Patents Assigned to Space
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Patent number: 6673597Abstract: The present invention provides systems for growing two or three dimensional mammalian cells within a culture medium facilitated by an electromagnetic field, and preferably, a time varying electromagnetic field. The cells and culture medium are contained within a fixed or rotating culture vessel, and the electromagnetic field is emitted from at least one electrode. In one embodiment, the electrode is spaced from the vessel. The invention further provides methods to promote neural tissue regeneration by means of culturing the neural cells in the claimed system. In one embodiment, neuronal cells are grown within longitudinally extending tissue strands extending axially along and within electrodes comprising electrically conductive channels or guides through which a time varying electrical current is conducted, the conductive channels being positioned within a culture medium.Type: GrantFiled: February 28, 2001Date of Patent: January 6, 2004Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: David A. Wolf, Thomas J. Goodwin
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Patent number: 6672544Abstract: A spacecraft embedded in a reference frame rotating relative to inertial space. The spacecraft generally includes actuators for maneuvering the spacecraft with respect to the reference frame, an attitude measurement device that measures the pitch and roll attitude of the spacecraft with respect to the reference frame, a control device adapted to keep the roll and pitch angles of the spacecraft close to the commanded roll and pitch angles, and a harmonic torque estimator adapted to read the commanded angular velocity of the spacecraft relative to an inertial frame, read momentum wheel speeds, read known predicted external torques and combine angular velocity, measured wheel speed and known external torque to produce an estimated observable periodic torque.Type: GrantFiled: March 1, 2002Date of Patent: January 6, 2004Assignee: Space Systems/LoralInventors: Lawrence McGovern, Xen Price
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Patent number: 6672593Abstract: A variable pressure washer has two interlocking channel rings separated by a channel and retained by a captive set of fasteners. Within the channel between the rings are multiple rows of springs having at least two different spring moduli. The washer is particularly suited for use with a polar boss assembly secured to a bulkhead of a pressure vessel such as of propellent tank dome structure where the washer allows for the substantially uniform deflection of multiple O-rings as affected by the curved structure.Type: GrantFiled: December 20, 2001Date of Patent: January 6, 2004Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Stanley S. Smeltzer, III, Hector Estrada
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Patent number: 6675050Abstract: A method, simulation, and apparatus are provided that are highly suitable for treatment of benign prostatic hyperplasia (BPH). A catheter is disclosed that includes a small diameter disk loaded monopole antenna surrounded by fusion material having a high heat of fusion and a melting point preferably at or near body temperature. Microwaves from the antenna heat prostatic tissue to promote necrosing of the prostatic tissue that relieves the pressure of the prostatic tissue against the urethra as the body reabsorbs the necrosed or dead tissue. The fusion material keeps the urethra cool by means of the heat of fusion of the fusion material. This prevents damage to the urethra while the prostatic tissue is necrosed. A computer simulation is provided that can be used to predict the resulting temperature profile produced in the prostatic tissue.Type: GrantFiled: December 18, 2000Date of Patent: January 6, 2004Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: G. Dickey Arndt, James Carl, Phong Ngo
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Patent number: 6671590Abstract: Methods and systems for reducing noise generated by rotating blades of a tiltrotor aircraft. A rotor-blade pitch angle associated with the tiltrotor aircraft can be controlled utilizing a swashplate connected to rotating blades of the tiltrotor aircraft. One or more Higher Harmonic Control (HHC) signals can be transmitted and input to a swashplate control actuator associated with the swashplate. A particular blade pitch oscillation (e.g., four cycles per revolution) is thereafter produced in a rotating frame of reference associated with the rotating blades in response to input of an HHC signal to the swashplate control actuator associated with the swashplate to thereby reduce noise associated with the rotating blades of the tiltrotor aircraft. The HHC signal can be transmitted and input to the swashplate control actuator to reduce noise of the tiltrotor aircraft in response to a user input utilizing an open-loop configuration.Type: GrantFiled: April 30, 2002Date of Patent: December 30, 2003Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Mark D. Betzina, Khanh Q. Nguyen
