric material between the first and second electrode patterns, and ii) extend radially outward from the region of the ferroelectric material (at which the electric field originates) and substantially parallel to the ferroelectric material's plane.
    Type: Grant
    Filed: January 16, 2003
    Date of Patent: May 2, 2006
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Robert G. Bryant, Robert L. Fox
  • Patent number: 7039207
    Abstract: An entertainment and pacification system for use with a child car seat has speakers mounted in the child car seat with a plurality of audio sources and an anti-noise audio system coupled to the child car seat. A controllable switching system provides for, at any given time, the selective activation of i) one of the audio sources such that the audio signal generated thereby is coupled to one or more of the speakers, and ii) the anti-noise audio system such that an ambient-noise-canceling audio signal generated thereby is coupled to one or more of the speakers. The controllable switching system can receive commands generated at one of first controls located at the child car seat and second controls located remotely with respect to the child car seat with commands generated by the second controls overriding commands generated by the first controls.
    Type: Grant
    Filed: March 18, 2003
    Date of Patent: May 2, 2006
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Susan Vinz Elrod, Richard W. Dabney
  • Publication number: 20060084752
    Abstract: An electroactive sensing or actuating material comprises a composite made from a polymer with polarizable moieties and an effective amount of carbon nanotubes incorporated in the polymer for a predetermined electomechanical operation of the composite when such composite is affected by an external stimulus. In another embodiment, the composite comprises a third component of micro-sized to nano-sized particles of an electroactive ceramic that is also incorporated in the polymer matrix. The method for making the three-phase composite comprises either incorporating the carbon nanotubes in the polymer matrix before incorporation of the particles of ceramic or mixing the carbon nanotubes and particles of ceramic together in a solution before incorporation in the polymer matrix.
    Type: Application
    Filed: March 3, 2005
    Publication date: April 20, 2006
    Applicant: USA as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Zoubeida Ounaies, Cheol Park, Joycelyn Harrison, Nancy Holloway, Gregory Draughon
  • Patent number: 7028953
    Abstract: A spacecraft heat dissipation method, and a spacecraft having an improved thermal radiator system that uses two-sided deployable thermal radiators that dissipates heat from both front and back surfaces thereof. The use of the two-sided deployable thermal radiators enables the thermal radiator system to have approximately 50% more heat dissipating capability than a system with just one surface exposed to dissipate heat. The spacecraft includes a body, one or more solar arrays, and the present radiator system which comprises opposite facing fixed payload radiators that are thermally coupled to selected ones of the deployable radiators by way of heat pipes. In an exemplary method a spacecraft is configured to have a body, one or more solar arrays opposite facing fixed payload radiators, and one or more two-sided deployable radiators selectively coupled to the fixed payload radiators. The spacecraft is launched into orbit.
    Type: Grant
    Filed: November 11, 2001
    Date of Patent: April 18, 2006
    Assignee: Space Systems/Loral
    Inventors: Susan Sebata, Lenny Low
  • Patent number: 7031503
    Abstract: A system is provided for automatically producing a temporally processed image which includes a storage unit which stores thereon a plurality of radiographic images, the plurality of radiographic images being taken at different points of time. The system is provided with an image input unit for capturing a new radiographic image so as to store the captured new radiographic image on the storage unit and an automatic maintenance control unit for automatically producing, in response to the capture of the new radiographic image, information specifying a predetermined number of pairs of the radiographic images. The specified pairs of the radiographic images includes the captured radiographic image. The system is further provided with an automatic producing unit for automatically producing a specified number of temporally processed images according to the information produced by the automatic maintenance control unit.
    Type: Grant
    Filed: October 25, 2001
    Date of Patent: April 18, 2006
    Assignee: Mitsubishi Space Software Co., Ltd.
    Inventors: Osamu Ozaki, Hironori Saki
  • Publication number: 20060070450
    Abstract: A system and method are provided for detecting cracks and their location in a structure. A circuit coupled to a structure has capacitive strain sensors coupled sequentially and in parallel to one another. When excited by a variable magnetic field, the circuit has a resonant frequency that is different for unstained and strained states. In terms of strained states, the resonant frequency is indicative of a region of the circuit that is experiencing strain induced by strain in a region of the structure in proximity to the region of the circuit. An inductor is electrically coupled to one end of each circuit. A magnetic field response recorder wirelessly transmits the variable magnetic field to the inductor and senses the resonant frequency of the circuit so-excited by the variable magnetic field.
    Type: Application
    Filed: September 12, 2005
    Publication date: April 6, 2006
    Applicant: U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Stanley Woodard, Qamar Shams
  • Patent number: 7023118
    Abstract: In a rotor assembly having a rotor supported for rotation by magnetic bearings, a processor controlled by software or firmware controls the generation of force vectors that position the rotor relative to its bearings in a “bounce” mode in which the rotor axis is displaced from the principal axis defined between the bearings and a “tilt” mode in which the rotor axis is tilted or inclined relative to the principal axis. Waveform driven perturbations are introduced to generate force vectors that excite the rotor in either the “bounce” or “tilt” modes.
