Patents Assigned to Space
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Publication number: 20050079115Abstract: The invention described herein involves a novel approach to the production of oxidation/reduction catalytic systems. The present invention serves to stabilize the tin oxide reducible metal-.oxide coating by co-incorporating at least another metal-oxide species, such as zirconium. In one embodiment, a third metal-oxide species is incorporated, selected from the group consisting of cerium, lanthanum, hafnium, and ruthenium. The incorporation of the additional metal oxide components serves to stabilize the active tin-oxide layer in the catalytic process during high-temperature operation in a reducing environment (e.g., automobile exhaust). Moreover, the additional metal oxides are active components due to their oxygen-retention capabilities. Together, these features provide a mechanism to extend the range of operation of the tin-oxide-based catalyst system for automotive applications, while maintaining the existing advantages.Type: ApplicationFiled: September 28, 2004Publication date: April 14, 2005Applicant: U.S.A. as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Jeffrey Jordan, David Schryer, Patricia Davis, Bradley Leighty, Anthony Watkins, Jacqueline Schryer, Donald Oglesby, Suresh Gulati, Jerry Summers
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Broadband communication systems and methods using low and high bandwidth request and broadcast links
Patent number: 6879808Abstract: Broadband data transmission systems and methods that provide point-to-multipoint broadcasting capability to implement Internet access and multimedia distribution services for a very large number of users. An exemplary system comprises a two-way communication link having at least one satellite, at least one user terminal that has two-way communication with the two-way communication link, and at least one gateway that has access to data and has two-way communication with the two-way communication link. The two-way communication link may comprise a low bandwidth two-way communication link, or a low bandwidth request link and high bandwidth data broadcast link. The high bandwidth link preferably broadcasts a wide area coverage beam to allows the requested information to be received by many terminals. The terminal and gateway may each include a cache. Software at the gateway operates to deliver requested data and related data to users using the user's request history and/or user profile.Type: GrantFiled: November 15, 2000Date of Patent: April 12, 2005Assignee: Space Systems/Loral, IncInventors: William D. Nations, David S. Puente, Robert E. Berry -
Patent number: 6879893Abstract: A monitoring system for a fleet of vehicles includes at least one data acquisition and analysis module (DAAM) mounted on each vehicle in the fleet, a control module on each vehicle in communication with each DAAM, and terminal module located remotely with respect to the vehicles in the fleet. Each DAAM collects/analyzes sensor data to generate analysis results that identify the state of a plurality of systems of the vehicle. Each vehicle's control module collects/analyzes the analysis results from each onboard DAAM to generate vehicle status results that identify potential sources of vehicle anomalies. The terminal module collects/analyzes the analysis results and vehicle status results transmitted from each control module from the fleet of vehicles to identify multiple occurrences of vehicle anomalies and multiple occurrences of those vehicle systems operating at a performance level that is unacceptable.Type: GrantFiled: September 30, 2003Date of Patent: April 12, 2005Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Stanley E. Woodard, Neil C. Coffey, Bryant D. Taylor, Keith L. Woodman
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Patent number: 6874126Abstract: Methods and apparatuses for controlling display of supplemental content on a computer screen are described. In one embodiment, a method for controlling display of supplemental content on a computer screen includes detecting that the supplemental content is displayed on the computer screen. The display of the supplemental content is controlled by a cursor position relative to a first predefined region. The method further includes triggering display of an interface element associated with the supplemental content when the cursor is positioned inside the predefined first region, defining a second region that covers at least a portion of the interface element and the current position of the cursor, and continuing the display of the supplemental content upon detecting that the cursor is positioned outside of the first region but within the second region.Type: GrantFiled: November 30, 2001Date of Patent: March 29, 2005Assignee: View Space TechnologiesInventor: Eugene Lapidous
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Patent number: 6873762Abstract: An apparatus and method for forming a Bragg grating on an optical fiber using a phase mask to diffract a beam of coherent energy and a lens combined with a pair of mirrors to produce two symmetrical virtual point sources of coherent energy in the plane of the optical fiber. The two virtual light sources produce an interference pattern along the optical fiber. In a further embodiment, the period of the pattern and therefore the Bragg wavelength grating applied to the fiber is varied with the position of the optical fiber relative the lens.Type: GrantFiled: April 8, 2002Date of Patent: March 29, 2005Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Ying Wang, Anup Sharma, Joseph Grant
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Patent number: 6869480Abstract: Methods are disclosed that provide for structures and techniques for the fabrication of ordered arrangements of crystallographically determined nanometer scale steps on single crystal substrates, particularly SiC. The ordered nanometer scale step structures are produced on the top surfaces of mesas by a combination of growth and etching processes. These structures, sometimes referred to herein as artifacts, are to enable step-height calibration, particularly suitable for scanning probe microscopes and profilometers, from less than one nanometer (nm) to greater than 10 nm, with substantially no atomic scale roughness of the plateaus on either side of each step.Type: GrantFiled: July 17, 2002Date of Patent: March 22, 2005Assignee: The United States of America as represented by the United States National Aeronautics and Space AdministrationInventors: Phillip B. Abel, J. Anthony Powell, Philip G. Neudeck
