Patents Assigned to The United States of America as represented by the Administration of the National Aeronautics and Space Administration
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Patent number: 9650127Abstract: A stretchable mesh material extends across the opening of a cavity of the landing gear of an aircraft when the landing gear is in the deployed position. The mesh material alters the flow of air across the opening of the landing gear cavity and significantly reduces the amount of noise produced by the wheel well at low-to-mid frequencies.Type: GrantFiled: March 11, 2014Date of Patent: May 16, 2017Assignee: THE UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATION OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONInventor: Mehdi R. Khorrami
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Patent number: 9373891Abstract: A device for at least one of receiving and transmitting electromagnetic radiation includes a feedhorn having a substantially smooth, electrically conducting inner surface extending from an open end to a feed end, the inner surface being substantially rotationally symmetrical about a longitudinal axis, wherein an orthogonal distance from a point on the longitudinal axis to the substantially smooth, electrically conducting inner surface increases monotonically as the point on the longitudinal axis is selected at successively greater distances from the feed end of the feedhorn towards the open end of the feedhorn such that a profile of the substantially smooth, electrically conducting inner surface of the feedhorn is monotonically increasing. The feedhorn has an operating bandwidth and the feedhorn provides a maximum of ?30 dB cross polarization response over at least 15% of the operating bandwidth.Type: GrantFiled: August 6, 2015Date of Patent: June 21, 2016Assignees: The Johns Hopkins University, The United States of America, As Represented by the Administration of the National Aeronautics and Space AdministrationInventors: Charles L. Bennett, Lingzhen Zeng, Edward J. Wollack, David T. Chuss
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Patent number: 8314201Abstract: Ceramic oxide aerogels incorporating periodically dispersed flexible linkages are provided. The flexible linkages impart greater flexibility than the native aerogels without those linkages, and have been shown to reduce or eliminate the need for supercritical CO2-mediated drying of the corresponding wet gels. The gels may also be polymer cross-linked via organic polymer chains that are attached to and extend from surface-bound functional groups provided or present over the internal surfaces of a mesoporous ceramic oxide particle network via appropriate chemical reactions.Type: GrantFiled: November 30, 2007Date of Patent: November 20, 2012Assignees: The United States of America as represented by the Administration of the National Aeronautics and Space Administration, Ohio Aerosapce InstituteInventors: Mary Ann B. Meador, Baochau N. Nguyen
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Patent number: 7382944Abstract: Disclosed is a method of producing cones and pillars on polymethylmethacralate (PMMA) optical fibers for glucose monitoring. The method, in one embodiment, consists of using electron beam evaporation to deposit a non-contiguous thin film of aluminum on the distal ends of the PMMA fibers. The partial coverage of aluminum on the fibers is randomly, but rather uniformly distributed across the end of the optical fibers. After the aluminum deposition, the ends of the fibers are then exposed to hyperthermal atomic oxygen, which oxidizes the areas that are not protected by aluminum. The resulting PMMA fibers have a greatly increased surface area and the cones or pillars are sufficiently close together that the cellular components in blood are excluded from passing into the valleys between the cones and pillars. The optical fibers are then coated with appropriated surface chemistry so that they can optically sense the glucose level in the blood sample than that with conventional glucose monitoring.Type: GrantFiled: July 14, 2006Date of Patent: June 3, 2008Assignee: The United States of America as represented by the Administration of the National Aeronautics and Space AdministrationInventor: Bruce A. Banks
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Patent number: 7240879Abstract: This invention is a method and supporting apparatus for autonomously capturing, servicing and de-orbiting a free-flying spacecraft, such as a satellite, using robotics. The capture of the spacecraft includes the steps of optically seeking and ranging the satellite using LIDAR; and matching tumble rates, rendezvousing and berthing with the satellite. Servicing of the spacecraft may be done using supervised autonomy, which is allowing a robot to execute a sequence of instructions without intervention from a remote human-occupied location. These instructions may be packaged at the remote station in a script and uplinked to the robot for execution upon remote command giving authority to proceed. Alternately, the instructions may be generated by Artificial Intelligence (AI) logic onboard the robot. In either case, the remote operator maintains the ability to abort an instruction or script at any time, as well as the ability to intervene using manual override to teleoperate the robot.Type: GrantFiled: May 6, 2005Date of Patent: July 10, 2007Assignee: United States of America as represented by the Administration of the National Aeronautics and Space AdministrationInventors: Frank J. Cepollina, Richard D. Burns, Jill M. Holz, James E. Corbo, Nicholas M. Jedhrich
