Patents Represented by Attorney, Agent or Law Firm Hardie R. Barr
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Patent number: 4974181Abstract: An adaptive data acquisition multiplexing system having a monitor terminal and one or more remote terminals with a communication link between them. The remote terminals each include signal conditioning for a plurality of sensors. Upon commands from the monitor terminal, signals providing the remote terminals' current configuration and status, and instructions for changing the remote terminal configuration, are transmitted from each remote terminal to the monitor terminal. Menu driven prompts at the monitor terminal permit commands to be transmitted from the monitor terminal to the remote terminals, selectively altering the configuration of any remote terminal to enable it to acquire and transmit data, as well as its configuration and status information, in the desired format. Alterations in any remote terminal's configuration can then be verified at the monitor terminal.Type: GrantFiled: April 15, 1988Date of Patent: November 27, 1990Assignee: The United States of America as represented by the Adminstrator, of the National Aeronautics and Space AdministrationInventors: Richard L. Sinderson, George A. Salazar, Clyde M. Haddick, Jr., Caroll J. Spahn, Chikkabelarangala N. Venkatesh
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Patent number: 4921292Abstract: A magnetic attachment mechanism adapted for interfacing with the manipulator arm (11) of a remote manipulator system and comprising a pair of permanent magnets (31,32) of rare earth material which are arranged in a stator-rotor relationship. The rotor magnet (32), is journalled for rotation about its longitudinal axis between pole plates (35,36) of the stator magnet (31), each of which includes an adhering surface (35a,36a). In a first rotary position corresponding to the "ON" condition, each of the poles of the rotor magnet (32) is closely adjacent a stator magnet pole plate of like polarity whereby the respective magnet fields are additive for producing a strong magnetic field emanating from the adhering surfaces (35a,36a) for attracting a ferrous magnetic plate 20, or the like, affixed to the payload (20 or 50).Type: GrantFiled: September 23, 1988Date of Patent: May 1, 1990Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: William D. Harwell, Mitchell B. Wu
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Patent number: 4920487Abstract: In a parallel processing computer system with multiple processing units and shared memory, a method is disclosed for uniformly balancing the aggregate computational load in, and utilizing a minimal memory by, a network having identical computations to be executed at each connection therein. Read-only and read-write memory are subdivided into a plurality of partitions, and the computational load is subdivided into a plurality of process sets, which function like artificial processing units. Said plurality of process sets is iteratively merged and reduced to the number of processing units without exceeding the balance load. Merger is based upon the value of a partition threshold, which is a measure of the memory utilization. The turnaround time and memory savings of the instant method are functions of the number of processing units available and the number of partitions into which memory is subdivided.Type: GrantFiled: December 12, 1988Date of Patent: April 24, 1990Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Paul T. Baffes
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Patent number: 4917173Abstract: A liquid supply control is disclosed for a heat transfer system which transports heat by liquid-vapor phase change of a working fluid. An assembly (10) of monogroove heat pipe legs (15) can be operated automatically as either heat acquisition devices or heat discharge sources. The liquid channels (27) of the heat pipe legs (15) are connected to a reservoir (35) which is filled and drained by respective filling and draining valves (30, 32). Information from liquid level sensors (50, 51) on the reservoir (35) is combined (60) with temperature information (55) from the liquid heat exchanger (12) and temperature information (56) from the assembly vapor conduit (42) to regulate filling and draining of the reservoir (35), so that the reservoir (35) in turn serves the liquid supply/drain needs of the heat pipe legs (15), on demand, by passive capillary action (20, 28).Type: GrantFiled: November 15, 1988Date of Patent: April 17, 1990Assignee: The United States of America as represented by the National Aeronautics and Space AdministrationInventors: Richard F. Brown, Fred Edelstein
