Patents Assigned to Space
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Patent number: 6761695Abstract: A method and apparatus for measuring intracranial pressure. In one embodiment, the method comprises the steps of generating an information signal that comprises components (e.g., pulsatile changes and slow changes) that are related to intracranial pressure and blood pressure, generating a reference signal comprising pulsatile components that are solely related to blood pressure, processing the information and reference signals to determine the pulsatile components of the information signal that have generally the same phase as the pulsatile components of the reference signal, and removing from the information signal the pulsatile components determined to have generally the same phase as the pulsatile components of the reference signal so as to provide a data signal having components wherein substantially all of the components are related to intracranial pressure.Type: GrantFiled: March 7, 2002Date of Patent: July 13, 2004Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: William T. Yost, John H. Cantrell, Jr.
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Patent number: 6760487Abstract: The invention presents The Estimated Spectrum Adaptive Postfilter (ESAP) and the Iterative Prepost Filter (IPF) algorithms. These algorithms model a number of image-adaptive post-filtering and pre-post filtering methods. They are designed to minimize Discrete Cosine Transform (DCT) blocking distortion caused when images are highly compressed with the Joint Photographic Expert Group (JPEG) standard. The ESAP and the IPF techniques of the present invention minimize the mean square error (MSE) to improve the objective and subjective quality of low-bit-rate JPEG gray-scale images while simultaneously enhancing perceptual visual quality with respect to baseline JPEG images.Type: GrantFiled: April 14, 2000Date of Patent: July 6, 2004Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Irving Linares
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Patent number: 6758382Abstract: A friction stir welding device that is configured to perform convention friction stir welding as well as self-reacting friction stir welding. A pin passes through an upper shoulder and can selectively attach to and detach from a lower shoulder in a preferred embodiment. A controller maintains the discrete position of, and/or force applied by, the upper and lower shoulders during self-reacting friction stir welding, or maintains the pin at a desired depth and/or applied force during conventional friction stir welding.Type: GrantFiled: May 2, 2003Date of Patent: July 6, 2004Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Robert W. Carter
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Patent number: 6760664Abstract: This invention is drawn to an autonomous navigation system using Global Positioning System (GPS) and magnetometers for low Earth orbit satellites. As a magnetometer is reliable and always provides information on spacecraft attitude, rate, and orbit, the magnetometer-GPS configuration solves GPS initialization problem, decreasing the convergence time for navigation estimate and improving the overall accuracy. Eventually the magnetometer-GPS configuration enables the system to avoid costly and inherently less reliable gyro for rate estimation. Being autonomous, this invention would provide for black-box spacecraft navigation, producing attitude, orbit, and rate estimates without any ground input with high accuracy and reliability.Type: GrantFiled: June 25, 2002Date of Patent: July 6, 2004Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Thienel K. Julie, Harman R. Richard, Itzhack Y. Bar-Itzhack
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Patent number: 6758098Abstract: A precision clamp accurately measures force over a wide range of conditions. Using a full bridge or other strain gage configuration, the elastic deformation of the clamp is measured or detected by the strain gages. The strain gages transmit a signal that corresponds to the degree of stress upon the clamp. The strain gage signal is converted to a numeric display. Calibration is achieved by zero and span potentiometers which enable accurate measurements by the force-measuring clamp.Type: GrantFiled: February 20, 2002Date of Patent: July 6, 2004Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Mark Nunnelee
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Patent number: 6759151Abstract: A multilayer article comprises a substrate comprising a ceramic or a silicon-containing metal alloy. The ceramic is a Si-containing ceramic or an oxide ceramic with or without silicon. An outer layer overlies the substrate and at least one intermediate layer is located between the outer layer and the substrate. An optional bond layer is disposed between the at least one intermediate layer and the substrate. The at least one intermediate layer may comprise an optional chemical barrier layer adjacent the outer layer, a mullite-containing layer and an optional chemical barrier layer adjacent to the bond layer or substrate. The outer layer comprises a compound having a low coefficient of thermal expansion selected from one of the following systems: rare earth (RE) silicates; at least one of hafnia and hafnia-containing composite oxides; zirconia-containing composite oxides and combinations thereof.Type: GrantFiled: May 22, 2002Date of Patent: July 6, 2004Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Kang N. Lee