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Patent number: 6669792Abstract: A process for making a cast article from an aluminum alloy includes first casting an article from an alloy having the following composition, in weight percent: Silicon (Si) 14.0-25.0 Copper (Cu) 5.5-8.0 Iron (Fe) 0-0.8 Magnesium (Mg) 0.5-1.5 Nickel (Ni) 0.05-1.2 Manganese (Mn) 0-1.0 Titanium (Ti) 0.05-1.2 Zirconium (Zr) 0.12-1.2 Vanadium (V) 0.05-1.2 Zinc (Zn) 0-0.9 Phosphorus (P) 0.001-0.1 Aluminum balance In this alloy the ration of Si:Mg is 15-35, and the ratio of Cu:Mg is 4-15. After an article is cast from the alloy, the cast article is aged at a temperature within the range of 400° F. to 500° F. for a time period within the range of four to 16 hours. It has been found especially advantageous if the cast article is first exposed to a solutionizing step prior to the aging step.Type: GrantFiled: March 2, 2001Date of Patent: December 30, 2003Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Jonathan A. Lee, Po-Shou Chen
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Patent number: 6667725Abstract: The present invention discloses and teaches apparatus for combining Radio Frequency (RF) technology with novel micro-inductor antennas and signal processing circuits for RF telemetry of real time, measured data, from microelectromechanical system (MEMS) sensors, through electromagnetic coupling with a remote powering/receiving device. Such technology has many applications, but is especially useful in the biomedical area.Type: GrantFiled: August 20, 2002Date of Patent: December 23, 2003Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Rainee N. Simons, Felix A. Miranda
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Patent number: 6667487Abstract: A containment apparatus for containing a cloud of charged particles comprises a cylindrical vacuum chamber having a longitudinal axis. Within the vacuum chamber is a containment region. A magnetic field is aligned with the longitudinal axis of the vacuum chamber. The magnetic field is time invariant and uniform in strength over the containment region. An electric field is also aligned with the longitudinal axis of the vacuum chamber and the magnetic field. The electric field is time invariant, and forms a potential well over the containment region. One or more means are disposed around the cloud of particles for inducing a rotating electric field internal to the vacuum chamber. The rotating electric field imparts energy to the charged particles within the containment region and compress the cloud of particles.Type: GrantFiled: January 31, 2003Date of Patent: December 23, 2003Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: William Herbert Sims, III, James Joseph Martin, Raymond A. Lewis
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Patent number: 6667826Abstract: A system for providing high-resolution color separation in electronic imaging. Comb drives controllably oscillate a red-green-blue (RGB) color strip filter system (or otherwise) over an electronic imaging system such as a charge-coupled device (CCD) or active pixel sensor (APS). The color filter is modulated over the imaging array at a rate three or more times the frame rate of the imaging array. In so doing, the underlying active imaging elements are then able to detect separate color-separated images, which are then combined to provide a color-accurate frame which is then recorded as the representation of the recorded image. High pixel resolution is maintained. Registration is obtained between the color strip filter and the underlying imaging array through the use of electrostatic comb drives in conjunction with a spring suspension system.Type: GrantFiled: March 1, 2002Date of Patent: December 23, 2003Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Frank T. Hartley, Anthony B. Hull
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Patent number: 6664298Abstract: 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.Type: GrantFiled: October 2, 2001Date of Patent: December 16, 2003Assignee: The United States of America as represented by the Administrator of the National Aeronautics & Space AdministrationInventors: Debra R. Reinhart, Christian Clausen, Cherie L. Geiger, Jacqueline Quinn, Kathleen Brooks
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Patent number: 6662572Abstract: There is provided a climate control system for a parked vehicle that includes a solar panel, thermostatic switch, fans, and thermoelectric coolers. The solar panel can serve as the sole source of electricity for the system. The system affords convenient installation and removal by including solar panels that are removably attached to the exterior of a vehicle. A connecting wire electrically connects the solar panels to a housing that is removably mounted to a partially opened window on the vehicle. The thermostatic switch, fans, and thermoelectric coolers are included within the housing. The thermostatic switch alternates the direction of the current flow through the thermoelectric coolers to selectively heat or cool the interior of the vehicle. The interior surface of the thermoelectric coolers are in contact with interior heat sinks that have air circulated across them by an interior fan.Type: GrantFiled: December 30, 2002Date of Patent: December 16, 2003Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Richard T. Howard