    Type: Grant
    Filed: March 12, 2003
    Date of Patent: April 4, 2006
    Assignee: The United States of America as represented by the Administrator of National Aeronautics and Space Administration
    Inventor: Carlos R. Morrison
  • Patent number: 7017812
    Abstract: A variable distance angular symbology reader utilizes at least one light source to direct light through a beam splitter and onto a target. A target may be angled relative to the impinging light beam up to and maybe even greater than 45°. A reflected beam from the target passes through the beam splitter and is preferably directed 90° relative to the light source through a telecentric lens to a scanner which records an image of the target such as a direct part marking code.
    Type: Grant
    Filed: November 26, 2003
    Date of Patent: March 28, 2006
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Harry F. Schramm, Jr., Eric L. Corder
  • Patent number: 7019847
    Abstract: A biosensor embodying the invention includes a sensing volume having an array of pores sized for immobilizing a first biological entity tending to bind to a second biological entity in such a manner as to change an index of refraction of the sensing volume. The biosensor further includes a ring interferometer, one volumetric section of the ring interferometer being the sensing volume, a laser for supplying light to the ring interferometer, and a photodetector for receiving light from the interferometer.
    Type: Grant
    Filed: December 9, 2003
    Date of Patent: March 28, 2006
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Gregory Bearman, David Cohen
  • Publication number: 20060060723
    Abstract: A method of controlling a shear layer for a fluid dynamic body introduces first periodic disturbances into the fluid medium at a first flow separation location. Simultaneously, second periodic disturbances are introduced into the fluid medium at a second flow separation location. A phase difference between the first and second periodic disturbances is adjusted to control flow separation of the shear layer as the fluid medium moves over the fluid dynamic body.
    Type: Application
    Filed: September 22, 2005
    Publication date: March 23, 2006
    Applicant: Administrator of the National Aeronautics and Space Administration
    Inventor: David Greenblatt
  • Publication number: 20060062950
    Abstract: A composite laminate material is supported during the roll press processing thereof by an assembly having: first and second perforated films disposed adjacent to first and second opposing surfaces of a mixture of uncured resin and fibers defining the composite laminate material, a gas permeable encasement surrounding the mixture and the first and second films, a gas impervious envelope sealed about the gas permeable encasement, and first and second rigid plates clamped about the gas impervious envelope.
    Type: Application
    Filed: September 23, 2004
    Publication date: March 23, 2006
    Applicant: USA as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Luke Catella
  • Publication number: 20060061396
    Abstract: A method and system utilize a processor's digital timer and two interrupts to form a frequency multiplier. The first interrupt's processing time window is definable by a first number of counts C1 of the digital timer while the second interrupt's processing time window is definable by a second number of counts C2 of the digital timer. A count value CV utilized by the system/method is based on a desired frequency multiplier N, the timer clock rate, and the time required for one cycle of an input signal. The first interrupt is triggered upon completion of one cycle of the input signal at which point the processing time window associated therewith begins. The second interrupt is triggered each time the timer's overflow signal is generated at which point the processing time window associated with the second interrupt begins.
    Type: Application
    Filed: September 17, 2004
    Publication date: March 23, 2006
    Applicant: U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Daniel Palumbo
  • Publication number: 20060063848
    Abstract: A fully imidized, solvent-free polyimide foam having excellent mechanical, acoustic, thermal, and flame resistant properties is produced. A first solution is provided, which includes one or more aromatic dianhydrides or derivatives of aromatic dianhydrides, and may include one or more aromatic diamines, dissolved in one or more polar solvents, along with an effective amount of one or more blowing agents. This first solution may also advantageously include effective amounts respectively of one or mores catalysts, one or more surfactants, and one or more fire retardants. A second solution is also provided which includes one or more isocyanates. The first and second solutions are rapidly and thoroughly mixed to produce an admixture, which is allowed to foam—in an open container, or in a closed mold—under ambient conditions to completion produce a foamed product. This foamed product is then cured by high frequency electromagnetic radiation, thermal energy, or a combination thereof.
    Type: Application
    Filed: May 5, 2005
    Publication date: March 23, 2006
    Applicant: U.S.A. as represented by the Administrator of the National Aeronautics & Space Administration
    Inventors: Juan Vazquez, Roberto Cano, Brian Jensen, Erik Weiser
  • Publication number: 20060059888
    Abstract: Control and/or drive device for a flying body for ejecting hot gas streams of a combusted fuel combination of at least a first and second component. Device includes a first hollow chamber body structured and arranged to contain first component, a second hollow chamber body structured and arranged to contain second component, a controllable fuel valve arranged between first hollow chamber body and second hollow chamber body to control feed of first component to second hollow chamber body, and a plurality of outlets structured and arranged to eject respective hot gas streams for influencing a flight path of flying body. Second hollow chamber body is formed as a combustion chamber for combusting the at least first and second components within second hollow chamber body to generate respective hot gas streams, and plurality of outlets are connected to the second hollow chamber body.
    Type: Application
    Filed: September 19, 2005
    Publication date: March 23, 2006
    Applicant: EADS SPACE TRANSPORTATION GmbH
    Inventor: Thomas Maier