Patents Assigned to Administration
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Patent number: 5020739Abstract: An emergency spin recovery parachute is housed within a centrally mounted housing on the aft end of an aircraft and is connected to a ring fitting within the housing. Two selectively latching shackles, connected to separate towlines are openly disposed adjacent the ring fitting. The towlines extend in opposite directions from the housing along the aircraft wing to attachment points adjacent the wing-tips, where the other end of each towline is secured. Upon pilot command, one of the open shackles latches to the ring fitting to attach the towline connected thereto, and a second command signal deploys the parachute. Suitable break-away straps secure the towlines to the aircraft surface until the parachute is deployed and the resulting force on the towline attached to the parachute overcomes the straps and permits the towline to extend to the point of attachment to exert sufficient drag on the spinning aircraft to permit the pilot to regain control of the aircraft.Type: GrantFiled: October 25, 1990Date of Patent: June 4, 1991Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Daniel M. Vairo, Raymond D. Whipple
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Patent number: 5020743Abstract: An acceleration free research laboratory is provided that is confined within a satellite but free of any physical engagement with the walls of the satellite, wherein the laboratory has adequate power, heating cooling and communications services to conduct basic research and development.An inner part containing the laboratory is positioned at the center-of-mass of a satellite within the satellite's outer shell. The satellite is then positioned such that its main axes are in a position parallel to its main axes are in a position parallel to its flight velocity vector or in the direction of the residual acceleration vector. When the satellite is in its desired orbit, the inner part is set free so as to follow that orbit without contacting the inside walls the outer shell.Type: GrantFiled: April 28, 1989Date of Patent: June 4, 1991Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Friedrich O. von Bun, Owen K. Garriott
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Patent number: 5020742Abstract: This airborne rescue system includes a boom (25) with telescoping members (31) for extending a line (19) and collar (14) to a rescue victim (16). The boom extends beyond the tip of the helicopter rotor (18) so that the victim may avoid in the rotor downwash. The rescue line is payed out and reeled in by winch (23). The line is temporarily retained under boom (25). When the boom is extended, the rescue line passes through clips (28). When the victim dons the collar and the tension in the line reaches a predetermined level, the clips open and release the line from the boom. Then the rescue line can form a straight line between the victim and the winch, and the victim can be lifted to the helicopter. A translator (57) is utilized to push out or pull in the telescoping members. The translator comprises a tape (58) and a rope (59). Inside the telescoping members the tape is curled around the rope and the tape has a tube-like configuration. The tape and rope are provided from supply spools 81 and 82, respectively.Type: GrantFiled: October 6, 1989Date of Patent: June 4, 1991Assignee: The United States of America as represented by the Administrator of National Aeronautics and Space AdministrationInventor: Leonard A. Haslim
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Patent number: 5021518Abstract: Ethynyl terminated imidothioethers (ETIs) are prepared by the reaction of a dimercaptan, such as 4,4'-dimercaptodiphenyl ether, and an ethynyl containing maleimide, such as N-(3-ethynylphenyl)maleimide. Blends of these ETIs and ethynyl terminated polymeric materials, such as ethynyl terminated sulfones and ethynyl terminated arylene ethers, are also prepared. These resin blends exhibit excellent processability, and the cured blends show excellent fracture toughness and solvent resistance, as well as excellent adhesive and composite properties.Type: GrantFiled: May 4, 1989Date of Patent: June 4, 1991Assignee: The United States of America as represented by the Adm inistration of the National Aeronautics and Space AdministrationsInventors: Paul M. Hergenrother, John W. Connell, R. Gerald Bass
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Patent number: 5021065Abstract: A prosthetic device for below-the-elbow amputees having a cuff, a stem, a housing, two hook-like fingers, an elastic band for holding the fingers together, and a brace. The fingers are pivotally mounted on a housing that is secured to the amputee's upper arm with the brace. The stem, which also contains a cam, is rotationally mounted within the housing and is secured to the cuff, which fits over the amputee's stump. By rotating the cammed stem between the fingers with the lower arm, the amputee can open and close the fingers.Type: GrantFiled: April 12, 1990Date of Patent: June 4, 1991Assignee: The United States of America as represented by the Administrator, National Aeronautics and Space AdministrationInventors: William E. Norton, Jewell G. Belcher, Jr., James R. Carden, Thomas W. West
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Patent number: 5020774Abstract: A flow regulator for high-pressure fluids at elevated temperatures includes a body having a flow passage extending between inlet and outlet openings. First and second orifice members are arranged in the flow passage so at least one of the orifice members can be moved transversely in relation to the flow passage between one operating position where the two orifice openings are aligned for establishing a maximum flow rate of fluids flowing through the flow passage and at least one other operating position in which the two openings are moderately misaligned with one another for establishing a predetermined reduced flow rate of fluids flowing through the flow passage.Type: GrantFiled: April 11, 1990Date of Patent: June 4, 1991Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Rollin C. Christianson
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Patent number: 5019176Abstract: A thin, lightweight solar cell utilizes front contact metallization. Both the front light receiving surface of the solar cell and the facing surface of the cover glass are recessed to accommodate this metallization. This enables the two surfaces to meet flush for an optimum seal.Type: GrantFiled: March 20, 1990Date of Patent: May 28, 1991Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Henry W. Brandhorst, Jr., Irving Weinberg
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Patent number: 5018688Abstract: A device for reducing drag and store separation difficulties caused by shallow cavities on aircraft in supersonic flight consisting of a slab of porous material cut to fit precisely inside the cavity. This slab is mounted inside the cavity such that a plenum chamber is formed between the slab and the floor of the cavity. This device allows air to flow through the chamber opposite to the direction of flow outside the chamber. This results in reduced drag and improved store separation characteristics.Type: GrantFiled: September 28, 1988Date of Patent: May 28, 1991Assignee: The United States of America as represented by the Administrator of the National AeronauticsInventors: Robert L. Stallings, Jr., Floyd J. Wilcox, Jr.
