Patents Assigned to Administration
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Patent number: 5116118Abstract: A sensor assembly to be carried on an aircraft or spacecraft which will travel along an arbitrary flight path, for providing an image of terrain over which the craft travels. The assembly includes a main linear sensor array and a plurality of auxiliary sensor arrays oriented parallel to, and at respectively different distances from, the main array. By comparing the image signals produced by the main sensor array with those produced by each auxiliary array, information relating to variations in velocity of the craft carrying the assembly can be obtained. The signals from each auxiliary array will provide information relating to a respectively different frequency range.Type: GrantFiled: June 28, 1990Date of Patent: May 26, 1992Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Kenneth L. Jones
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Patent number: 5116331Abstract: A silicon pressure die is bonded to a borosilicate substrate above a pneumatic port. A Wheatstone bridge circuit is formed on the silicon pressure die and has bridge elements of silicon doped with boron to a deposit density level of approximately 1.times.10.sup.19 -10.sup.21 boron/cm.sup.3. A current source is provided to excite the Wheatstone bridge circuit. In addition, a temperature sensor is provided to provide temperature readings.Type: GrantFiled: April 23, 1991Date of Patent: May 26, 1992Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: John J. Chapman
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Patent number: 5116939Abstract: A process for preparing polyimides having enhanced melt flow properties is described. The process consists of heating a mixture of a high molecular weight poly(amic acid) or polyimide with a low molecular weight amic acid or imide additive in the range of 0.05 to 15% by weight of additive. The polyimide powders so obtained show improved processability, as evidenced by lower melt viscosity by capillary rheometry. Likewise, films prepared from mixtures of polymers with additives show improved processability with earlier onset of stretching by TMA.Type: GrantFiled: August 11, 1987Date of Patent: May 26, 1992Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: James C. Fletcher, J. Richard Pratt, Terry L. St. Clair, Diane M. Stoakley, Harold D. Burks
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Patent number: 5113659Abstract: A plurality of heat pipes in a shell receive concentrated solar energy and transfer the energy to a heat activated system. To provide for even distribution of the energy despite uneven impingement of solar energy on the heat pipes, absence of solar energy at times, or failure of one or more heat pipes, energy storage means are disposed on the heat pipes which extend through a heat pipe thermal coupling means into the heat activated device. To enhance energy transfer to the heat activated device, the heat pipe coupling cavity means may be provided with extensions into the device. For use with a Stirling engine having passages for working gas, heat transfer members may be positioned to contact the gas and the heat pipes. The shell may be divided into sections by transverse walls. To prevent cavity workihg fluid from collecting to the extensions, a porous body is positioned in the cavity.Type: GrantFiled: March 27, 1991Date of Patent: May 19, 1992Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Karl W. Baker, Miles O. Dustin
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Patent number: 5113714Abstract: A joystick control device having a lower U-shaped bracket, an upper U-shaped bracket, a handle attached to the upper U-shaped bracket, with the upper U-shaped bracket connected to the lower U-shaped bracket by a compliant joint allowing six degrees of freedom for the joystick. The compliant joint consists of at least one cable segment affixed between the lower U-shaped bracket and the upper U-shaped bracket. At least one input device is located between the lower U-shaped bracket and the upper U-shaped bracket.Type: GrantFiled: February 20, 1991Date of Patent: May 19, 1992Assignee: The United States of America as represented by the Administrator of the National Aeronautics & Space AdministrationInventors: Wayne D. Eklund, James J. Kerley
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Patent number: 5112120Abstract: The invention is a natural flow wing and a method for constructing the same. The method comprises contouring a three-dimensional upper surface and a three-dimensional lower surface of the natural flow wing independently of one another into a prescribed shape. Experimental data and theoretical analysis show that flow and pressure-loading over an upper surface of a wing tend to be conical about an apex of the wing, producing favorable and unfavorable regions of performance based on drag. The method reduces these unfavorable regions by shaping the upper surface such that a maximum thickness near a tip of the natural flow wing moves aft, thereby contouring the wing to coincide more closely with the conical nature of the flow on the upper surface. Nearly constant compressive loading characterizes the flow field over a lower surface of the conventional wing.Type: GrantFiled: July 31, 1990Date of Patent: May 12, 1992Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Richard M. Wood, Steven X. S. Bauer
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Patent number: 5113064Abstract: A method and apparatus are disclosed for edge phasing an array of segments in a segmented primary telescope mirror using white light from a far field source and starting with the inner edge of each segment in the first ring of segments. The segments are individually phased for zero piston and tilt error with respect to the edge of a reference surface in the open center position of the telescope mirror, and proceeding from ring to ring by edge phasing one edge of each segment in each subsequent ring with an edge of a segment in a preceding ring that has been edge phased. After edge phasing of all segments in the telesope mirror array has been completed, full surface phasing can be achieved using a conventional Shack-Hartmann technique followed by finding the RMS best fit for each segment of the mirror array.Type: GrantFiled: March 6, 1991Date of Patent: May 12, 1992Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Paul K. Manhart
