Patents Assigned to Administration
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Patent number: 5003235Abstract: The invention, a single element magnetic suspension actuator with bidirectional force capability along a single axis, includes an electromagnet 11 and a nonmagnetic suspended element 12. A permanent magnet 13 mounted on the suspended element 12 interacts with a magnetic field established by the electromagnet 11 to produce bidirectional forces in response to a variable force command voltage V.sub.FC applied to the electromagnet 11. A sensor 14 measures the position of the suspended element 12 on the single axis which is a function of force command voltage V.sub.FC.Type: GrantFiled: September 11, 1989Date of Patent: March 26, 1991Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Nelson J. Groom
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Patent number: 5003011Abstract: A decapeptide of the formula:N-Ac-A.sup.1 -A.sup.2 -A.sup.3 -SER.sup.4 -A.sup.5 -A.sup.6 -A.sup.7 -A.sup.8 -A.sup.9 -A.sup.10,wherein each A.sup.1, A.sup.2, and A.sup.3, independently, is D-.beta.-Nal, D-p-X-Phe (where X is halogen, H, NH.sub.2, NO.sub.2, OH, or C.sub.1-3 alkyl); A.sup.5 is p-X-Phe (where X is halogen, H, NH.sub.2, NO.sub.2, OH, or C.sub.1-3 alkyl); A.sup.6 is D-Lys, D-Arg, .beta.-Nal, D-.beta.-Nal, D-Trp, D-p-X-Phe (where X is halogen, H, NH.sub.2, NO.sub.2, or C.sub.1-3 alkyl) or D-lys-.epsilon.-NH-R (where R is H, a branched or straight chain or cyclo C.sub.1 -C.sub.10 alkyl group, or an aryl group); A.sup.7 is p-X-Phe (where X is halogen, H, NH.sub.2, NO.sub.2, OH, C.sub.2 F.sub.5, or C.sub.1-3 alkyl), cyclohexyala, or Trp; A.sup.8 is Arg, Lys, or Lys-.epsilon.-NH-R (where R is H, a branched or straight chain or cyclo C.sub.1 -C.sub.10 alkyl group, or an aryl croup); A.sup.9 is Pro; and A.sup.10 is D-Ala-NH.sub.2, Gly-NH.sub.2, D-Ser, or D-Ser-NH.sub.2 ; provided that at least one of A.Type: GrantFiled: October 13, 1989Date of Patent: March 26, 1991Assignee: The Administrators of the Tulane Educational FundInventors: David H. Coy, Jacques-Pierre Moreau
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Patent number: 5002890Abstract: A spiral vane bioreactor of a perfusion type in which a vertical chamber (10), intended for use in a microgravity condition, has a central rotating filter assembly (30) and has flexible membranes (56) disposed to rotate annularly about the filter assembly. The flexible members have end portions disposed angularly with respect to one another. A fluid replenishment medium is input (68) from a closed loop liquid system to a completely liquid filled chamber containing microcarrier beads, cells and a fluid medium. Output (36) of spent medium is to the closed loop. In the closed loop, the output and input parameters are sensed by sensors (82,96); a manifold 86 permits recharging of the nutrients and pH adjustment; oxygen is supplied and carbon dioxide removed, bubbles are removed and the system is monitored and controlled by a microprocessor (100).Type: GrantFiled: November 29, 1988Date of Patent: March 26, 1991Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Dennis R. Morrison
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Patent number: 5000033Abstract: An apparatus for testing O-ring gaskets under a variety of temperature, pressure, and dynamic loading conditions. Specifically, this apparatus has the ability to simulate a dynamic loading condition where the sealing surface in contact with the O-ring moves both away from and axially along the face of the O-ring.Type: GrantFiled: June 5, 1989Date of Patent: March 19, 1991Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: James E. Turner, Donald S. McCluney
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Patent number: 5000416Abstract: An alignment positioning mechanism for correcting and compensating for misalignment of structures to be coupled thereby. The mechanism comprises a power screw 12 with a base portion 13 and a threaded shank portion 14. A mounting fixture 18 is provided for rigidly coupling said base portion to the mounting interface of a supporting structure with the axis of the screw perpendicular thereto. A traveling ball nut 40 threaded on the power screw 12 is formed with an external annular arcuate surface 41 configured in the form of a spherical segment and enclosed by a ball nut housing 50 with a conforming arcuate surface 51 for permitting gimballed motion thereon. The ball nut housing 50 is provided with a mounting surface 53a which is positionable in cooperable engagement with the mounting interface of a primary structure to be coupled to said supporting structure.Type: GrantFiled: January 26, 1990Date of Patent: March 19, 1991Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Peter M. Fantasia
