Patents Assigned to Space
-
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
-
Patent number: 6647855Abstract: Provided herein are apparatuses for deployment of at least one hypervelocity shield on a structure in exoatmospheric space. The apparatuses comprise a means of attaching to the structure at least at one place on the structure and further comprise at least one of the hypervelocity shields and a means of deploying said shields. Also provided are methods of deploying the hypervelocity shields using said apparatuses.Type: GrantFiled: September 30, 2002Date of Patent: November 18, 2003Assignee: The United States of America as represented by the United States National Aeronautics and Space AdministrationInventors: Eric L. Christiansen, Justin H. Kerr
-
Patent number: 6647685Abstract: A tool for the spacing of tiles during installation includes a central body with radially projecting prongs that are fitted between adjacent tiles to control the spacing thereof.Type: GrantFiled: January 10, 2002Date of Patent: November 18, 2003Assignee: Space-It-RiteInventors: Joseph L. Annarella, Robert Grzybowski, John F. Dumelle
-
Patent number: 6650280Abstract: System and methods are disclosed for fluid measurements which may be utilized to determine mass flow rates such as instantaneous mass flow of a fluid stream. In a preferred embodiment, the present invention may be utilized to compare an input mass flow to an output mass flow of a drilling fluid circulation stream. In one embodiment, a fluid flow rate is determined by utilizing a microwave detector in combination with an acoustic sensor. The acoustic signal is utilized to eliminate 2&pgr; phase ambiguities in a reflected microwave signal. In another embodiment, a fluid flow rate may be determined by detecting a phase shift of an acoustic signal across two different predetermined transmission paths. A fluid density may be determined by detecting a calibrated phase shift of an acoustic signal through the fluid. In another embodiment, a second acoustic signal may be transmitted through the fluid to define a particular 2&pgr; phase range which defines the phase shift.Type: GrantFiled: September 14, 2001Date of Patent: November 18, 2003Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: G. Dickey Arndt, Phong H. Ngo, James R. Carl, Kent A. Byerly
-
Patent number: 6650125Abstract: A method and system for locating leaks of conductive fluids from non-conductive pipes and other structures or for locating non-conductive pipes or structures having conductive fluid contained therein, employ a charge generator to apply a time varying charge to the conductive fluid, and a capacitive type detector that can detect the variable charge that is induced in the fluid. The capacitive detector, which preferably includes a handheld housing, employs a large conductive pickup plate that is used to locate the pipe or leak by scanning the plate over the ground and detecting the induced charge that is generated when the plate comes in close proximity to the pipe or leak. If a leak is encountered, the resulting signal will appear over an area larger than expected for a buried pipe, assuming the leak provides an electrically conductive path between the flow and the wet surrounding ground.Type: GrantFiled: December 6, 2001Date of Patent: November 18, 2003Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Robert C. Youngquist
-
Patent number: 6647809Abstract: A high temperature anemometer includes a pair of substrates. One of the substrates has a plurality of electrodes on a facing surface, while the other of the substrates has a sensor cavity on a facing surface. A sensor is received in the sensor cavity, wherein the sensor has a plurality of bondpads, and wherein the bond pads contact the plurality of electrodes when the facing surfaces are mated with one another. The anemometer further includes a plurality of plug-in pins, wherein the substrate with the cavity has a plurality of trenches with each one receiving a plurality of plug-in pins. The plurality of plug-in pins contact the plurality of electrodes when the substrates are mated with one another. The sensor cavity is at an end of one of the substrates such that the sensor partially extends from the substrate. The sensor and the substrates are preferably made of silicon carbide.Type: GrantFiled: August 29, 2002Date of Patent: November 18, 2003Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Robert S. Okojie, Gustave C. Fralick, George J. Saad
-
Patent number: 6648543Abstract: A flange (1) for a space vessel (2), which flange (1) is arranged so as to reduce a shock or impact wave that occurs upon the release of a coupling (5). The coupling (5) is intended to impart a radially inwardly acting force to hold together two separable space vessel parts (3, 4) via two flanges (1, 6) belonging to respective space vessel parts (3, 4). The first flange (1) comprises at least one weakened point (9) so that it has a substantially broken annular shape, in order to thus reduce its energy-absorbing capacity when it is bent inward by the force (F).Type: GrantFiled: April 19, 2002Date of Patent: November 18, 2003Assignee: Saab Ericsson Space ABInventor: Örjan Arulf
