Patents Represented by Attorney, Agent or Law Firm John F. Schipper
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Patent number: 7549338Abstract: Method and system (i) to determine when a selected target molecule is present or absent in a fluid, (2) to estimate concentration of the target molecule in the fluid and (3) estimate possible presence of a second (different) target molecule in the fluid, by analyzing differences in resonant frequencies of vibration of a thin beam suspended in the fluid, after the fluid has moved across the beam.Type: GrantFiled: September 28, 2007Date of Patent: June 23, 2009Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: John F. Schipper
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Patent number: 7531775Abstract: A photometer that tracks a path of a moving light source with little or no motion of the photometer components. The system includes a non-moving, truncated paraboloid of revolution, having a paraboloid axis, a paraboloid axis, a small entrance aperture, a larger exit aperture and a light-reflecting inner surface, that receives and reflects light in a direction substantially parallel to the paraboloid axis. The system also includes a light processing filter to receive and process the redirected light, and to issue the processed, redirected light as processed light, and an array of light receiving elements, at least one of which receives and measures an associated intensity of a portion of the processed light. The system tracks a light source moving along a path and produces a corresponding curvilinear image of the light source path on the array of light receiving elements.Type: GrantFiled: September 30, 2005Date of Patent: May 12, 2009Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Anthony W. Strawa
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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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Patent number: 7516890Abstract: Method and system for monitoring present location and/or present status of a target inventory item, where the inventory items are located on one or more inventory shelves or other inventory receptacles that communicate with an inventory base station through use of responders such as RFIDs. A user operates a hand held interrogation and display (IAD) module that communicates with, or is part of, the base station, to provide an initial inquiry. Information on location(s) of the target inventory item is also indicated visibly and/or audibly on the receptacle(s) for the user. Status information includes an assessment of operation readiness and a time, if known, that the specified inventory item or class was last removed or examined or modified. Presentation of a user access level may be required for access to the target inventory item. Another embodiment provides inventory information for a stack as a sight-impaired or hearing-impaired person passes adjacent to that stack.Type: GrantFiled: May 25, 2006Date of Patent: April 14, 2009Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Stevan M. Spremo, Usen E. Udoh
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Patent number: 7490367Abstract: Method and system for processing waste from human activities, including solids, liquids and vapors. A fluid-impermeable bag, lined with a liquid-impermeable but vapor-permeable membrane, defining an inner bag, is provided. A vacuum force is provided to extract vapors so that the waste is moved toward a selected region in the inner bag, extracted vapors, including the waste vapors and vaporized portions of the waste liquids are transported across the membrane, and most or all of the solids remain within the liner. Extracted vapors are filtered, and sanitized components thereof are isolated and optionally stored. The solids remaining within the liner are optionally dried and isolated for ultimate disposal.Type: GrantFiled: September 20, 2006Date of Patent: February 17, 2009Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Eric Litwiller, John A. Hogan, John W. Fisher
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Patent number: 7473436Abstract: Method and system for functionalizing a collection of carbon nanotubes (CNTs). A selected precursor gas (e.g., H2 or F2 or CnHm) is irradiated to provide a cold plasma of selected target species particles, such as atomic H or F, in a first chamber. The target species particles are directed toward an array of CNTs located in a second chamber while suppressing transport of ultraviolet radiation to the second chamber. A CNT array is functionalized with the target species particles, at or below room temperature, to a point of saturation, in an exposure time interval no longer than about 30 sec. *Discrimination against non-target species is provided by (i) use of a target species having a lifetime that is much greater than a lifetime of a non-target species and/or (2) use of an applied magnetic field to discriminate between charged particle trajectories for target species and for non-target species.Type: GrantFiled: April 5, 2004Date of Patent: January 6, 2009Assignees: The United States of America as represented by the Administrator of the National Aeronautics and Space Administrator, SETI InstituteInventors: Bishun N. Khare, Meyya Meyyappan
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Patent number: 7473930Abstract: Method and system for providing a dynamically reconfigurable display having nanometer-scale resolution, using a patterned array of multi-wall carbon nanotube (MWCNT) clusters. A diode, phosphor or other light source on each MWCNT cluster is independently activated, and different color light sources (e.g., red, green, blue, grey scale, infrared) can be mixed if desired. Resolution is estimated to be 40-100 nm, and reconfiguration time for each MWCNT cluster is no greater than one microsecond.Type: GrantFiled: July 1, 2005Date of Patent: January 6, 2009Assignee: The United States of America as represented by the United States National Aeronautics and Space AdministrationInventors: Lance D. Delzeit, John F. Schipper
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Patent number: 7454321Abstract: Method system, and product from application of the method, for design of a subsonic airfoil shape, beginning with an arbitrary initial airfoil shape and incorporating one or more constraints on the airfoil geometric parameters and flow characteristics. The resulting design is robust against variations in airfoil dimensions and local airfoil shape introduced in the airfoil manufacturing process. A perturbation procedure provides a class of airfoil shapes, beginning with an initial airfoil shape.Type: GrantFiled: July 1, 2005Date of Patent: November 18, 2008Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Man Mohan Rai