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Patent number: 4998842Abstract: A quick-connect fastener is arranged with a tubular body that is arranged to be engaged against the exterior surface of a hollow attachment fitting and coincidentally aligned with an opening in the fitting. A collet having normally-contracted fingers with outwardly-enlarged ends is operatively arranged in the body to be moved forwardly by an expander member mounted in the tubular body for advancing the collet fingers through the opening in the attachment fitting. Biasing means are arranged between the expander member and a toggle linkage in the tubular body which is selectively operated to urge the expander member forwardly into engagement with the collet fingers with an initial biasing force to advance their forward portions through the body opening and then expand them outwardly. The biasing means also provide a subsequent biasing force for retaining the collet members in their expanded positions once their enlarged forward end portions are on the opposite side of the body.Type: GrantFiled: April 30, 1990Date of Patent: March 12, 1991Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Philip L. Sheridan
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Patent number: 4999553Abstract: A method and apparatus to control a robot or manipulator configuration over the entire motion based on augmentation of the manipulator forward kinematics. A set of kinematic functions is defined in Cartesian or joint space to reflect the desirable configuration that will be achieved in addition to the specified end-effector motion. The user-defined kinematic functions and the end-effector Cartesian coordinates are combined to form a set of task-related configuration variables as generalized coordinates for the manipulator. A task-based adaptive scheme is then utilized to directly control the configuration variables so as to achieve tracking of some desired reference trajectories throughout the robot motion. This accomplishes the basic task of desired end-effector motion, while utilizing the redundancy to achieve any additional task through the desired time variation of the kinematic functions.Type: GrantFiled: December 28, 1989Date of Patent: March 12, 1991Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Homayoun Seraji
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Patent number: 4997158Abstract: A mechanical strain isolator mount 10 is provided to preserve the alignmental integrity of alignment sensitive instrument 25. Alignment sensitive instrument 25 is mounted on rectangular base 11. Flexural legs 15, 16, and 17 are connected at their proximal ends to rectangular base 11 at points, A, B, C, respectively. Flexural legs 15, 16, and 17 are also spaced parallel to sides AB, BC, and CD respectively. Mounting pads 20, 21, and 22 are respectively connected to legs 15, 16, and 17 at the distal ends thereof and attach mechanical strain isolator mount 10 to substrate 30 by means of threaded bolts 23. When a mounting pad and its respective leg is subjected to lateral strains in either the X or Y directon via substrate 30, the respective leg relieves the strain by bending in the direction of the strain. An axial strain on a mounting pad in the Z direction is relieved by a rotational motion of legs 15, 16, and 17 in the direction of the strain.Type: GrantFiled: November 27, 1989Date of Patent: March 5, 1991Assignee: The United States of America as represented by the Administrator, of the National Aeronautics and Space AdministrationInventor: Gordon E. James
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Patent number: 4997297Abstract: This invention consists of a bearing (26) designed to operate in a cryogenic environment and which has an inner raceway (30) generally constructed as an annular band fitted by an interference fit to a rotating shaft (12). A pair of annular tension bands (32, 34) are fitted onto opposed sides of the band and function to firmly clamp the raceway (30) to the shaft (12). This occurs because the tension bands are constructed of a material which, when cooled to aproximately -385.degree. F., shrinks more than the raceway (30) and the shaft (12) to which it is fitted. The bands further relax somewhat at room temperature and permit the interference fit between the raceway (30) and the shaft (12) to be sized such that the raceway (30) is not overly stessed.Type: GrantFiled: January 31, 1990Date of Patent: March 5, 1991Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Dale H. Blount
