Patents Represented by Attorney Keith L. Dixon
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Patent number: 7255483Abstract: A thrust roller bearing system comprising an inner rotating member, an outer rotating member and multiple rollers coupling the inner rotating member with outer rotating member. The inner and outer rotating members include thrust lips to enable the rollers to act as thrust rollers. The rollers contact inner and outer rotating members at bearing contact points along a contact line. Consequently, the radial/tilt and thrust forces move synchronously and simultaneously to create a bearing action with no slipping.Type: GrantFiled: June 18, 2002Date of Patent: August 14, 2007Assignee: United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: John M. Vranish
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Patent number: 7248342Abstract: This invention is directed to a 3-dimensional imaging lidar, which utilizes modest power kHz rate lasers, array detectors, photon-counting multi-channel timing receivers, and dual wedge optical scanners with transmitter point-ahead correction to provide contiguous high spatial resolution mapping of surface features including ground, water, man-made objects, vegetation and submerged surfaces from an aircraft or a spacecraft.Type: GrantFiled: December 5, 2003Date of Patent: July 24, 2007Assignee: United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: John J. Degnan
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Patent number: 7008605Abstract: A non-catalytic process for the production of carbon nanotubes includes supplying an electric current to a carbon anode and a carbon cathode which have been securely positioned in the open atmosphere with a gap between them. The electric current creates an electric arc between the carbon anode and the carbon cathode, which causes carbon to be vaporized from the carbon anode and a carbonaceous residue to be deposited on the carbon cathode. Inert gas is pumped into the gap to flush out oxygen, thereby preventing interference with the vaporization of carbon from the anode and preventing oxidation of the carbonaceous residue being deposited on the cathode. The anode and cathode are cooled while electric current is being supplied thereto. When the supply of electric current is terminated, the carbonaceous residue is removed from the cathode and is purified to yield carbon nanotubes.Type: GrantFiled: November 8, 2002Date of Patent: March 7, 2006Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Jeanette M. Benavides
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Patent number: 6990436Abstract: This invention presents a method for computing Instantaneous Frequency by applying Empirical Mode Decomposition to a signal and using Generalized Zero-Crossing (GZC) and Extrema Sifting. The GZC approach is the most direct, local, and also the most accurate in the mean. Furthermore, this approach will also give a statistical measure of the scattering of the frequency value. For most practical applications, this mean frequency localized down to quarter of a wave period is already a well-accepted result. As this method physically measures the period, or part of it, the values obtained can serve as the best local mean over the period to which it applies. Through Extrema Sifting, instead of the cubic spline fitting, this invention constructs the upper envelope and the lower envelope by connecting local maxima points and local minima points of the signal with straight lines, respectively, when extracting a collection of Intrinsic Mode Functions (IMFs) from a signal under consideration.Type: GrantFiled: November 28, 2003Date of Patent: January 24, 2006Assignee: 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: 6901353Abstract: This invention presents Normalized Amplitude Hilbert Transform (NAHT) and Normalized Hilbert Transform(NHT), both of which are new methods for computing Instantaneous Frequency. This method is designed specifically to circumvent the limitation set by the Bedorsian and Nuttal Theorems, and to provide a sharp local measure of error when the quadrature and the Hilbert Transform do not agree. Motivation for this method is that straightforward application of the Hilbert Transform followed by taking the derivative of the phase-angle as the Instantaneous Frequency (IF) leads to a common mistake made up to this date. In order to make the Hilbert Transform method work, the data has to obey certain restrictions.Type: GrantFiled: July 8, 2003Date of Patent: May 31, 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: 6895115Abstract: A method, computer readable storage, and apparatus for implementing a recursive hierarchical segmentation algorithm on a parallel computing platform. The method includes setting a bottom level of recursion that defines where a recursive division of an image into sections stops dividing, and setting an intermediate level of recursion where the recursive division changes from a parallel implementation into a serial implementation. The segmentation algorithm is implemented according to the set levels. The method can also include setting a convergence check level of recursion with which the first level of recursion communicates with when performing a convergence check.Type: GrantFiled: April 23, 2001Date of Patent: May 17, 2005Assignee: The United States of America as represented by the United States National Aeronautics and Space AdministrationInventor: James C. Tilton