-
Publication number: 20030212243Abstract: The present invention relates generally to polyimides. It relates particularly to novel polyimides prepared from 2,3,3′,4′-biphenyltetracarboxylic dianhydride and aromatic diamines. These novel polyimides have low color, good solubility, high thermal emissivity, low solar absorptivity and high tensile strength.Type: ApplicationFiled: April 7, 2003Publication date: November 13, 2003Applicant: Administrator of the National Aeronautics and Space AdministrationInventors: Paul M. Hergenrother, Joseph G. Smith, John W. Connell, Kent A. Watson
-
Patent number: 6646723Abstract: The present invention is an improved distance measuring interferometer that includes high speed phase modulators and additional phase meters to generate and analyze multiple heterodyne signal pairs with distinct frequencies. Modulation sidebands with large frequency separation are generated by the high speed electro-optic phase modulators, requiring only a single frequency stable laser source and eliminating the need for a first laser to be tuned or stabilized relative to a second laser. The combination of signals produced by the modulated sidebands is separated and processed to give the target distance. The resulting metrology apparatus enables a sensor with submicron accuracy or better over a multi-kilometer ambiguity range.Type: GrantFiled: May 7, 2002Date of Patent: November 11, 2003Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Serge Dubovitsky, Oliver P. Lay
-
Patent number: 6641638Abstract: The present invention describes a process for converting vapor streams from sources containing at least one nitrogen-containing oxidizing agent therein to a liquid fertilizer composition comprising the steps of: a) directing a vapor stream containing at least one nitrogen-containing oxidizing agent to a first contact zone, b) contacting said vapor stream with water to form nitrogen oxide(s) from said at least one nitrogen-containing oxidizing agent, c) directing said acid(s) as a second stream to a second contact zone, d) exposing said second stream to hydrogen peroxide which is present within said second contact zone in a relative amount of at least 0.Type: GrantFiled: February 17, 2000Date of Patent: November 4, 2003Assignee: The United States of America as represented by the Administrator of the National Aeronautics & Space AdministrationInventors: Dale E. Lueck, Clyde F. Parrish
-
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
-
Patent number: 6641083Abstract: A balloon comprising an envelope, wherein the envelope has a multilayered structure comprising a gas-impervious sheet, and a liquid absorbent sheet overlaid on the inner surface of the gas-impervious sheet.Type: GrantFiled: February 4, 2002Date of Patent: November 4, 2003Assignee: The Director-General of the Institute of Space and Astronautical ScienceInventors: Naoki Izutsu, Nobuyuki Yajima
-
Publication number: 20030201901Abstract: A method is provided for marking electrical wiring with condition indicators. One or more markers are added to one or both of the insulative material and a surface of an electrical conductor such that it bonds thereto. Each marker is capable of emanating into a surrounding atmospheric environment as a gaseous effluent in response to a specific condition experienced by the electrical conductor.Type: ApplicationFiled: April 21, 2003Publication date: October 30, 2003Applicant: Administrator of the National Aeronautics and Space AdministrationInventors: William T. Yost, Daniel F. Perey, K. Elliott Cramer
-
Publication number: 20030200786Abstract: Passive and active methods for anticipating problems with electrical wiring are provided. An insulative material in contact with an electrical conductor has at least one impurity that is impregnated in the insulative material and/or disposed thereon. An environment around the electrical conductor is monitored for the presence or the level of the impurity(ies) emanating from the insulative material in the form of a gaseous effluent. An alarm signal is generated when a predetermined level of the gaseous effluent is detected.Type: ApplicationFiled: April 21, 2003Publication date: October 30, 2003Applicant: U.S.A. as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: William T. Yost, K. Elliott Cramer, Daniel F. Perey
-
Patent number: 6639178Abstract: Process for the local removal of a coating (2), consisting of at least one metallic layer and/or at least one metal-oxide layer, applied on a translucent or transparent substrate (1) made of natural or synthetic glass or of transparent plastic, characterised in that, by means of a solid-state pulse laser (4) or at least one pulsed laser diode, a pulsed laser beam (3) whose pulse is inferior to the 30 ns and whose wave length(s) is/are comprised between 10 micrometers and 360 nanometers is directed onto the coating (2) to those spots where the latter has to be removed, whereby the applied wave lengths are such that the absorption of the substrate (1) and of the coating (2) as a whole is less than 30%.Type: GrantFiled: July 22, 2002Date of Patent: October 28, 2003Assignee: Wallonia Space Logistics, en Abrege WSL, Societe AnonymeInventor: Axel Kupisiewicz