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Patent number: 4995272Abstract: A low frequency torsional suspension system for testing a space structure uses a plurality of suspension stations attached to the space structure along the length thereof in order to suspend the space structure from an overhead support. Each suspension station includes a disk pivotally mounted to the overhead support, and two cables which have upper ends connected to the disk and lower ends connected to the space structure. The two cables define a parallelogram with the center of gravity of the space structure being vertically beneath the pivot axis of the disk. The vertical distance between the points of attachment of the cables to the disk and the pivot axis of the disk is adjusted to lower the frequency of the suspension system to a level which does not interfere with frequency levels of the space structure, thereby enabling accurate measurement.Type: GrantFiled: May 26, 1989Date of Patent: February 26, 1991Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Wilmer H. Reed, III, Ronald R. Gold
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Patent number: 4995700Abstract: A magnetically operated shutter mechanism is provided that will function in cryogenic or cryogenic zero gravity environments to selectively block radiation such as light from passing through a window to a target object such as a mirror or detector located inside a cryogenic container such as a dewar. The mechanism includes a shutter paddle blade that is moved by an electromagnetically actuated torquing device between an open position where the target object is exposed to ambient radiation or light and a closed position where the shutter paddle blade shields the ambient radiation or light from the target object. The purpose of the shuttering device is to prevent the mirror or other target object from being directly exposed to radiation passing through the window located on the side wall of the dewar, thereby decreasing or eliminating any temperature gradient that would occur within the target object due to exposure to the radiation.Type: GrantFiled: March 31, 1989Date of Patent: February 26, 1991Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Richard D. Barney, Thomas J. Magner
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Patent number: 4995697Abstract: A fiber optic interferometer utilizes a low coherence LED laser as a light source which is filtered and driven at two RF frequencies, high and low, that are specific to the initial length of the resonator chamber. A displacement of a reflecting mirror changes the length traveled by the nonreferencing signal. The low frequency light undergoes destructive interference which reduces the average intensity of the wave while the high frequency light undergoes constructive interference which increases the average intensity of the wave. The ratio of these two intensity measurements is proportional to the displacement incurred.Type: GrantFiled: September 7, 1989Date of Patent: February 26, 1991Assignee: The United States of America as represented by the administrator of the National Aeronautics and Space AdministrationInventor: Grigory Adamovsky
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Patent number: 4991799Abstract: An orbital debris sweeper is provided for removing particles from orbit which otherwise may impact and damage an orbiting spacecraft. The debris sweeper includes a central sweeper core which carries a debris monitoring unit, and a plurality of large area impact panels rotatable about a central sweeper rotational axis. In response to information from the debris monitoring unit, a computer determines whether individual monitored particles preferably impact one of the rotating panels or pass between the rotating panels. A control unit extends or retracts one or more booms which interconnect the sweeper core and the panels to change the moment of inertia of the sweeper and thereby the rotational velocity of the rotating panels.Type: GrantFiled: February 16, 1990Date of Patent: February 12, 1991Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Andrew J. Petro
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Patent number: 4992528Abstract: A graphite fiber reinforced polymer matrix is layed up, cured, and thermally aged at about 750.degree. F. in the presence of an inert gas. The heat treatment improves the structural integrity and alters the electrical conductivity of the materials. In the preferred embodiment PMR-15 polyimides and Celion-6000 graphite fibers are used.Type: GrantFiled: December 5, 1988Date of Patent: February 12, 1991Assignee: The United States of America, as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Kenneth J. Bowles, Carl E. Lowell