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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: 6847354Abstract: A three-dimensional (3-D) interactive display and method of forming the same, includes a transparent capaciflector (TC) camera formed on a transparent shield layer on the screen surface. A first dielectric layer is formed on the shield layer. A first wire layer is formed on the first dielectric layer. A second dielectric layer is formed on the first wire layer. A second wire layer is formed on the second dielectric layer. Wires on the first wire layer and second wire layer are grouped into groups of parallel wires with a turnaround at one end of each group and a sensor pad at the opposite end. An operational amplifier is connected to each of the sensor pads and the shield pad biases the pads and receives a signal from connected sensor pads in response to intrusion of a probe. The signal is proportional to probe location with respect to the monitor screen.Type: GrantFiled: March 13, 2001Date of Patent: January 25, 2005Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: John M. Vranish
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Patent number: 6782124Abstract: An apparatus and method of analysis for three-dimensional (3D) physical phenomena. The physical phenomena may include any varying 3D phenomena such as time varying polar ice flows. A repesentation of the 3D phenomena is passed through a Hilbert transform to convert the data into complex form. A spatial variable is separated from the complex representation by producing a time based covariance matrix. The temporal parts of the principal components are produced by applying Singular Value Decomposition (SVD). Based on the rapidity with which the eigenvalues decay, the first 3-10 complex principal components (CPC) are selected for Empirical Mode Decomposition into intrinsic modes. The intrinsic modes produced are filtered in order to reconstruct the spatial part of the CPC. Finally, a filtered time series may be reconstructed from the first 3-10 filtered complex principal components.Type: GrantFiled: November 29, 2000Date of Patent: August 24, 2004Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Per Gloersen
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Patent number: 6740224Abstract: A process for manufacturing carbon nanotubes, including a step of inducing electrical current through a carbon anode and a carbon cathode under conditions effective to produce the carbon nanotubes, wherein the carbon cathode is larger than the carbon anode. Preferably, a welder is used to induce the electrical current via an arc welding process. Preferably, an exhaust hood is placed on the anode, and the process does not require a closed or pressurized chamber. The process provides high-quality, single-walled carbon nanotubes, while eliminating the need for a metal catalyst.Type: GrantFiled: June 11, 2002Date of Patent: May 25, 2004Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Jeanette M. Benavides, Henning W. Leidecker, Jeffrey Frazier
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Patent number: 6648522Abstract: A fiber optic connector polishing fixture assembly for supporting a terminus of a fiber optic cable before a polishing surface. The assembly comprises: a fiber optic polishing fixture adapted to support the terminus before the polishing surface; a fixture support connected to the fixture for supporting the fixture before the polishing surface; and an adjustable connection between the fixture and the fixture support having user accessible adjustment controls for allowing a user to operate the controls to shift the fixture and fixture support relative to one another for substantially eliminating an apex offset of the terminus with respect to the polishing surface.Type: GrantFiled: March 13, 2001Date of Patent: November 18, 2003Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: John R. Kolasinski, Joseph Roch Moszcziewski
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Patent number: 6640949Abstract: A one-way bearing is provided having sprags and rolling bearings both disposed between an inner and an outer race. The sprags may comprise three-dimensional sprags for preventing rotation in a non-preferential direction. The rolling bearings may comprise thrust rollers for transmitting axial, tilt, and radial loads between the inner and outer races.Type: GrantFiled: March 1, 2002Date of Patent: November 4, 2003Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: John M. Vranish
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Patent number: 6631325Abstract: A computer implemented physical signal analysis method is includes two essential steps and the associated presentation techniques of the results. All the steps exist only in a computer: there are no analytic expressions resulting from the method. The first step is a computer implemented Empirical Mode Decomposition to extract a collection of Intrinsic Mode Functions (IMF) from nonlinear, nonstationary physical signals based on local extrema and curvature extrema. The decomposition is based on the direct extraction of the energy associated with various intrinsic time scales in the physical signal. Expressed in the IMF's, they have well-behaved Hilbert Transforms from which instantaneous frequencies can be calculated. The second step is the Hilbert Transform. The final result is the Hilbert Spectrum. Thus, the invention can localize any event on the time as well as the frequency axis. The decomposition can also be viewed as an expansion of the data in terms of the IMF's.Type: GrantFiled: May 21, 1998Date of Patent: October 7, 2003Assignee: The United States as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Norden Eh Huang, Zheng Shen
