Patents Assigned to NASA
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Publication number: 20100097058Abstract: A carbon nanotube magnetometer including a system and method of making the same that includes a single-walled carbon nanotube network formed on a substrate. Electrodes are deposited on opposite ends of the network and a magnetic needle is deposited on the network between the electrodes. A trench is formed under the network in the substrate to facilitate movement of the needle.Type: ApplicationFiled: June 14, 2007Publication date: April 22, 2010Applicant: NASA HeadquartersInventor: Stephanie A. Getty
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Patent number: 7702427Abstract: Method and system for evaluating and implementing air traffic management tools and approaches for managing and avoiding an air traffic incident before the incident occurs. The invention provides flight plan routing and direct routing or wind optimal routing, using great circle navigation and spherical Earth geometry. The invention provides for aircraft dynamics effects, such as wind effects at each altitude, altitude changes, airspeed changes and aircraft turns to provide predictions of aircraft trajectory (and, optionally, aircraft fuel use). A second system provides several aviation applications using the first system. These applications include conflict detection and resolution, miles-in trail or minutes-in-trail aircraft separation, flight arrival management, flight re-routing, weather prediction and analysis and interpolation of weather variables based upon sparse measurements.Type: GrantFiled: July 30, 2004Date of Patent: April 20, 2010Assignee: The United States of America as represented by the National Aeronautics and Space Administration (NASA)Inventors: Banavar Sridhar, Kapil S. Sheth, Gano Broto Chatterji, Karl D. Bilimoria, Shon Grabbe, John F. Schipper
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Publication number: 20100090885Abstract: A digital radar system includes a transmitter, the transmitter configured to transmit a signal; a receiver, the receiver configured to receive a return signal; and two analog to digital conversion (ADC) units, the ADC units configured to digitize the return signal at a rate higher than a Nyquist rate for the transmitted signal. A method of operating a digital radar includes transmitting a signal via a transmitter; receiving a return signal via a receiver; and digitizing the return signal by two analog to digital conversion (ADC) units at a rate higher than a Nyquist rate for the transmitted signal.Type: ApplicationFiled: September 8, 2009Publication date: April 15, 2010Applicant: NASA HQ'sInventor: UDAYAN MALLIK
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Patent number: 7698274Abstract: Method and system for providing selective access to different portions of a database by different subgroups of database users. Where N users are involved, up to 2N?1 distinguishable access subgroups in a group space can be formed, where no two access subgroups have the same members. Two or more members of a given access subgroup can edit, substantially simultaneously, a document accessible to each member.Type: GrantFiled: September 22, 2004Date of Patent: April 13, 2010Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration (NASA)Inventors: David A. Maluf, Yuri O. Gawdiak
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Publication number: 20100053634Abstract: A method of aligning an array of mirrors and computer program product therefor. The method may be used to align mirrors in a sparse aperture telescope system, e.g., a spaced based imaging interferometer. An image projected onto mirrors in an array of mirrors is reflected onto a sensor, where a point spread function (PSF) is collected from a pair of mirrors. A spatial image is extracted from PSF sidebands and a difference (e.g., piston difference) is determined for the pair of mirrors from the spatial image. Tip and tilt are determined for the pair of mirrors from spatial image characteristics.Type: ApplicationFiled: August 26, 2008Publication date: March 4, 2010Applicant: NASA HeadquartersInventor: Richard G. Lyon
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Patent number: 7672969Abstract: A computer-based system for configuring and displaying information on changes in, and present status of, a collection of events associated with a project. Classes of icons for decision events, configurations and feedback mechanisms, and time lines (sequential and/or simultaneous) for related events are displayed. Metadata for each icon in each class is displayed by choosing and activating the corresponding icon. Access control (viewing, reading, writing, editing, deleting, etc.) is optionally imposed for metadata and other displayed information.Type: GrantFiled: August 25, 2006Date of Patent: March 2, 2010Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration (NASA)Inventors: Yuri O. Gawdiak, Mohana M. Gurram, David A. Maluf, Luis A. Mederos
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Patent number: 7666939Abstract: Dispersions of carbon nanotubes exhibiting long term stability are based on a polymer matrix having moieties therein which are capable of a donor-acceptor complexation with carbon nanotubes. The carbon nanotubes are introduced into the polymer matrix and separated therein by standard means. Nanocomposites produced from these dispersions are useful in the fabrication of structures, e.g., lightweight aerospace structures.Type: GrantFiled: May 11, 2006Date of Patent: February 23, 2010Assignees: National Institute of Aerospace Associates, The United States of America as represented by the Administrator of NASAInventors: Kristopher Eric Wise, Cheol Park, Emilie J. Siochi, Joycelyn S. Harrison, Peter T. Lillehei, Sharon E. Lowther
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Patent number: 7662459Abstract: A thermal protection system for atmospheric entry of a vehicle, the system including a honeycomb structure with selected cross sectional shapes that receives and holds thermally cured thermal protection (TP) blocks that have corresponding cross sectional shapes. Material composition for TP blocks in different locations can be varied to account for different atmospheric heating characteristics at the different locations. TP block side walls may be attached to all, or to less than all, the corresponding honeycomb structure side walls.Type: GrantFiled: July 17, 2008Date of Patent: February 16, 2010Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration (NASA)Inventor: Peter T. Zell