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Patent number: 7113820Abstract: Real time cardiac electrical data are received from a patient, manipulated to determine various useful aspects of the ECG signal, and displayed in real time in a useful form on a computer screen or monitor. The monitor displays the high frequency data from the QRS complex in units of microvolts, juxtaposed with a display of conventional ECG data in units of millivolts or microvolts. The high frequency data are analyzed for their root mean square (RMS) voltage values and the discrete RMS values and related parameters are displayed in real time. The high frequency data from the QRS complex are analyzed with imbedded algorithms to determine the presence or absence of reduced amplitude zones, referred to herein as “RAZs”. RAZs are displayed as “go, no-go” signals on the computer monitor. The RMS and related values of the high frequency components are displayed as time varying signals, and the presence or absence of RAZs may be similarly displayed over time.Type: GrantFiled: July 12, 2001Date of Patent: September 26, 2006Assignee: The United States of America as represented by the Administration of the National Aeronautics and Space AdministrationInventors: Todd T. Schlegel, Jude L. DePalma, Saeed Moradi
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Patent number: 7050161Abstract: An apparatus controls positions of plural mirror segments in a segmented mirror with an edge sensor system and a controller. Current mirror segment edge sensor measurements and edge sensor reference measurements are compared with calculated edge sensor bias measurements representing a global radius of curvature. Accumulated prior actuator commands output from an edge sensor control unit are combined with an estimator matrix to form the edge sensor bias measurements. An optimal control matrix unit then accumulates the plurality of edge sensor error signals calculated by the summation unit and outputs the corresponding plurality of actuator commands. The plural mirror actuators respond to the actuator commands by moving respective positions of the mirror segments. A predetermined number of boundary conditions, corresponding to a plurality of hexagonal mirror locations, are removed to afford mathematical matrix calculation.Type: GrantFiled: August 6, 2003Date of Patent: May 23, 2006Assignee: The United States of America as represented by the Administration of the National Aeronautics and Space AdministrationInventor: John M. Rakoczy
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Patent number: 6972056Abstract: A method for cleaning or otherwise removing amorphous carbon and other residues that arise in growth of a carbon nanotube (CNT) array. The CNT array is exposed to a plurality of hydroxyls or hydrogen, produced from a selected vapor or liquid source such as H2O or H2O2, and the hydroxyls or hydrogen (neutral or electrically charged) react with the residues to produce partly or fully dissolved or hydrogenated or hydroxylizated products that can be removed or separated from the CNT array. The hydroxyls or hydrogen can be produced by heating the CNT array, residue and selected vapor or liquid source or by application of an electromagnetic excitation signal with a selected frequency or range of frequencies to dissociate the selected vapor or liquid. The excitation frequency can be “chirped” to cover a selected range of frequencies corresponding to dissociation of the selected vapor or liquid. Sonication may be used to supplement dissociation of the H2O and/or H2O2.Type: GrantFiled: April 25, 2002Date of Patent: December 6, 2005Assignee: The United States of America as represented by the Administration of the National Aeronautics and Space AdministrationInventors: Lance D. Delzeit, Clement J. Delzeit
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Patent number: 6039930Abstract: A process for providing elemental metals or metal oxides distributed on a carbon substrate or self-supported utilizing graphite oxide as a precursor. The graphite oxide is exposed to one or more metal chlorides to form an intermediary product comprising carbon, metal, chloride, and oxygen This intermediary product can be flier processed by direct exposure to carbonate solutions to form a second intermediary product comprising carbon, metal carbonate, and oxygen. Either intermediary product may be further processed: a) in air to produce metal oxide; b) in an inert environment to produce metal oxide on carbon substrate; c) in a reducing environment to produce elemental metal distributed on carbon substrate. The product generally takes the shape of the carbon precursor.Type: GrantFiled: October 14, 1998Date of Patent: March 21, 2000Assignee: The United States of America as represented by Administration of the National Aeronautics and Space AdministrationInventor: Ching-Cheh Hung
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Patent number: 5949364Abstract: A method and system are provided to produce images of an object. A receiving station is positioned in view of a range-coded signal emitting satellite and the object. The receiving station is sensitive to direct transmission of the range-coded signal and reflections of the range-coded signal from the object. Both range from the receiving station to the object and a Doppler frequency shift history between the receiving station and the object is determined using the direct transmission and reflections of the range-coded signal. An image is formed using the two-dimensional record provided by the range and the Doppler frequency shift history.Type: GrantFiled: January 6, 1998Date of Patent: September 7, 1999Assignee: The United States of America as represented by the Administration of the National Aeronautics and Space AdministrationInventors: Stephen J. Katzberg, James L. Garrison, Jr.