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Patent number: 6757641Abstract: A multi-sensor transducer and processing method allow insitu monitoring of the senor accuracy and transducer ‘health’. In one embodiment, the transducer has multiple sensors to provide corresponding output signals in response to a stimulus, such as pressure. A processor applies individual weight factors to reach of the output signals and provide a single transducer output that reduces the contribution from inaccurate sensors. The weight factors can be updated and stored. The processor can use the weight factors to provide a ‘health’ of the transducer based upon the number of accurate versus in-accurate sensors in the transducer.Type: GrantFiled: June 28, 2002Date of Patent: June 29, 2004Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Christopher D. Immer, John Lane, Anthony J. Eckhoff, Jose M. Perotti
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Patent number: 6755530Abstract: Method and system for processing light signals received by the eye of a human or other animal, where the eye may be compromised or non-functioning. Incident light is received at first and second pixels in a photodetector array and provides a pixel electrical signal representing the received light. Each of an array of carbon nanotube (CNT) towers is connected to a pixel, has a first tower end penetrating a retinal active layer of the animal and has a second tower end positioned to receive to receive and transport the pixel electrical signal to the retinal active layer. The CNT tower may be coated with a biologically active substance or chemically modified to promote neurite connections with the tower. The photoreceptor array can be provide with a signal altering mechanism that alters at least one of light intensity and wavelength intensity sensed by a first pixel relative to a second pixel, to correct for one or more selected eye problems.Type: GrantFiled: July 16, 2002Date of Patent: June 29, 2004Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: David J. Loftus, Theodore Leng, Harvey Fishman
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Method for measuring diffusion coefficient in conductive melts, and apparatus for measuring the same
Publication number: 20040118190Abstract: Two conductive solid materials with their respective different compositions are joined in parallel with a gravity direction thereof, and then, heated and melted under static magnetic field orthogonal to the gravity direction to form two conductive melts with their respective different compositions. Then, the conductive melts are maintained for a predetermined period of time under the static magnetic field, and cooled and solidified.Type: ApplicationFiled: June 30, 2003Publication date: June 24, 2004Applicant: The Institute of Space and Astronautical ScienceInventors: Yuko Inatomi, Kazuhiko Kuribayashi -
Publication number: 20040122637Abstract: An embedded real-time operating system model which uses flight software to verify commands, fault annunciations, and telemetry acquisition is provided. The system includes or provides an avionics emulator, emulation of craft avionics and other components, complying command data or mission simulation software, and a portable computer for the cargo PC in a system to allow analysis of a payload and its interaction without access to actual flight computers of the craft.Type: ApplicationFiled: October 8, 2003Publication date: June 24, 2004Applicant: United Space Alliance, LLCInventors: Bill Askew, Matthew Barry, Roger Luty, Jon Morsics, Ayman Quaddumi, James Calvert Thompson
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Patent number: 6753293Abstract: A process for forming catalysts by coating substrates with two or more catalytic components, which comprises the following sequence of steps. First, the substrate is infused with an adequate amount of solution having a starting material comprising a catalytic component precursor, wherein the thermal decomposition product of the catalytic component precursor is a catalytic component. Second, the excess of the solution is removed from the substrate, thereby leaving a coating of the catalytic component precursor on the surface of the substrate. Third, the coating of the catalytic component precursor is converted to the catalytic component by thermal decomposition. Finally, the coated substance is etched to increase the surface area. The first three steps are then repeated for at least a second catalytic component. This process is ideally suited for application in producing efficient low temperature oxidation catalysts.Type: GrantFiled: June 30, 2000Date of Patent: June 22, 2004Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Eric J. Kielin, Billy T. Upchurch, David R. Schryer
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Patent number: 6753469Abstract: A power source converts &agr;-particle energy into electricity by coulomb collision in doped diamond films. Alpha particle decay from curium-244 creates electron-hole pairs by freeing electrons and holes inside the crystal lattice in N- and P-doped diamond films. Ohmic contacts provide electrical connection to an electronic device. Due to the built-in electric field at the rectifying junction across the N- and P-doped diamond films, the free electrons are constrained to traveling in generally one direction. This one direction then supplies electrons in a manner similar to that of a battery. The radioactive curium layer may be disposed on diamond films for even distribution of &agr;-particle radiation. The resulting power source may be mounted on a diamond substrate that serves to insulate structures below the diamond substrate from &agr;-particle emission. Additional insulation or isolation may be provided in order to prevent damage from &agr;-particle collision.Type: GrantFiled: August 5, 2002Date of Patent: June 22, 2004Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Elizabeth A. Kolawa, Jagdishbhai U. Patel, Jean-Pierre Fleurial