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Patent number: 7438422Abstract: A portable structure, simply constructed with inexpensive and generally lightweight materials, for displaying a selected portion of the night sky and selected planets, satellites, comets and other astronomically observable objects that are visually perceptible within that portion of the night sky. The structure includes a computer having stored signals representing the observable objects, an image projector that converts and projects the stored signals as visually perceptible images, a first curvilinear light-reflecting surface to receive and reflect the visually perceptible images, and a second curvilinear surface to receive and display the visually perceptible images reflected from the first surface. The images may be motionless or may move with passage of time.Type: GrantFiled: January 18, 2006Date of Patent: October 21, 2008Assignee: United States of America as represented by the Administrator of the National Aeronautics & Space AdministrationInventor: Timothy P. Castellano
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Patent number: 7431242Abstract: A convex shell structure for enhanced aerodynamic performance and/or reduced heat transfer requirements for a space vehicle that re-enters an atmosphere. The structure has a fore-body, an aft-body, a longitudinal axis and a transverse cross sectional shape, projected on a plane containing the longitudinal axis, that includes: first and second linear segments, smoothly joined at a first end of each the first and second linear segments to an end of a third linear segment by respective first and second curvilinear segments; and a fourth linear segment, joined to a second end of each of the first and second segments by curvilinear segments, including first and second ellipses having unequal ellipse parameters. The cross sectional shape is non-symmetric about the longitudinal axis. The fourth linear segment can be replaced by a sum of one or more polynomials, trigonometric functions or other functions satisfying certain constraints.Type: GrantFiled: November 1, 2005Date of Patent: October 7, 2008Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration (NASA)Inventors: James L. Brown, Joseph A. Garcia, Dinesh K. Prabhu
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Patent number: 7426848Abstract: A method and system for estimating one, two or more unknown components in a gas. A first array of spaced apart carbon nanotubes (“CNTs”) is connected to a variable pulse voltage source at a first end of at least one of the CNTs. A second end of the at least one CNT is provided with a relatively sharp tip and is located at a distance within a selected range of a constant voltage plate. A sequence of voltage pulses {V(tn)}n at times t=tn (n=1, . . . , N1; N1?3) is applied to the at least one CNT, and a pulse discharge breakdown threshold voltage is estimated for one or more gas components, from an analysis of a curve I(tn) for current or a curve e(tn) for electric charge transported from the at least one CNT to the constant voltage plate. Each estimated pulse discharge breakdown threshold voltage is compared with known threshold voltages for candidate gas components to estimate whether at least one candidate gas component is present in the gas.Type: GrantFiled: August 5, 2005Date of Patent: September 23, 2008Assignee: United States of America as Represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Jing Li, Meyya Meyyappan
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Patent number: 7381459Abstract: A composite thermal protection structure, for applications such as atmospheric re-entry vehicles, that can withstand temperatures as high as 3600° F. The structure includes an exposed surface cap having a specially formulated coating, an insulator base adjacent to the cap with another specially formulated coating, and one or more pins that extend from the cap through the insulator base to tie the cap and base together, through ceramic bonding and mechanical attachment. The cap and insulator base have corresponding depressions and projections that mate and allow for differences in thermal expansion of the cap and base.Type: GrantFiled: February 12, 2004Date of Patent: June 3, 2008Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration (NASA)Inventors: David A. Stewart, Daniel B. Leiser
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Patent number: 7383238Abstract: The present invention relates to an Inductive Monitoring System (IMS), its software implementations, hardware embodiments and applications. Training data is received, typically nominal system data acquired from sensors in normally operating systems or from detailed system simulations. The training data is formed into vectors that are used to generate a knowledge database having clusters of nominal operating regions therein. IMS monitors a system's performance or health by comparing cluster parameters in the knowledge database with incoming sensor data from a monitored-system formed into vectors. Nominal performance is concluded when a monitored-system vector is determined to lie within a nominal operating region cluster or lies sufficiently close to a such a cluster as determined by a threshold value and a distance metric. Some embodiments of IMS include cluster indexing and retrieval methods that increase the execution speed of IMS.Type: GrantFiled: February 24, 2004Date of Patent: June 3, 2008Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: David L. Iverson
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Patent number: 7378963Abstract: System and method for visual and audible communication between a central operator and N mobile communicators (N?2), including an operator transceiver and interface, configured to receive and display, for the operator, visually perceptible and audibly perceptible signals from each of the mobile communicators. The interface (1) presents an audible signal from each communicator as if the audible signal is received from a different location relative to the operator and (2) allows the operator to select, to assign priority to, and to display, the visual signals and the audible signals received from a specified communicator. Each communicator has an associated signal transmitter that is configured to transmit at least one of the visual signal and the audio signal associated with the communicator, where at least one of the signal transmitters includes at least one sensor that senses and transmits a sensor value representing a selected environmental or physiological parameter associated with the communicator.Type: GrantFiled: September 20, 2005Date of Patent: May 27, 2008Inventors: Durand R. Begault, Mark R. Anderson, Bryan McClain, Joel D. Miller