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Patent number: 6626792Abstract: A gear bearing having a first gear and a second gear, each having a plurality of teeth. Each gear operates on two non-parallel surfaces of the opposing gear teeth to perform both gear and bearing functions simultaneously. The gears are moving at substantially the same speed at their contact points. The gears may be roller gear bearings or phase-shifted gear bearings, and may be arranged in a planet/sun system or used as a transmission.Type: GrantFiled: March 3, 2001Date of Patent: September 30, 2003Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: John M. Vranish
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Patent number: 6538796Abstract: A micro-electromechanical device that comprises miniaturized mechanical louvers, referred to as Micro Electro-Mechanical Systems (MEMS) louvers are employed to achieve a thermal control function for spacecraft and instruments. The MEMS louvers are another form of a variable emittance control coating and employ micro-electromechanical technology. In a function similar to traditional, macroscopic thermal louvers, the MEMS louvers of the present invention change the emissivity of a surface. With the MEMS louvers, as with the traditional macroscopic louvers, a mechanical vane or window is opened and closed to allow an alterable radiative view to space.Type: GrantFiled: March 31, 2000Date of Patent: March 25, 2003Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Theordore D. Swanson
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Patent number: 6479808Abstract: Systems and methods for processing light from multiple fields (48, 54, 55) of view without excessive machinery for scanning optical elements. In an exemplary embodiment of the invention, multiple holographic optical elements (41, 42, 43, 44, 45), integrated on a common film (4), diffract and project light from respective fields of view.Type: GrantFiled: June 28, 2000Date of Patent: November 12, 2002Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Geary K. Schwemmer
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Patent number: 6287404Abstract: An assembly for supporting a fiber optic termination or connector in a centrifuge and comprising a cylindrical body member having a top portion adapted to receive the ferrule body portion of a fiber optic termination or connector and a bottom portion for receiving a cylindrical piston/sealing unit. The piston portion of the piston/sealing unit includes a compressible tip which is adapted to a butt up against the outer end of the ferrule body portion of the fiber optic termination or connector. A cylindrical end cap fits over the upper end of the body member for holding the fiber optic termination in place on the body member and causing a seal to be formed between the termination or connector and the upper portion of the body member adjacent the compressible tip of the plunger. The parts, when fitted together, are placed in a centrifuge which is operated for a predetermined spin cycle, so as to cause any bubbles in the uncured liquid adhesive to be vented outwardly from the termination through the end cap.Type: GrantFiled: December 13, 1999Date of Patent: September 11, 2001Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: John R. Kolasinski
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Patent number: 6211822Abstract: The spaceborne Global Positioning System receiver provides navigational solutions and is designed for use in low Earth orbit. The spaceborne GPS receiver can determine the orbital position of a spacecraft using any of the satellites within the GPS constellation. It is a multiple processor system incorporating redundancy by using a microcontroller to handle the closure of tracking loops for acquired GPS satellites, while a separate microprocessor computes the spacecraft navigational solution and handles other tasks within the receiver. The spaceborne GPS receiver can use either microcontroller or the microprocessor to close the satellite tracking loops. The use of microcontroller provides better tracking performance of acquired GPS satellites. The spaceborne GPS receiver utilizes up to seven separate GPS boards, with each board including its own set of correlators, down-converters and front-end components. The spaceborne GPS receiver also includes telemetry and time-marking circuitry.Type: GrantFiled: July 7, 1999Date of Patent: April 3, 2001Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdminstrationsInventors: Lamar F. Dougherty, Frederick A. Niles, Miriam D. Wennersten
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Patent number: 5967267Abstract: A roller type sprag member consisting of three main elements, an outer roller half section, an inner roller half section, and an assembly-location pin. The sprag locks using roller locking techniques in a manner well known in the case of a three-dimensional (3-D) locking sprag. It unlocks, however, using a roll technique in which the inner and outer roller halves rotate in mutually opposite directions, one clockwise and the other counterclockwise. In the process of rotation, the roller is foreshortened between the distance across the sprag contact surfaces, whereupon it loses its ability to act as a locking sprag and releases.Type: GrantFiled: February 12, 1996Date of Patent: October 19, 1999Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: John M. Vranish
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Patent number: RE36772Abstract: A capacitive proximity sensing element, backed by a reflector driven at the same voltage as and in phase with the sensor, is used to reflect the field lines away from a grounded robot arm towards an intruding object, thus dramatically increasing the sensor's range and sensitivity.Type: GrantFiled: November 6, 1996Date of Patent: July 11, 2000Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: John M. Vranish, Robert L. McConnell