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Patent number: 7655145Abstract: Method and system for processing of a liquid (“contaminant liquid”) containing water and containing urine and/or other contaminants in a two step process. Urine, or a contaminated liquid similar to and/or containing urine and thus having a relatively high salt and urea content is passed through an activated carbon filter to provide a resulting liquid, to remove most of the organic molecules. The resulting liquid is passed through a semipermeable membrane from a membrane first side to a membrane second side, where a fortified drink having a lower water concentration (higher osmotic potential) than the resulting liquid is positioned. Osmotic pressure differential causes the water, but not most of the remaining inorganic (salts) contaminant(s) to pass through the membrane to the fortified drink. Optionally, the resulting liquid is allowed to precipitate additional organic molecules before passage through the membrane.Type: GrantFiled: September 28, 2006Date of Patent: February 2, 2010Assignee: United States Government as represented by the Administrator of the National Aeronautics and Space Administration (NASA)Inventors: Sherwin J. Gormly, Michael T. Flynn
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Patent number: 7650232Abstract: Method and system for analyzing and processing information on one or more aircraft flight paths, using a four-dimensional coordinate system including three Cartesian or equivalent coordinates (x, y, z) and a fourth coordinate ? that corresponds to a distance estimated along a reference flight path to a nearest reference path location corresponding to a present location of the aircraft. Use of the coordinate ?, rather than elapsed time t, avoids coupling of along-track error into aircraft altitude and reduces effects of errors on an aircraft landing site. Along-track, cross-track and/or altitude errors are estimated and compared with a permitted error bounding space surrounding the reference flight path.Type: GrantFiled: September 22, 2005Date of Patent: January 19, 2010Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration (NASA)Inventor: Russell A. Paielli
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Patent number: 7590606Abstract: A system that allows a team of geographically dispersed users to collaboratively analyze a mishap event. The system includes a reconfigurable ontology, including instances that are related to and characterize the mishap, a semantic network that receives, indexes and stores, for retrieval, viewing and editing, the instances and links between the instances, a network browser interface for retrieving and viewing screens that present the instances and links to other instances and that allow editing thereof, and a rule-based inference engine, including a collection of rules associated with establishment of links between the instances. A possible conclusion arising from analysis of the mishap event may be characterized as one or more of: not a credible conclusion; an unlikely conclusion; a credible conclusion; conclusion needs analysis; conclusion needs supporting data; conclusion proposed to be closed; and an un-reviewed conclusion.Type: GrantFiled: November 5, 2003Date of Patent: September 15, 2009Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration (NASA)Inventors: Richard M. Keller, Tina L. Panontin, Robert E. Carvalho, Ian Sturken, James F. Williams, Shawn R. Wolfe, Yuri O. Gawdiak
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Patent number: 7574357Abstract: Method and system for generating electromyographic or sub-audible signals (“SAWPs”) and for transmitting and recognizing the SAWPs that represent the original words and/or phrases. The SAWPs may be generated in an environment that interferes excessively with normal speech or that requires stealth communications, and may be transmitted using encoded, enciphered or otherwise transformed signals that are less subject to signal distortion or degradation in the ambient environment.Type: GrantFiled: June 24, 2005Date of Patent: August 11, 2009Assignee: The United States of America as represented by the Admimnistrator of the National Aeronautics and Space Administration (NASA)Inventors: C. Charles Jorgensen, Bradley J. Betts
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Patent number: 7529633Abstract: Method and system for determining chemical composition of a single-component or multiple-component gas, using a discharge holdoff mechanism. A voltage difference V between two spaced apart electrodes is brought to a selected value and held, the holdoff time interval ?t(V;ho) required before gas discharge occurs is measured, and the associated electrical current or cumulative electrical charge is measured. As the voltage difference V increases, the time interval length ?t(V;ho) decreases monotonically. Particular voltage values, V? and V0, correspond to initial appearance of discharge (?t??) and prompt discharge (?t?0). The values V? and V0 and the rate of decrease of ?t(V;ho) and/or the rate of increase of current or cumulative charge with increasing V are characteristic of one or more gas components present.Type: GrantFiled: August 5, 2005Date of Patent: May 5, 2009Assignee: The United States of America as represented by the National Aeronautics and Space Administration (NASA)Inventors: John F. Schipper, Jing Li
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Publication number: 20090101557Abstract: A device for producing medical grade water in spacecrafts has a heat exchange unit which initially heats a water supply before being channeled to a membrane filter module which separates the water supply into liquid retentate and purified gaseous permeate.Type: ApplicationFiled: September 18, 2006Publication date: April 23, 2009Applicant: NASAInventor: Chung-Yi A. Tsai
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Patent number: 7510802Abstract: A thin-film electrode for a bio-nanobattery is produced by consecutively depositing arrays of a ferritin protein on a substrate, employing a spin self-assembly procedure. By this procedure, a first ferritin layer is first formed on the substrate, followed by building a second, oppositely-charged ferritin layer on the top of the first ferritin layer to form a bilayer structure. Oppositely-charged ferritin layers are subsequently deposited on top of each other until a desired number of bilayer structures is produced. An ordered, uniform, stable and robust, thin-film electrode material of enhanced packing density is presented, which provides optimal charge density for the bio-nanobattery.Type: GrantFiled: March 9, 2006Date of Patent: March 31, 2009Assignees: National Institute of Aerospace Associates, The United States of America as represented by the Administration of NASAInventors: Sang-Hyon Chu, Sang H. Choi, Jae-Woo Kim, Peter T. Lillehei, Yeonjoon Park, Glen C. King, James R. Elliott, Jr.