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Patent number: 6660110Abstract: A heat treatment assembly and heat treatment methods are disclosed for producing different microstructures in the bore and rim portions of nickel-based superalloy disks, particularly suited for gas turbine applications. The heat treatment assembly is capable of being removed from the furnace and disassembled to allow rapid fan or oil quenching of the disk. For solutioning heat treatments of the disk, temperatures higher than that of this solvus temperature of the disk are used to produce coarse grains in the rim of each disk so as to give maximum creep and dwell crack resistance at the rim service temperature. At the same time, solution temperature lower than the solvus temperature of the disk are provided to produce fine grain in the bore of the disk so as to give maximum strength and low cycle fatigue resistance.Type: GrantFiled: April 8, 2002Date of Patent: December 9, 2003Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: John Gayda, Timothy P. Gabb, Peter T. Kantzos
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Patent number: 6660165Abstract: The present invention is to provide a method for regenerating inorganic porous particles, a method for purifying water and a continuous water purification device, which can be easily applied as a recycling system of water in special environments such as space environment, by safely removing impurities contained in water and water vapor with a usage of a compact facility without using any chemicals. The method for regenerating inorganic porous particles is characterized in that adsorbed products such as ammonia and/or amines, are reduced by heating to 100-200° C. under a reduced pressure of 10 Pa or less. The method for purifying water and the continuous water purification device are characterized in that a dense membrane having cationic groups and/or a composite membrane in which a hydrophilic membrane is layered on a surface of a hydrophobic porous membrane is used as a permeable membrane are used as a permeable membrane.Type: GrantFiled: October 30, 2000Date of Patent: December 9, 2003Assignees: Japan, represented by Director General of Forestry and Forest Products Research Institute Forestry Agency, Ministry of Argriculture Forestry and Fisheries, The National Space Development Agency of Japan, The Japan Space ForumInventors: Yasuhiko Hirabayashi, Nobukazu Onishi
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Patent number: 6660927Abstract: Solar panel includes solar cells affixed to one or more sheet elements and a frame for supporting the sheet elements, wherein the frame is provided with attachment members for attaching the sheet elements to the frame. The attachment members include one or more pretensioned strings, the sheet elements being attached to the strings. Preferably, the sheet elements are composed of flexible material and are attached to the string in a corrugated shape, wherein the sheet elements are provided with at least one row of apertures for weaving a string through successive apertures of the row.Type: GrantFiled: June 27, 2002Date of Patent: December 9, 2003Assignee: Dutch Space B.V.Inventor: Robert Zwanenburg
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Patent number: 6658329Abstract: A video guidance sensor system for use in automated docking of a chase vehicle with a target vehicle wherein the chase vehicle includes a laser rangefinder that uses pulse or phase time of flight measurement to measure distance. The laser rangefinder includes a diode laser pulse or phase driver that produces an output signal to a timing element and simultaneously operates a laser diode. The laser diode produces an intense light beam of a predetermined wavelength which is directed to retroreflectors that are positioned on a passive target. The laser rangefinder includes an avalanche photodetector that produces a corresponding output signal when detecting light reflected from the retroreflectors. The timing element measures a time interval between the output of the laser diode and the detection of light and supplies a corresponding output signal to a computer in order to determine the range of the target vehicle relative to the chase vehicle.Type: GrantFiled: May 2, 2002Date of Patent: December 2, 2003Assignee: The United States of America as represented by the United States National Aeronautics and Space AdministrationInventors: Richard T. Howard, Albert S. (Nick) Johnston, Michael L. Book, Thomas C. Bryan