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Patent number: 5112923Abstract: Imide/arylene ether block copolymers are prepared by reacting anhydride terminated poly(amic acids) with amine terminated poly(arylene ethers) in polar aprotic solvents and chemically or thermally cyclodehydrating the resulting intermediate poly(amic acids). The resulting block copolymers have one glass transition temperature or two, depending upon the particular structure and/or the compatibility of the block units. Most of these block copolymers form tough, solvent resistant films with high tensile properties.Type: GrantFiled: November 21, 1989Date of Patent: May 12, 1992Assignee: Administrator of the National Aeronautics and Space AdministrationInventors: Brian J. Jensen, Paul M. Hergenrother, Robert G. Bass
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Patent number: 5112154Abstract: A connector assembly comprised of two halves, each respectively including a shell type connector sub-assembly, one being an active half and the other being a passive half. The active half includes an alignment cusp that causes a coupling motion in response to coming in contact with the outer portion of the other half which causes the respective connectors within the two sub-assemblies to move toward each other into coupling relationship at twice the rate at which the two sub-assemblies come together. Both halves are adapted to rotate about and translate along respective mutually orthogonal axes to facilitate an interconnection.Type: GrantFiled: December 31, 1990Date of Patent: May 12, 1992Assignee: The United States of America as represented by the Administrator, National Aeronautics and Space AdministrationInventor: Malcolm B. Milam
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Patent number: 5110436Abstract: This disclosure is directed to an electrolysis cell forming hydrogen and oxygen at spaced terminals. The anode terminal is porous and able to form oxygen within the cell and permit escape of the gaseous oxygen through the anode and out through a flow line in the presence of backpressure. Hydrogen is liberated in the cell at the opposing solid metal cathode which is permeable to hydrogen but not oxygen so that the migratory hydrogen formed in the cell is able to escape from the cell. The cell is maintained at an elevated pressure so that oxygen liberated by the cell is delivered at elevated pressure without pumping to raise the pressure of the oxygen.Type: GrantFiled: February 1, 1991Date of Patent: May 5, 1992Assignee: The United States of America as represented by the Adminstrator of the National Aeronautics and Space AdministrationInventors: Franz H. Schubert, David J. Grigger
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Patent number: 5111345Abstract: A disk memory device is provided that will maximize the storage capacity of a memory disk while at the same time maximize the record and playback data rate. Two recording disks are mounted upon a common shaft that is rotated at a fixed speed. Each disk has a recording area including a surface upon which data can be recorded/read in the form of tracks arranged either in concentric tracks or in a spiral. The recording area surfaces are divided into multiple concentric track groups. Two read/write heads and two head positioning servos (including electronic controls) are mounted such that each disk recording surface can be read out or written by the read/write heads. Each track of the multiple track groups of the first disk are given designated numbers beginning with the outer track of the outermost or edge track group and continuing in higher consecutive numbers until the inner track of the innermost track group is designated.Type: GrantFiled: May 26, 1989Date of Patent: May 5, 1992Assignee: The United States of America as represented by the Administrator, National Aeronautics & Space AdministrationInventor: Ronald M. Muller
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Patent number: 5110694Abstract: The conductivity is increased an order of magnitude and interfacial charge transfer resistance is substantially decreased by incorporating a minor amount of 12-Crown-4 ether in a polyethylene oxide-lithium salt solid electrolyte film.Type: GrantFiled: October 11, 1990Date of Patent: May 5, 1992Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Ganesan Nagasubramanian, Salvador DiStefano
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Patent number: 5108214Abstract: A coupling device with a thermal interface occuring along a curved vertical surface is disclosed. One curved surface is on a cold pin extending from a "cold" object and the other curved surface is on a hot pin extending from a "hot" object. The cold pin is fixed and does not move while the hot pin is a flexible member and its movement towards the cold pin will bring the two curved surfaces together forming the coupling and the thermal interface. The actuator member is a shape-memory actuation wire which is attached between the hot pin and the hot object. By properly programming the actuation wire, heat from the hot object will cause the actuation wire to move the hot pin towards the cold pin forming an effective thermal interface. The shape-memory actuation wire is made from a shape-memory-effect alloy such as Nitinol.Type: GrantFiled: June 13, 1991Date of Patent: April 28, 1992Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Malcolm B. Milam
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Patent number: 5109345Abstract: An autonomous docking system is provided which produces commands for the steering and propulsion system of a chase vehicle used in the docking of that chase vehicle with a target vehicle. The docking system comprises a passive optical target affixed to the target vehicle and comprising three reflective areas including a central area mounted on a short post, and tracking sensor and process controller apparatus carried by the chase vehicle.Type: GrantFiled: February 20, 1990Date of Patent: April 28, 1992Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Richard W. Dabney, Richard T. Howard