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Patent number: 5018852Abstract: A method and apparatus for detecting and tracking moving objects in a noise environment cluttered with fast- and slow-moving objects and other time-varying background. A pair of phase conjugate light beams carrying the same spatial information commonly cancel each other out through an image subtraction process in a phase conjugate interferometer, wherein gratings are formed in a fast photorefractive phase conjugate mirror material. In the steady state, there is no output. When the optical path of one of the two phase conjugate beams is suddenly changed, the return beam loses its phase conjugate nature and the interferometer is out of balance, resulting in an observable output. The observable output lasts until the phase conjugate nature of the beam has recovered. The observable time of the output signal is roughly equal to the formation time of the grating.Type: GrantFiled: August 16, 1990Date of Patent: May 28, 1991Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Li-Jen Cheng, Tsuen-Hsi Liu
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Patent number: 5019533Abstract: Voids in aluminum metallization conductors on a chip are avoided or healed after the chip is subjected to thermal treatment at a high temperature sufficient to allow diffusion of silicon by rapidly cooling the chip, preferably by immersion of the chip in liquid nitrogen.Type: GrantFiled: May 26, 1989Date of Patent: May 28, 1991Assignee: The United States of America as represented by the adminstrator of the National Aeronautics and Space AdministrationInventors: Edward F. Cuddihy, Russell A. Lawton, Thomas R. Gavin
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Patent number: 5019470Abstract: In a method of fabricating a rechargeable battery which includes a positive electrode which contains a chloride of a selected metal when the electrode is in its active state, the improvement comprising fabricating the positive electrode by: providing a porous matrix composed of a metal; providing a solution of the chloride of the selected metal; and impregnating the matrix with the chloride from the solution.Type: GrantFiled: March 30, 1990Date of Patent: May 28, 1991Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Ratnakumar V. Bugga, Salvador DiStefano, C. Perry Bankston
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Patent number: 5019175Abstract: A method for the destruction of halogenated organic compounds contained in a contaminated medium comprises adding an aqueous solution of polyethylene glycol to the contaminated medium in an amount to provide from about 0.1 to about 20 weight percent of polyethylene glycol, based on the weight of the contaminated medium. An alkali metal hydroxide is then added in an amount of from about 2 to about 20 weight percent, based on the weight of the contaminated medium. The medium is then heated to substantially dehydrate the medium and then further heated at a temperature between about 100.degree. and 350.degree. C. to effect destruction of the halogenated organic compounds. An acid is then added to the medium in an amount sufficient to neutralize the same.Type: GrantFiled: May 11, 1989Date of Patent: May 28, 1991Assignee: The United States of America as represented by the Administrator, Environmental Protection AgencyInventors: Charles J. Rogers, Alfred Kornel, Harold L. Sparks
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Patent number: 5019824Abstract: A multistage estimator is provided for the parameters of a received carrier signal possibly phase-modulated by unknown data and experiencing very high Doppler, Doppler rate, etc., as may arise, for example, in the case of Global Positioning Systems (GPS) where the signal parameters are directly related to the position, velocity and jerk of the GPS ground-based receiver. In a two-stage embodiment of the more general multistage scheme, the first stage, selected to be a modified least squares algorithm referred to as differential least squares (DLS), operates as a coarse estimator resulting in higher rms estimation errors but with a relatively small probability of the frequency estimation error exceeding one-half of the sampling frequency, provides relatively coarse estimates of the frequency and its derivatives.Type: GrantFiled: May 1, 1990Date of Patent: May 28, 1991Assignee: The United States of America as represented by the Administrator, National Aeronautics and Space AdministrationInventor: Rajendra Kumar
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Patent number: 5016418Abstract: A deployable structure that synchronously deploys in both length and width is disclosed which is suitable for use as a structural component for orbiting space stations or large satellites. The structure is designed with maximum packing efficiency so that large structures may be collapsed and transported in the cargo bay of the Space Shuttle. The synchronous deployment feature allows the structure to be easily deployed in space without a complex deployment mechanism. The structure is made up of interconnected structural units, each generally in the shape of a parallelepiped. The structural units are constructed of structural members connected with hinged and fixed connections at connection nodes in each corner of the parallelepiped. Diagonal members along each face of the parallelepiped provide structural rigidity and are equipped with mid-length, self-locking hinges to allow the structure to collapse.Type: GrantFiled: August 22, 1986Date of Patent: May 21, 1991Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Marvin D. Rhodes, John M. Hedgepeth