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Publication number: 20030218210Abstract: In a power MOSFET, on an N+ drain layer 21 as a substrate, a second N base layer 3 and a first N− base layer 22 are deposited in the order by epitaxial growth. In a surface portion of the layer 22, there are selectively formed a P base region 23, in a surface portion of which an N+ source region 24 is selectively formed. On a channel region in the P base region 23, a gate electrode 26 is formed with a gate insulator film 25 held between. A source electrode 27 and a drain electrode 28 are formed on the N+ source region 24 and on the back of the substrate, respectively. The layer 3 is made to have a thickness equal to or more than ¼ of that of the first N− base layer 22, and an averaged impurity concentration between 1×1015/cm3 and 3×1017/cm3.Type: ApplicationFiled: February 14, 2003Publication date: November 27, 2003Applicants: Fuji Electric Co., Ltd., National Space Development Agency of JapanInventors: Saburo Tagami, Takashi Kobayashi, Fumiaki Kirihata, Satoshi Kuboyama
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Publication number: 20030220169Abstract: A joint may have a multi-stage planetary gearbox between the stationary housing and the rotary housing. To accommodate different gear ratios, the rotary housing may be joined to the stationary housing by a releasable attachment. This allows portions of the planetary gearbox to be replaced so that, for instance, the last stage may be chosen as either a simple or compound differential planetary stage. To allow for different capacities, a quotient of a sum of all teeth of a sun gear of a stage and of the ring gear with which the planetary gears of the stage mesh to both the number three and the number four yields an integer. In this way, the stage may be provided with either three or four planetary gears. The gearbox may have a ring gear common to a plurality of simple planetary stages. Where the final stage is a simple planetary stage, the carrier may be provided with a flange extending around, and bearing mounted to, the common ring gear.Type: ApplicationFiled: May 24, 2002Publication date: November 27, 2003Applicant: MacDonald Dettwiler Space and Advanced Robotics Ltd.Inventor: Robert D. Norman
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Patent number: 6653259Abstract: A method of fabricating large bulk high temperature superconducting articles which comprises the steps of selecting predetermined sizes of crystalline superconducting materials and mixing these specific sizes of particles into a homogeneous mixture which is then poured into a die. The die is placed in a press and pressurized to predetermined pressure for a predetermined time and is heat treated in the furnace at predetermined temperatures for a predetermined time. The article is left in the furnace to soak at predetermined temperatures for a predetermined period of time and is oxygenated by an oxygen source during the soaking period.Type: GrantFiled: December 20, 2001Date of Patent: November 25, 2003Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Ronald J. Koczor, Robert A. Hiser
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Patent number: 6651481Abstract: Embodiments of apparatuses and methods are provided that use light sources instead of sound sources for characterizing and calibrating sensors for measuring small pressures to mitigate many of the problems with using sound sources. In one embodiment an apparatus has a light source for directing a beam of light on a sensing surface of a pressure sensor for exerting a force on the sensing surface. The pressure sensor generates an electrical signal indicative of the force exerted on the sensing surface. A modulator modulates the beam of light. A signal processor is electrically coupled to the pressure sensor for receiving the electrical signal.Type: GrantFiled: October 12, 2001Date of Patent: November 25, 2003Assignee: The United States of America as represented by the United States National Aeronautics and Space AdministrationInventor: Robert C Youngquist
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Patent number: 6651739Abstract: System and methods are disclosed for transmitting and receiving electromagnetic pulses through a geological formation. A preferably programmable transmitter having an all-digital portion in a preferred embodiment may be operated at frequencies below 1 MHz without loss of target resolution by transmitting and over sampling received long PN codes. A gated and stored portion of the received signal may be correlated with the PN code to determine distances of interfaces within the geological formation, such as the distance of a water interfaces from a wellbore. The received signal is oversampled preferably at rates such as five to fifty times as high as a carrier frequency. In one method of the invention, an oil well with multiple production zones may be kept in production by detecting an approaching water front in one of the production zones and shutting down that particular production zone thereby permitting the remaining production zones to continue operating.Type: GrantFiled: February 21, 2001Date of Patent: November 25, 2003Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: G. Dickey Arndt, James R. Carl, Kent A. Byerly, B. Jon Amini