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Patent number: 6749573Abstract: A fetal heart monitoring system preferably comprising a backing plate having a generally concave front surface and a generally convex back surface, and at least one sensor element attached to the concave front surface for acquiring acoustic fetal heart signals produced by a fetus within a body. The sensor element has a shape that conforms to the generally concave back surface of the backing plate. In one embodiment, the at least one sensor element comprises an inner sensor, and a plurality of outer sensors surrounding the inner sensor. The fetal heart monitoring system can further comprise a web belt, and a web belt guide movably attached to the web belt. The web belt guide being is to the convex back surface of the backing plate.Type: GrantFiled: February 13, 2001Date of Patent: June 15, 2004Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Timothy D. Bryant, Mark W. Wynkoop, Nancy M. H. Holloway, Allan J. Zuckerwar
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Patent number: 6750438Abstract: An optical detector system includes an electrically resistive screen that is substantially transparent to radiation energy having a wavelength of interest. An electron transfer element (e.g., a low work function photoactive material or a carbon nanotube (CNT)-based element) has a first end and a second end with its first end spaced apart from the screen by an evacuated gap. When radiation energy passes through the screen with a bias voltage being applied thereto, transfer of electrons through the electron transfer element is induced from its first to its second end such that a quantity indicative of the electrons transferred can be detected.Type: GrantFiled: March 13, 2002Date of Patent: June 15, 2004Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Jeffrey D. Jordan
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Patent number: 6749533Abstract: 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: GrantFiled: May 24, 2002Date of Patent: June 15, 2004Assignee: MacDonald Dettwiler, Space and Advanced Robotics Ltd.Inventor: Robert D. Norman
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Patent number: 6751422Abstract: A spatial light communication equipment being capable of providing compatibility between two communication equipments placed opposite to each other and of providing, with simplified configurations, highly accurate seizure and tracking capability and excellent beam directivity for ultra-long-distance communication. Angular error in a receiving beam is detected by an angle detector disposed on an optical axis of light reflected by a first reflecting plane of a beam deflector and, based on detected results, an angle deflected by the beam deflector is corrected.Type: GrantFiled: January 22, 2001Date of Patent: June 15, 2004Assignee: NEC Toshiba Space Systems, Ltd.Inventor: Koichi Shiratama
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Patent number: 6745662Abstract: A sandwich core comprises two faceplates separated by a plurality of cells. The cells are comprised of walls positioned at oblique angles relative to a perpendicular axis extending through the faceplates. The walls preferably form open cells and are constructed from rows of ribbons. The walls may be obliquely angled relative to more than one plane extending through the perpendicular axis.Type: GrantFiled: August 6, 2001Date of Patent: June 8, 2004Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Donald B. Ford
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Patent number: 6745942Abstract: A magnetic symbology reader has a housing containing a polarized light source which directs light through a magneto-optic sensor onto a reflector which reflects light back through the magneto-optic sensor and then through at least one analyzer and into at least one camera. A view finder allows the user to monitor the image on the magneto-optic sensor as seen by a viewfinder camera while a processor is coupled to possibly a second camera so that when an image is detected, the image from the camera may be processed by the processor to output information associated with the symbol to an external source. The analyzer and polarized light source provide contrast in the images detected by the sensor. A bias/erase coil located about the magneto-optic sensor can enhance or erase images on the sensor.Type: GrantFiled: August 5, 2002Date of Patent: June 8, 2004Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Harry F. Schramm, William C. L. Shih, Gerald L. Fitzpatrick, Craig Knisely
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Patent number: 6746410Abstract: A method and apparatus for measuring changes in intracranial pressure (ICP) utilizing the variation of the surface wave propagation parameters of the patient's skull to determine the change in ICP.Type: GrantFiled: April 4, 2002Date of Patent: June 8, 2004Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: William T. Yost, John H. Cantrell, Jr.
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Patent number: 6748257Abstract: To prevent erroneous detection of a ribcage boundary from a chest image, an outer search limit point is decided with precision. A profile of smoothed pixel-value integrated averages in each of right and left lung field of the image is obtained, a threshold for each of the right and left lung fields with the profile taken as a reference is decided, and each of the right and left lung fields is searched from a central part of each lung field outwardly on the image so that a position exceeding the threshold is determined. The position is set as the outer search limit point for a series of a upper lung ribcage boundary candidate points. In the search, in cases the position exceeding the threshold is not found, a first derivative of the profile is used to decide the outer search limit point.Type: GrantFiled: October 25, 2001Date of Patent: June 8, 2004Assignee: Mitsubishi Space Software Co., Ltd.Inventor: Osamu Ozaki