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Patent number: 4893470Abstract: A technique for producing thrust by generating a hybrid plume plasma exhaust is disclosed. A plasma flow is generated and introduced into a nozzle which features one or more inlets positioned to direct a flow of neutral gas about the interior of the nozzle. When such a neutral gas flow is combined with the plasma flow within the nozzle, a hybrid plume is constructed including a flow of hot plasma along the center of the nozzle surrounded by a generally annular flow of neutral gas, with an annular transition region between the pure plasma and the neutral gas. The temperature of the outer gas layer is below that of the pure plasma and generally separates the pure plasma from the interior surfaces of the nozzle. The neutral gas flow both insulates the nozzle walls from the high temperatures of the plasma flow and adds to the mass flow rate of the hybrid exhaust. The rate of flow of neutral gas into the interior of the nozzle may be selectively adjusted to control the thrust and specific impulse of the device.Type: GrantFiled: September 23, 1988Date of Patent: January 16, 1990Assignee: The United States of America as represented by the Administrator, National Aeronautics and Space AdministrationInventor: Franklin R. Chang
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Patent number: 4890918Abstract: Improved techniques are provided for alignment of two objects. The present invention is particularly suited for three-dimensional translation and three-dimensional rotational alignment of objects in outer space. A camera 18 is fixedly mounted to one object, such as a remote manipulator arm 10 of the spacecraft, while the planar reflective surface 30 is fixed to the other object, such as a grapple fixture 20. A monitor 50 displays in real-time images from the camera, such that the monitor displays both the reflected image of the camera and visible markings on the planar reflective surface when the objects are in proper alignment. The monitor may thus be viewed by the operator and the arm 10 manipulated so that the reflective surface is perpendicular to the optical axis of the camera, the roll of the reflective surface is at a selected angle with respect to the camera, and the camera is spaced a pre-selected distance from the reflective surface.Type: GrantFiled: September 15, 1988Date of Patent: January 2, 1990Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Leo G. Monford
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Patent number: 4864847Abstract: A fluid leak indicator (30) for detecting and indicating leaks in visually inaccessible fluid tubing joints (20, 21), such as those obstructed by insulation (24), includes a bag system (25) and a wicking system (30) surrounding or wrapping the joints (20, 21) under the visual obstructing material (24). Leaking fluid is collected in the bag (25) or on the wicking material (34) where it is conducted along the wicking material (34) to a visibly accessible capturing transparent indicator bulb (35) for providing a visual indication of the leak without requiring a chemical change in the capturing indicator bulb (35).Type: GrantFiled: May 29, 1985Date of Patent: September 12, 1989Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: George E. Anderson, Shu Loo
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Patent number: 4860014Abstract: A microwave radar signal is generated (16) and split by a circular (20). A phase shifter (24) introduces a plurality of phase shifts into a first part of the split signal which is then transmitted (36) by antenna (34). A like plurality of phase shifts are introduced by the phase shifter into the return signal (40) from the target. The circulator delivers the phase shifted return signal and the leakage signal from the circulator to a mixer (44) which generates an i.f. signal output at the doppler frequency. The i.f. signal is amplified (46l ), filtered (54), counted (58) per unit of time and the result displayed (62) to provide indications of target sense and range rate. An oscillator (50) controls rate of phase shift in the transmitted and received signals and provides a time base for the counter. The phase shift magnitude increases may be continuous and linear or discrete functions of time.Type: GrantFiled: November 25, 1987Date of Patent: August 22, 1989Assignee: The United State of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Paul W. Shores, John W. Griffin, Herbert S. Kobayashi
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Patent number: 4832951Abstract: Apparatus and method of removing desirable constituents from an infusible material by infusion extraction, where a piston operating in a first chamber draws a solvent into the first chamber where it may be heated, and then moves the heated solvent into a second chamber containing the infusible material, and where infusion extraction takes place. The piston then moves the solvent containing the extract through a filter into the first chamber, leaving the extraction residue in the second chamber.Type: GrantFiled: November 10, 1987Date of Patent: May 23, 1989Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Franklin R. Chang-Diaz