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Publication number: 20090078900Abstract: A valve includes a generally elongate pintle; a spacer having a rounded surface that bears against the pintle; a bulbous tip fixed to the spacer; and a hollow, generally cylindrical collar fixed to the pintle, the collar enclosing the spacer and the tip and including an opening through which a portion of the tip extends, the opening in the collar and interior of the collar being of a size such that the tip floats therein.Type: ApplicationFiled: September 25, 2007Publication date: March 26, 2009Applicant: NASA HeadquartersInventor: James T. Smith
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Publication number: 20090078929Abstract: A method of making nanowires includes providing a silicon substrate having a silicon dioxide insulation on the surface thereof. The silicon dioxide is etched to form one or more pillars, each having a plurality of sidewalls. A thin film of gold is deposited on a sidewall and is subjected to an annealing process. The annealing process causes the gold film to form a globular catalyst particle. The structure is placed in an LPCVD furnace into which is introduced silane gas. Silicon from the gas migrates through the catalyst particle and grows a nanowire from the sidewall of the pillar to a desired length. Electrical contacts are provided at each end of the nanowire to create an active component useable in an electronic circuit.Type: ApplicationFiled: September 26, 2007Publication date: March 26, 2009Applicant: NASA HeadquartersInventor: Stephanie A. Getty
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Patent number: 7501032Abstract: According to the invention, compositions of Ni—Ti—Pt high temperature, high force, shape memory alloys are disclosed that have transition temperatures above 100° C.; have narrow hysteresis; and produce a high specific work output.Type: GrantFiled: February 28, 2006Date of Patent: March 10, 2009Assignee: The United States of America as represented by the Administration of NASAInventors: Ronald D. Noebe, Susan L. Draper, Michael V. Nathal, Anita Garg
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Patent number: 7493869Abstract: The present invention is an apparatus and method for producing very large area and large volume plasmas. The invention utilizes electron cylcotron resonances in conjunction with permanent magnets to produce dense, uniform plasmas for long life ion thruster applications or for plasma processing applications such as etching, deposition, ion milling and ion implantation. The large area source is at least five times larger than the 12-inch wafers being processed to date. Its rectangular shape makes it easier to accommodate to materials processing than sources that are circular in shape. The source itself represents the largest ECR ion source built to date. It is electrodeless and does not utilize electromagnets to generate the ECR magnetic circuit, nor does it make use of windows.Type: GrantFiled: December 16, 2005Date of Patent: February 24, 2009Assignee: The United States of America as represented by the Administration of NASAInventors: John E. Foster, Michael J. Patterson
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Patent number: 7446459Abstract: A hybrid piezoelectric energy harvesting transducer system includes: (a) first and second symmetric, pre-curved piezoelectric elements mounted separately on a frame so that their concave major surfaces are positioned opposite to each other; and (b) a linear piezoelectric element mounted separately on the frame and positioned between the pre-curved piezoelectric elements. The pre-curved piezoelectric elements and the linear piezoelectric element are spaced from one another and communicate with energy harvesting circuitry having contact points on the frame. The hybrid piezoelectric energy harvesting transducer system has a higher electromechanical energy conversion efficiency than any known piezoelectric transducer.Type: GrantFiled: July 13, 2006Date of Patent: November 4, 2008Assignees: National Institute of Aerospace Associates, The United States of America as represented by the Administrator of NASAInventors: Tian-Bing Xu, Xiaoning Jiang, Ji Su, Paul W. Rehrig, Wesley S. Hackenberger