-
Publication number: 20030191410Abstract: A method is presented for determining diastolic intracranial pressure (ICP) in a patient. A first change in the length of a path across the skull of the patient caused by a known change in ICP is measured and used to determine an elasticity constant for the patient. Next, a second change in the length of the path across the patient's skull occurring between systolic and diastolic portions of the patient's heartbeat is measured. The patient's diastolic ICP is a function of the elasticity constant and the second change.Type: ApplicationFiled: September 25, 2002Publication date: October 9, 2003Applicant: National Aeronautics and Space Administration as represented by the Administrator (NASA)Inventors: William T. Yost, John H. Cantrell, Alan R. Hargens
-
Publication number: 20030191411Abstract: A method is presented for determining absolute intracranial pressure (ICP) in a patient. Skull expansion is monitored while changes in ICP are induced. The patient's blood pressure is measured when skull expansion is approximately zero. The measured blood pressure is indicative of a reference ICP value. Subsequently, the method causes a known change in ICP and measures the change in skull expansion associated therewith. The absolute ICP is a function of the reference ICP value, the known change in ICP and its associated change in skull expansion, and a measured change in skull expansion.Type: ApplicationFiled: September 25, 2002Publication date: October 9, 2003Applicant: National Aeronautics and Space Administration as represented by the Administrator (NASA)Inventors: William T. Yost, John H. Cantrell, Alan R. Hargens
-
Publication number: 20030191409Abstract: 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. In one embodiment, the method comprises the steps of transmitting an ultrasonic bulk compressional wave onto the surface of the skull at a predetermined angle with respect to the skull so as to produce a surface wave, receiving the surface wave at an angle with respect to the skull which is substantially the same as the predetermined angle and at a location that is a predetermined distance from where the ultrasonic bulk compressional wave was transmitted upon the skull, determining the retardation or advancement in phase of the received surface wave with respect to a reference phase, and processing the determined retardation or advancement in phase to determine circumferential expansion or contraction of the skull and utilizing the determined circumferential change to determine the change in intracranial pressure.Type: ApplicationFiled: April 4, 2002Publication date: October 9, 2003Applicant: National Aeronautics and Space AdministrationInventors: William T. Yost, John H. Cantrell
-
Patent number: 6629341Abstract: A method for fabricating a piezoelectric macro-fiber composite actuator comprises providing a piezoelectric material that has two sides and attaching one side upon an adhesive backing sheet. The method further comprises slicing the piezoelectric material to provide a plurality of piezoelectric fibers in juxtaposition. A conductive film is then adhesively bonded to the other side of the piezoelectric material, and the adhesive backing sheet is removed. The conductive film has first and second conductive patterns formed thereon which are electrically isolated from one another and in electrical contact with the piezoelectric material. The first and second conductive patterns of the conductive film each have a plurality of electrodes to form a pattern of interdigitated electrodes. A second film is then bonded to the other side of the piezoelectric material. The second film may have a pair of conductive patterns similar to the conductive patterns of the first film.Type: GrantFiled: October 29, 1999Date of Patent: October 7, 2003Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: W. Keats Wilkie, Robert G. Bryant, Robert L. Fox, Richard F. Hellbaum, James W. High, Antony Jalink, Jr., Bruce D. Little, Paul H. Mirick
-
Patent number: 6629446Abstract: A single vector calibration system is provided which facilitates the calibration of multi-axis load cells, including wind tunnel force balances. The single vector system provides the capability to calibrate a multi-axis load cell using a single directional load, for example loading solely in the gravitational direction. The system manipulates the load cell in three-dimensional space, while keeping the uni-directional calibration load aligned. The use of a single vector calibration load reduces the set-up time for the multi-axis load combinations needed to generate a complete calibration mathematical model. The system also reduces load application inaccuracies caused by the conventional requirement to generate multiple force vectors. The simplicity of the system reduces calibration time and cost, while simultaneously increasing calibration accuracy.Type: GrantFiled: January 8, 2001Date of Patent: October 7, 2003Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Peter A. Parker