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Patent number: 5017883Abstract: A differential detection technique for MPSL signals is provided which uses a multiple symbol observation interval on the basis of which a joint decision is made regarding the phase of the received symbols. In accordance with the invention, a first difference phase is created between first and second received symbols. Next the first difference phase is correlated with the possible values thereof to provide a first plurality of intermediate output signals. A second difference phase is next created between second and third received symbols. The second difference phase is correlated with plural possible values thereof to provide a second plurality of intermediate output signals. Next, a third difference phase is created between the first and third symbols. The third difference phase is correlated with plural possible values thereof to provide a third plurality of intermediate output signals.Type: GrantFiled: July 31, 1990Date of Patent: May 21, 1991Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Dariush Divsalar, Marvin K. Simon
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Patent number: 5017549Abstract: An electromagnetic projectile launcher provides acceleration of a superconducting projectile through the diamagnetic repulsion of the superconducting projectile. A superconducting layer is provided aft of the projectile, either directly on the projectile or on a platform upon which the projectile is carried, and a travelling magnetic field is caused to propagate along a magnetic field drive coil in which the projectile is disposed. The resulting diamagnetic repulsion between the superconducting projectile and the travelling magnetic field causes the projectile to be propelled along the coil. In one embodiment, a segmented drive coil is used to generate the travelling magnetic field.Type: GrantFiled: October 31, 1989Date of Patent: May 21, 1991Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Glen A. Robertson
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Patent number: 5015963Abstract: A synchronous demodulator includes a switch which is operated in synchronism with an incoming periodic signal and both divides and applies that signal to two signal channels. The two channels each include a network for computing and holding, for a predetermined length of time, the average signal value on that channel and applies those values, in the form of two other signals, to the inputs of a diffferential amplifier. The networks may be R-C networks. The output of the differential amplifier may or may not form the output of the synchronous detector and may or may not be filtered. The output will not include a periodic signal due to the presence of a dc offset. Additionally, the output will not contain any substantial ripple due to periodic components in the input signal.Type: GrantFiled: September 29, 1989Date of Patent: May 14, 1991Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: John F. Sutton
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Patent number: 5016063Abstract: An electronic shift register memory (20) at the molecular level is described. The memory elements are based on a chain of electron transfer molecules (22) and the information is shifted by photoinduced (26) electron transfer reactions. Thus, multi-step sequences of charge transfer reactions are used to move charge with high efficiency down a molecular chain. The device integrates compositions of the invention onto a VLSI substrate (36), providing an example of a "molecular electronic device" which may be fabricated. Three energy level schemes, molecular implementation of these schemes, optical excitation strategies, charge amplification strategies, and error correction strategies are described.Type: GrantFiled: August 14, 1989Date of Patent: May 14, 1991Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: David N. Beratan, Jose N. Onuchic
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Patent number: 5014917Abstract: This device seals the sliding interfaces between structural panels that are roughly perpendicular to each other or whose edges are butted against one another. The seal is mounted in a rectangular groove in a movable structural panel and comprises a plurality of particles or balls densely packed in an outer sheathing. The balls are laterally preloaded to maintain sealing contact with the adjacent wall using a pressurized linear bellows. Distortions in the adjacent panel are accommodated by rearrangement of the particles within the outer sheathing.Type: GrantFiled: November 27, 1989Date of Patent: May 14, 1991Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Paul J. Sirocky, Bruce M. Steinetz
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Patent number: 5015851Abstract: A slow positron beam generator uses a conductive source residing between two test films. Moderator pieces are placed next to the test films on the opposite side of the conductive source. A voltage potential is applied between the moderator pieces and the conductive source. Incident energetic positrons are, first, emitted from the conductive source, second, passed through test film, and then, third, isotropically strike moderator pieces before diffusing out of the moderator pieces as slow positrons. The slow positrons diffusing out of moderator pieces are attracted to the conductive source which is held at an appropriate potential below the moderator pieces. The slow positrons have to pass through the test films before reaching the conductive source. A voltage is adjusted so that the potential difference between the moderator pieces and the conductive source forces the positrons to stop in the test films.Type: GrantFiled: May 31, 1990Date of Patent: May 14, 1991Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Jag J. Singh, Abe Eftekhari, Terry L. St. Clair