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Patent number: 4818999Abstract: A system for deriving direct digital indications of frequency and phase difference between two incoming pulse trains adaptable for collision avoidance systems or the like.A pair of radar beams 152 and 152A are directed toward a target 153 and corresponding beams 154 and 154A returning therefrom are detected. A digital difference circuit 110 forms a pulse train 66 from the Doppler shift frequencies of each beam pair having a repetition rate functionally related to the difference in magnitude of the shift frequencies. Pulses from the pulse train are counted as a function of time. Visual indications thereof on display 144 are correlative to target position relative to beams 152 and 152A.Type: GrantFiled: October 29, 1986Date of Patent: April 4, 1989Assignee: The United States of America as represented by the Administrator of The National Aeronautics and Space AdministrationInventors: Herbert S. Kobayashi, Christopher L. Lichtenberg, Paul W. Shores, Allen R. Cunningham
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Patent number: 4815279Abstract: A technique for producing thrust by generating a hybrid plume plasma exhaust is disclosed. A plasma flow is generated and introduced into a nozzle which features one or more inlets positioned to direct a flow of neutral gas about the interior of the nozzle. When such a neutral gas flow is combined with the plasma flow within the nozzle, a hybrid plume is constructed including a flow of hot plasma along the center of the nozzle surrounded by a generally annular flow of neutral gas, with an annular transition region between the pure plasma and the neutral gas. The temperature of the outer gas layer is below that of the pure plasma and generally separates the pure plasma from the interior surfaces of the nozzle. The neutral gas flow both insulates the nozzle walls from the high temperatures of the plasma flow and adds to the mass flow rate of the hybrid exhaust. The rate of flow of neutral gas into the interior of the nozzle may be selectively adjusted to control the thrust and specific impulse of the device.Type: GrantFiled: April 13, 1987Date of Patent: March 28, 1989Assignee: The United States of America as represented by the National Aeronautics and Space AdministrationInventor: Franklin R. Chang
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Patent number: 4810438Abstract: An analytical technique for controlling the curing process of fiber-reinforced composite materials that are formed using thermosetting resins. The technique is the percent gel method and involves development of a time-to-gel equation as a function of temperature. From this equation a rate-of-gel equation is then determined, and a percent gel is calculated which is the product of rate-of-gel times time. Percent gel accounting is used to control the proper pressure application point in an autoclave cure process to achieve desired properties in a production composite part.Type: GrantFiled: April 30, 1987Date of Patent: March 7, 1989Assignee: The United States of America as represented by the United States National Aeronautics and Space AdministrationInventors: Charles N. Webster, Robert O. Scott
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Patent number: 4772893Abstract: A steerable multibeam five element cross-feed cluster antenna (16) system. The feed power is divided into five branches. Each branch includes a switching network (12A-12E) comprised of a plurality of time delay elements (90A; 92A) each individually controlled by a respective electromagnetic latching switch (56A,B; 58A,B; 60A,B; 62A,B; 46A,B). Frequency independent individual two-dimensional beam steering at IF scanning frequencies is thereby provided wherein discrete incremental time delays are introduced by the switching networks into each branch and the signals recombined thereafter to form each beam. The electromagnetic latched switching reduces power consumption and permits higher power switching and reciprocal coincident transmit and receive operation. Frequency independence due to incremental time delay switching permits coincident reciprocal operation and steering for transmit-receive signal paths carrying different transmit-receive frequencies.Type: GrantFiled: June 10, 1987Date of Patent: September 20, 1988Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Richard S. Iwasaki
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Patent number: 4772175Abstract: An erectable manipulator placement system for use on a space station and comprising an elongate lattice-like boom having dual guide tracks attached to parallel chords thereof, a carriage-like dolly movable along said tracks, and a segmented maneuvering arm-like assembly pivotally mounted on and extending from said dolly. The system further includes a turntable base pivotally interconnected with the proximal end of the boom and positioned either on a part of a transferring vehicle, or on another payload component being carried by said transferring vehicle, or on the space station.Type: GrantFiled: November 13, 1986Date of Patent: September 20, 1988Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Margaret E. Grimaldi