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Patent number: 5608179Abstract: An ignitor initiates combustion of liquid propellant in a gun by utilizing a heated catalyst onto which the liquid propellant is sprayed in a manner which mitigates the occurrence of undesirable combustion chamber oscillations. The heater heats the catalyst sufficiently to provide the activation necessary to initiate combustion of the liquid propellant sprayed thereonto. Two embodiments of the ignitor and three alternative mountings thereof within the combustion chamber are disclosed. The ignitor may also be utilized to dispose of contaminated, excess, or waste liquid propellant in a safe, controlled, simple, and reliable manner.Type: GrantFiled: February 18, 1994Date of Patent: March 4, 1997Assignee: The United States of America as represented by the Administration of the National Aeronautics and Space AdministrationInventors: Gerald E. Voecks, Ned W. Ferraro
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Patent number: 5226447Abstract: A detection system is provided for sensing a malfunction of a valve having an outlet connected to an end of a first pipe through which pressurized fluid may be flowed in a downstream direction away from the valve. The system includes a bypass pipe connected at its opposite ends to the first pipe and operative to bypass a portion of the fluid flow therethrough around a predetermined section thereof. A housing is interiorly divided by a flexible diaphragm into first and second opposite chambers which are respectively communicated with the first pipe section and the bypass pipe, the diaphragm being spring-biased toward the second chamber. The diaphragm housing cooperates with check valves and orifices connected in the two pipes to create and maintain a negative pressure in the first pipe section in response to closure of the valve during pressurized flow through the first pipe. A pressure switch senses the negative pressure and transmits a signal indicative thereof to a computer.Type: GrantFiled: October 7, 1992Date of Patent: July 13, 1993Assignee: The United States of America as represented by the Administration of the National Aeronautics and Space AdministrationInventor: Richard K. Burley
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Patent number: 5188153Abstract: An apparatus and method for integral fill yarn insertion and beatup is provided. A modified rapier contains a channel for holding fill yarn. The channel is covered with a flexible and inflatable boot, and an inflating apparatus for this boot is also attached. Fill yarn is inserted into the channel, and the rapier is extended into a shed formed by warp yarn. Next, the rapier is pushed into the fell of the fabric, and the flexible and inflatable cover inflated, which both pushes the yarn into the fell of the fabric and performs beatup. The rapier is withdrawn and the shed closed to complete one step of the weaving process.Type: GrantFiled: September 26, 1991Date of Patent: February 23, 1993Assignee: The United States of America as represented by the Administration of the National Aeronautics and Space AdministrationInventor: Gary L. Farley
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Patent number: 4837300Abstract: Novel copolyimides are prepared by reacting one or more aromatic dianhydrides with a meta-substituted phenylene diamine and an aromatic bridged diamine. The incorporation of meta-substituted phenylene diamine derived units and bridged aromatic diamine derived units into the linear aromatic polymer backbone results in a copolyimide of improved flexibility, processability, and melt-flow characteristics. The novel copolyimides are especially useful as thermoplastic hot-melt adhesives.Type: GrantFiled: July 9, 1987Date of Patent: June 6, 1989Assignee: The United States of America as represented by the Administration of the National Aeronautics and Space AdministrationInventors: Terry L. St. Clair, Harold D. Burks, Donald J. Progar