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Patent number: 7375826Abstract: A laser scanner computes a range from a laser line to an imaging sensor. The laser line illuminates a detail within an area covered by the imaging sensor, the area having a first dimension and a second dimension. The detail has a dimension perpendicular to the area. A traverse moves a laser emitter coupled to the imaging sensor, at a height above the area. The laser emitter is positioned at an offset along the scan direction with respect to the imaging sensor, and is oriented at a depression angle with respect to the area. The laser emitter projects the laser line along the second dimension of the area at a position where a image frame is acquired. The imaging sensor is sensitive to laser reflections from the detail produced by the laser line. The imaging sensor images the laser reflections from the detail to generate the image frame.Type: GrantFiled: September 23, 2004Date of Patent: May 20, 2008Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration (NASA)Inventors: Joseph P. Lavelle, Stefan R. Schuet
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Patent number: 7346172Abstract: Methods and systems for distinguishing an auditory alert signal from a background of one or more non-alert signals. In a first embodiment, a prefix signal, associated with an existing alert signal, is provided that has a signal component in each of three or more selected frequency ranges, with each signal component in each of three or more selected level at least 3-10 dB above an estimated background (non-alert) level in that frequency range. The alert signal may be chirped within one or more frequency bands. In another embodiment, an alert signal moves, continuously or discontinuously, from one location to another over a short time interval, introducing a perceived spatial modulation or jitter.Type: GrantFiled: March 28, 2001Date of Patent: March 18, 2008Assignee: The United States of America as represented by the United States National Aeronautics and Space AdministrationInventor: Durand R. Begault
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Patent number: 7333735Abstract: Ultrafast directional beam switching, using coupled VCSELs is combined with a light modulator to provide information transfer at bit rates of tens of GHz. This approach is demonstrated to achieve beam switching frequencies of 32-50 GHz in some embodiments and directional beam switching with angular differences 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. A Mach-Zehnder interferometer, a Fabry-Peror etalon, or a semiconductor-based electro-absorption transmission channel, among others, can be used as a light modulator.Type: GrantFiled: June 30, 2004Date of Patent: February 19, 2008Assignee: United States of America as Represented by the Administrator of the National Aeronautics and Space Administration (NASA)Inventor: Peter M. Goorjian
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Patent number: 7314648Abstract: A composite thermal protection structure, for applications such as atmospheric re-entry vehicles, that can withstand temperatures as high as 3600° F. The structure includes an exposed surface cap having a specially formulated coating, an insulator base adjacent to the cap with another specially formulated coating, and one or more pins that extend from the cap through the insulator base to tie the cap and base together, through ceramic bonding and mechanical attachment. The cap and insulator base have corresponding depressions and projections that mate and allow for differences in thermal expansion of the cap and base. A thin coating of a reaction cured glass formulation is optionally provided on the structure to allow reduce oxidization and/or to reduce catalytic efficiency.Type: GrantFiled: July 27, 2004Date of Patent: January 1, 2008Assignee: United States of America as represented by the Administrator of the National Aeronautics and Space Administration (NASA)Inventors: David A. Stewart, Daniel B. Leiser
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Patent number: 7313475Abstract: A method and associated system for time delay banking for aircraft arrival time, aircraft departure time and/or en route flight position. The delay credit value for a given flight may decrease with passage of time and may be transferred to or traded with other flights having the same or a different user (airline owner or operator). The delay credit value for a given aircraft flight depends upon an initial delay credit value, which is determined by a central system and depends upon one or more other flight characteristics. Optionally, the delay credit value decreases with passage of time. Optionally, a transaction cost is assessed against a delay credit value that is used on behalf of another flight with the same user or is traded with a different user.Type: GrantFiled: February 1, 2005Date of Patent: December 25, 2007Assignee: United States of America as Represented by the Administrator of the National Aeronautics and Space Administration (NASA)Inventor: Steven M. Green
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Patent number: 7293001Abstract: System and method for optimization of a design associated with a response function, using a hybrid neural net and support vector machine (NN/SVM) analysis to minimize or maximize an objective function, optionally subject to one or more constraints. As a first example, the NN/SVM analysis is applied iteratively to design of an aerodynamic component, such as an airfoil shape, where the objective function measures deviation from a target pressure distribution on the perimeter of the aerodynamic component. As a second example, the NN/SVM analysis is applied to data classification of a sequence of data points in a multidimensional space. The NN/SVM analysis is also applied to data regression.Type: GrantFiled: November 14, 2005Date of Patent: November 6, 2007Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administrator (NASA)Inventor: Man Mohan Rai