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Patent number: 6866752Abstract: A method for providing an ultra thin electrical circuit integral with a portion of a surface of an object, including using a focal Vacuum Arc Vapor Deposition device having a chamber, a nozzle and a nozzle seal, depressing the nozzle seal against the portion of the object surface to create an airtight compartment in the chamber and depositing one or more ultra thin film layer(s) only on the portion of the surface of the object, the layers being of distinct patterns such that they form the circuit.Type: GrantFiled: August 23, 2001Date of Patent: March 15, 2005Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Harry F. Schramm
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Patent number: 6867533Abstract: An electrostrictive polymer actuator comprises an electrostrictive polymer with a tailorable Poisson's ratio. The electrostrictive polymer is electroded on its upper and lower surfaces and bonded to an upper material layer. The assembly is rolled tightly and capped at its ends. In a membrane structure having a membrane, a supporting frame and a plurality of threads connecting the membrane to the frame, an actuator can be integrated into one or more of the plurality of threads. The electrostrictive polymer actuator displaces along its longitudinal axis, thereby affecting movement of the membrane surface.Type: GrantFiled: October 23, 2000Date of Patent: March 15, 2005Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Ji Su, Joycelyn S. Harrison
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Patent number: 6866098Abstract: System and methods 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: October 30, 2002Date of Patent: March 15, 2005Assignee: The United States of America as represented by the National Aeronautics and Space AdministrationInventors: G. Dickey Arndt, James R. Carl, Kent A. Byerly, B. Jon Amini
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Patent number: 6864473Abstract: A dynamic optical filtration system and method effectively blocks bright light sources without impairing view of the remainder of the scene. A sensor measures light intensity and position so that selected cells of a shading matrix may interrupt the view of the bright light source by a receptor. A beamsplitter may be used so that the sensor may be located away from the receptor. The shading matrix may also be replaced by a digital micromirror device, which selectively sends image data to the receptor.Type: GrantFiled: December 7, 2000Date of Patent: March 8, 2005Assignee: The United States of America as represented by the United States National Aeronautics and Space AdministrationInventors: Jean-Loup Chretien, Edward T. Lu
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Patent number: 6863712Abstract: A gas-liquid separator uses a helical passageway to impart a spiral motion to a fluid passing therethrough. The centrifugal fore 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 filtered through a gas-permeable, liquid-impervious membrane and discharged through a central passageway.Type: GrantFiled: September 25, 2002Date of Patent: March 8, 2005Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Steve R. Gonda, Yow-Min D. Tsao, Wenshan Lee
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Patent number: 6865208Abstract: Ultrafast directional beam switching is achieved using coupled VCSELs. This approach is demonstrated to achieve beam switching frequencies of 40 GHz and more and switching directions of about eight degrees. This switching scheme is likely to be useful for ultrafast optical networks at frequencies much higher than achievable with other approaches.Type: GrantFiled: June 10, 2002Date of Patent: March 8, 2005Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Peter M. Goorjian, Cun-Zheng Ning
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Patent number: 6860099Abstract: An injector for use with the rocket thruster has a plurality of fuel ports separated from a plurality of oxidizer ports. The oxidizer and fuel ports are paired together directing their respective fluids along a path with radial and tangential components so that the two fluids impinge at a predetermined spaced apart distance from the chamber wall of the combustion chamber at an impingement track. By providing the fuel at a steeper angle relative to the chamber walls than the oxidizer, the fuel can be utilized to provide a fuel rich zone near the chamber walls to assist in cooling the chamber walls during operation.Type: GrantFiled: January 9, 2003Date of Patent: March 1, 2005Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: George D. Xenofos, W. Neill Myers, Huu Trinh, R. Scott Michaels
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Patent number: 6862558Abstract: The present invention discloses a computer implemented signal analysis method through the Hilbert-Huang Transformation (HHT) for analyzing acoustical signals, which are assumed to be nonlinear and nonstationary. The Empirical Decomposition Method (EMD) and the Hilbert Spectral Analysis (HSA) are used to obtain the HHT. Essentially, the acoustical signal will be decomposed into the Intrinsic Mode Function Components (IMFs). Once the invention decomposes the acoustic signal into its constituting components, all operations such as analyzing, identifying, and removing unwanted signals can be performed on these components. Upon transforming the IMFs into Hilbert spectrum, the acoustical signal may be compared with other acoustical signals.Type: GrantFiled: February 13, 2002Date of Patent: March 1, 2005Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Norden E. Huang