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Patent number: 5108568Abstract: A method of reducing electrophoretic mobility of macromolecules, particles, cells and other substances is provided which comprises interacting in a conventional electrophoretic separating procedure the substances with a polymer-linked affinity compound comprised of a hydrophilic neutral polymer such as polyethylene glycol bound to a second component such as a hydrophobic compound, an immunocompound such as an antibody or antibody active fragment, or a ligand such as a hormone, drug, antigen or a hapten. The reduction of electrophoretic mobility achieved is directly proportional to the concentration of the polymer-linked affinity compound employed, and such reduction can comprise up to 100% for particular particles and cells. The present invention is advantageous in that electrophoretic separation can now be achieved for substances whose native surface charge structure had prevented them from being separated by normal electrophoretic means.Type: GrantFiled: October 18, 1990Date of Patent: April 28, 1992Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: James M. Van Alstine
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Patent number: 5107920Abstract: Various heat exchange apparatuses are described in which an oscillating flow of primary coolant is used to dissipate an incident heat flux. The oscillating flow may be imparted by a reciprocating piston, a double action twin reciprocating piston, fluidic oscillators or electromagnetic pumps. The oscillating fluid flows through at least one conduit in either an open loop or a closed loop. A second flow of coolant may be used to flow over the outer walls of at least one conduit to remove heat transferred from the primary coolant to the walls of the conduit.Type: GrantFiled: March 30, 1990Date of Patent: April 28, 1992Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Stephen J. Scotti, Max L. Blosser, Charles J. Camarda
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Patent number: 5109425Abstract: A computer-simulated cortical network computes the visibility of shifts in the direction of movement and computes: 1) the magnitude of the position difference between the test and background patterns, 2) localized contrast differences at different spatial scales analyzed by computing temporal gradients of the difference and sum of the outputs of paired even- and odd-symmetric bandpass filters convolved with the input pattern and 3) using global processes that pool the output from paired even- and odd-symmetric simple and complex cells across the spatial extent of the background frame of reference to determine the direction a test pattern moved relative to a textured background. The direction of movement of an object in the field of view of a robotic vision system is detected in accordance with non-linear Gabor function algorithms. The movement of objects relative to their background is used to infer the 3-dimensional structure and motion of object surfaces.Type: GrantFiled: September 30, 1988Date of Patent: April 28, 1992Assignee: The United States of America as represented by the United States National Aeronautics and Space AdministrationInventor: Teri B. Lawton
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Patent number: 5107107Abstract: An angular position encoder is provided that minimizes the effects of eccentricity and other misalignments between the disk and the read stations by employing heads which incorporate beam steering optics with the ability to actively track the disk in directions along the disk radius and normal to its surface. The device adapts features prevalent in optical disk technology toward the application of angular position sensing. A reflective disk and the principles of interferometry are employed. The servo controlled steering optics move so as to acquire a track on the disk lying at a predetermined radius and distance below the head, and then adjust position and orientation in order to maintain view of the disk track as required. Thus, the device is actively self-aligning.Type: GrantFiled: March 30, 1990Date of Patent: April 21, 1992Assignee: The United States of America as represented by the Administarator of the National Aeronautics and Space AdministrationInventor: Eric P. Osborne
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Patent number: 5107526Abstract: A high resolution x-ray microscope for imaging microscopic structures within biological specimens has an optical system including a highly polished primary and secondary mirror coated with identical multilayer coatings, the mirrors acting at normal incidence. The coatings have a high reflectivity in the narrow wave bandpass between 23.3 and 43.7 angstroms and have low reflectivity outside of this range. The primary mirror has a spherical concave surface and the secondary mirror has a spherical convex surface. The radii of the mirrors are concentric about a common center of curvature on the optical axis of the microscope extending from the object focal plane to the image focal plane. The primary mirror has an annular configuration with a central aperture and the secondary mirror is positioned between the primary mirror and the center of curvature for reflecting radiation through the apertture to a detector.Type: GrantFiled: October 31, 1990Date of Patent: April 21, 1992Assignee: The United State of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Richard B. Hoover
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Patent number: 5104683Abstract: The invention is a multi-color luminescent display 10 comprising an insulator substrate 11 and a single layer of host material 13 which may be a phosphor deposited thereon that hosts one or more different impurities 14, therein forming a pattern of selected and distinctly colored phosphors such as blue, green and red phosphors in the single layer of host material 13. Transparent electrical conductor means 12 may be provided for subjecting selected portions of the pattern of colored phosphors to an electric field thereby forming a multi-color, single layer electroluminescent display.Type: GrantFiled: April 30, 1991Date of Patent: April 14, 1992Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: James B. Robertson