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Patent number: 4989715Abstract: A method and a detector for controlling coins inserted into a slot of a device are disclosed, in which a device for imparting oscillations to a coin is arranged, The frequency of oscillations is measured and compared with a predetermined value in an electronic device which actuates a coin separating device which guides unsuitable coins into a separation passage.Type: GrantFiled: August 22, 1988Date of Patent: February 5, 1991Assignee: Grunig AdministrationInventor: Dieter Grunig
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Patent number: 4990922Abstract: This is a system for measuring ocean surface currents from an airborne platform. A radar system having two spaced antennas wherein one antenna is driven and return signals from the ocean surface are detected by both antennas is employed to get raw ocean current data which is saved for later processing. There are a pair of GPS systems including a first antenna carried by the platform at a first location and a second antenna carried by the platform at a second location displaced from the first antenna for determining the position of the antennas from signals from orbiting GPS navigational satellites. This data is also saved for later processing. The saved data is subsequently processed by a ground-based computer system to determine the position, orientation, and velocity of the platform as well as to derive measurements of currents on the ocean surface.Type: GrantFiled: March 14, 1990Date of Patent: February 5, 1991Assignee: The United States of America as represented by the Administrator, National Aeronautics and Space AdministrationInventors: Lawrence E. Young, Jeffrey M. Srinivasan, Thomas K. Meehan, Timothy N. Munson, George H. Purcell, Jr., Jess B. Thomas, Courtney B. Duncan
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Patent number: 4990312Abstract: In the preferred embodiment of the promoted combustion chamber disclosed herein, a thick-walled tubular body that is capable of withstanding extreme pressures is arranged with removable upper and lower end closures to provide access to the chamber defined within the body. A bracket is arranged in the chamber for dependently supporting a test sample of a material being evaluated in the chamber. To facilitate the real-time analysis of a test sample, several pressure-tight viewing ports capable of withstanding the simulated environmental conditions are arranged in the walls of the tubular body for observing the test sample during the course of a test. A replaceable heat-resistant tubular member and replaceable flame-resistant internal liners are arranged to be fitted inside of the chamber for protecting the interior wall surfaces of the combustion chamber during the evaluation tests.Type: GrantFiled: July 18, 1989Date of Patent: February 5, 1991Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Michelle A. Rucker, Joel M. Stoltzfus
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Patent number: 4990739Abstract: An improved plasma gun coaxially injects particles of ceramic materials having high melting temperatures into the central portion of a plasma jet. This results in a more uniform and higher temperature and velocity distribution of the sprayed particles. The position of the cathode is adjustable to facilitate optimization of the performance of the gun wherein grains of the ceramic material are melted at lower power input labels.Type: GrantFiled: July 7, 1989Date of Patent: February 5, 1991Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Isidor Zaplatynsky
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Patent number: 4991181Abstract: A catalyst for the combination of CO and O.sub.2 to form CO.sub.2 which includes a platinum group metal--e.g., platinum; a reducible metal oxide having multiple valence states--e.g., SnO.sub.2 ; and a compound which can bind water to its structure--e.g., silica gel. This catalyst is ideally suited for application to high-powered, pulsed, CO.sub.2 lasers operating in a sealed or closed-cycle condition.Type: GrantFiled: November 30, 1989Date of Patent: February 5, 1991Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Billy T. Upchurch, Irvin M. Miller, David R. Brown, Patricia P. Davis, David R. Schryer, Kenneth G. Brown, John D. Van Norman
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Patent number: 4990988Abstract: Laterally stacked Schottky diodes (25) for infrared sensor applications are fabricated utilizing porous silicon (10) having pores (12). A Schottky metal contact (24) is formed in the pores, such as by electroplating. The sensors may be integrated with silicon circuits on the same chip with a high quantum efficiency, which is ideal for IR focal plane array applications due to uniformity and reproducibility.Type: GrantFiled: June 9, 1989Date of Patent: February 5, 1991Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: True-Lon Lin