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Patent number: 6859509Abstract: A PLL circuit uses a multiple frequency range PLL in order to phase lock input signals having a wide range of frequencies. The PLL includes a VCO capable of operating in multiple different frequency ranges and a divider bank independently configurable to divide the output of the VCO. A frequency detector detects a frequency of the input signal and a frequency selector selects an appropriate frequency range for the PLL. The frequency selector automatically switches the PLL to a different frequency range as needed in response to a change in the input signal frequency. Frequency range hysteresis is implemented to avoid operating the PLL near a frequency range boundary.Type: GrantFiled: February 4, 2000Date of Patent: February 22, 2005Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Robert David Koudelka
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Patent number: 6858197Abstract: Method and system for producing a selected pattern or array of at least one of a single wall nanotube and/or a multi-wall nanotube containing primarily carbon. A substrate is coated with a first layer (optional) of a first selected metal (e.g., Al and/or Ir) and with a second layer of a catalyst (e.g., Fe, Co, Ni and/or Mo), having selected first and second layer thicknesses provided by ion sputtering, arc discharge, laser ablation, evaporation or CVD. The first layer and/or the second layer may be formed in a desired non-uniform pattern, using a mask with suitable aperture(s), to promote growth of carbon nanotubes in a corresponding pattern. A selected heated feed gas (primarily CH4 or C2Hn with n=2 and/or 4) is passed over the coated substrate and forms primarily single wall nanotubes or multiple wall nanotubes, depending upon the selected feed gas and its temperature. Nanofibers, as well as single wall and multi-wall nanotubes, are produced using plasma-aided growth from the second (catalyst) layer.Type: GrantFiled: March 13, 2002Date of Patent: February 22, 2005Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Lance D. Delzeit
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Patent number: 6856073Abstract: A fluid-control electro-active device includes a piezo-diaphragm made from a ferroelectric material sandwiched by first and second electrode patterns configured to introduce an electric field into the ferroelectric material when voltage is applied thereto. The electric field originates at a region of the ferroelectric material between the first and second electrode patterns, and extends radially outward from this region of the ferroelectric material and substantially parallel to the plane of the ferroelectric material. The piezo-diaphragm deflects symmetrically about this region in a direction substantially perpendicular to the electric field. An annular region coupled to and extending radially outward from the piezo-diaphragm perimetrically borders the piezo-diaphragm. A housing is connected to the annular region and defines at least one fluid flow path therethrough with the piezo-diaphragm disposed therein.Type: GrantFiled: March 13, 2003Date of Patent: February 15, 2005Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Robert G. Bryant, Dennis C. Working
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Patent number: 6854510Abstract: A spacecraft, along with a spacecraft radiator system and spacecraft heat dissipation method are disclosed. The spacecraft comprises a body, a plurality of solar arrays, and the spacecraft radiator system. The spacecraft radiator system comprises first and second opposite facing payload radiators, first and second opposite facing deployable radiators, and one or more coupling or loop heat pipes cross coupling opposite facing payload and deployable radiators so that they function in tandem. By cross-coupling the opposite facing payload and deployable radiators, one of the two radiators acting in tandem is always in the shade during solstice seasons. Consequently, the solar load processed by the radiator system is minimized, thereby, increasing the thermal dissipation capability of the radiator system by approximately 15%.Type: GrantFiled: April 24, 2001Date of Patent: February 15, 2005Assignee: Space Systems/Loral, Inc.Inventors: Lenny Low, Susan Sebata
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Patent number: 6855433Abstract: This invention is a series of mechanically resilient polymeric films, comprising rod-coil block polyimide copolymers, which are doped with a lithium compound providing lithium ion conductivity, that are easy to fabricate into mechanically resilient films with acceptable ionic or protonic conductivity at a variety of temperatures. The copolymers consists of short-rigid polyimide rod segments alternating with polyether coil segments. The rods and coil segments can be linear, branched or mixtures of linear and branched segments. The highly incompatible rods and coil segments phase separate, providing nanoscale channels for ion conduction. The polyimide segments provide dimensional and mechanical stability and can be functionalized in a number of ways to provide specialized functions for a given application. These rod-coil black polyimide copolymers are particularly useful in the preparation of ion conductive membranes for use in the manufacture of fuel cells and lithium based polymer batteries.Type: GrantFiled: June 16, 2004Date of Patent: February 15, 2005Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Mary Ann B. Meador, James D. Kinder
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Patent number: 6856403Abstract: An apparatus and method for performing quality inspections on a test surface based on optically stimulated emission of electrons. In one embodiment, the apparatus comprises a device for producing optical radiation having a plurality of different spectrum lines, selecting at least one of the spectrum lines, and directing the selected spectrum line to the test surface, and circuitry for detecting a current of photoelectrons emitted from the test surface, generating a signal indicative of photoelectron current, and for indicating a condition of quality based on the generated signal indicative of the photoelectron current.Type: GrantFiled: September 11, 2003Date of Patent: February 15, 2005Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Christopher S. Welch, Daniel F. Perey