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Patent number: 4762173Abstract: A high effectiveness contour matching contact heat exchanger (10) includes two opposing plates (12,13), each having alternating double rows (25) of attached pins (20). The ends (23) of the pins (20) opposite their respective plates (12,13) are received in tight-fitting holes (40) in the opposite plate (12,13), providing for flexibility of the heat exchanger (10) to maintain efficient thermal transfer contact between the plates (12,13) and the external thermal sources (50,51) of heat or cold, without causing gaps between the ends (23) of the pins (20) and their respective opposite plates (12,13) that decrease heat transfer effectiveness by adversely affecting flow distribution of the fluid flowing therepast.Type: GrantFiled: December 19, 1986Date of Patent: August 9, 1988Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Robert L. Blakely, George J. Roebelen, Jr., Arthur K. Davenport
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Patent number: 4762619Abstract: A suitable member formed from sintered, powdered, stainless steel is contacted with a nitrate solution of a soluble alkali metal nitrate and a metal such as zirconium in a pH range and for a time sufficient to effect the formation of a membrane of zirconium oxide on the stainless steel support, the membrane preferably including an organic polymeric material such as polyacrylic acid.Type: GrantFiled: August 19, 1986Date of Patent: August 9, 1988Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Joseph L. Gaddis, Craig A. Brandon
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Patent number: 4757315Abstract: A signal is transmitted from a first location to a remote second location where a target carrying a transponder is positioned. The transponder re-radiates the signal to the first location where it is received. A phase comparator generates from the transmitted and received signals a measurement of their phase difference which is functionally related to the distance between the first and second locations. In one embodiment, the transponder is a passive parametric oscillator, being powered by energy received from the transmitted signal, which generates and transmits a subharmonic of the transmitted signal.Type: GrantFiled: February 20, 1986Date of Patent: July 12, 1988Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Christopher L. Lichtenberg, Paul W. Shores, Herbert S. Kobayashi
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Patent number: 4750543Abstract: A pumped loop two-phase heat transfer system, operating at a nearly constant temperature throughout, includes a plurality of independently operating grooved capillary heat exchanger plates supplied with working fluid through independent flow modulation valves connected to a liquid supply line, a vapor line for collecting vapor from the heat exchangers, a condenser between the vapor and the liquid lines, and a fluid circulating pump between the condenser and the heat exchangers.Type: GrantFiled: April 1, 1987Date of Patent: June 14, 1988Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Fred Edelstein
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Patent number: 4736927Abstract: The object of the invention is to provide a mechanical force actuator which is light weight and manipulatable and utilizes linear motion for push or pull forces while maintaining a constant overall length.The mechanical force producing mechanism comprises a linear actuator mechanism (22,23) and a linear motion shaft (11) mounted parallel to one another. The linear motion shaft (11) is connected to a stationary or fixed housing (12) and to a movable housing (26) where the movable housing (26) is mechanically actuated through actuator mechanism (22,26) by either manual means (21) or motor means (20). The housings (12,26) are adapted to releasably receive a variety of jaw or pulling elements (28) adapted for clamping or prying action. The stationary housing (12) is adapted to be pivotally mounted to permit an angular position of the housing to allow the tool to adapt to skewed interfaces. The actuator mechanisms (22,23) is operated by through a gear train (19) to obtain linear motion of the actuator mechanism.Type: GrantFiled: April 30, 1987Date of Patent: April 12, 1988Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: John P. Clancy
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Patent number: 4736490Abstract: A bracket hinge and bracket members (10, 10') with a spring biased and movable locking member (30). The locking or latch member (30) has ear parts (38, 39) received in locking openings (25, 25') where wedging surfaces (40, 41) on the ear parts cooperate with complimentary surfaces (42, 42') on the bracket members for bringing the bracket members into a tight end-to-end alignment when the bracket members are in an extended position. When the locking member (30) is moved to an unlocking position, pivoting of the hinge about a pivot pin (32) automatically places locking pins (70, 71) in a circular shaped groove (55) on the locking member (30) to retain the locking member (30) in an unlocked position. In pivoting the hinge from an extended position to a folded position, longitudinal spring members (80, 81) are placed under tension over annular rollers (60, 61) so that the spring tension in a folded position assists in return of the hinge from a folded position to an extended position.Type: GrantFiled: October 29, 1986Date of Patent: April 12, 1988Assignee: The United State of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Clarence J. Wesselski