Patents Represented by Attorney Thomas H. Jones
  • Patent number: 5075243
    Abstract: Amorphous Co:Si (1:2 ratio) films (12) are electron gun-evaporated on clean Si(111) substrates (10), such as in a molecular beam epitaxy system. These layers are then crystallized selectively with a focused electron beam (14) to form very small crystalline CoSi.sub.2 regions (12') in an amorphous matrix. Finally, the amorphous regions are etched away selectively using plasma or chemical techniques.
    Type: Grant
    Filed: March 27, 1991
    Date of Patent: December 24, 1991
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Kai-Wei Nieh, True-Lon Lin, Robert W. Fathauer
  • Patent number: 5072379
    Abstract: A method and associated apparatus for finding the lowest cost path of several variable paths comprising a plurality of linked cost-incurring areas existing between an origin point and a destination point. The method comprises the steps of, connecting a plurality of nodes together in the manner of the cost-incurring areas; programming each node to have a cost associated therewith corresponding to one of the cost-incurring areas; injecting a signal into one of the nodes representing the origin point; propagating the signal through the plurality of nodes from inputs to outputs thereof; reducing the signal in magnitude at each node as a function of the respective cost of the node; and, starting at one of the nodes representing the destination point and following a path having the least reduction in magnitude of the signal from node to node back to the one of the nodes representing the origin point whereby the lowest cost path from the origin point to the destination point is found.
    Type: Grant
    Filed: May 26, 1989
    Date of Patent: December 10, 1991
    Assignee: The United States of America as represented by the Adminstrator of the National Aeronautics and Space Administration
    Inventor: Silvio P. Eberhardt
  • Patent number: 5066337
    Abstract: A thermal power transfer system using a phase change liquid gas fluid in a closed loop configuration has a heat exchanger member connected to a gas conduit for inputting thermal energy into the fluid. The pressure in the gas conduit is higher than a liquid conduit that is connected to a heat exchanger member for outputting thermal energy. A solid electrolyte member acts as a barrier between the gas conduit and the liquid conduit adjacent a solid electrolyte member. The solid electrolyte member has the capacity of transmitting ions of a fluid through the electrolyte member. The ions can be recombined with electrons with the assistance of a porous electrode. An electrical field is applied across the solid electrolyte member to force the ions of the fluid from a lower pressure liquid conduit to the higher pressure gas conduit.
    Type: Grant
    Filed: August 16, 1990
    Date of Patent: November 19, 1991
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Pradeep Bhandari, Toshio Fujita
  • Patent number: 5066748
    Abstract: An electropolymerized film comprised of polymers and copolymers of a monomer having the general formula: ##STR1## is formed on the surface of an anode. The finished structures have superior electrical and mechanical properties for use in applications such as electrostatic dissipation and for the reduction of the radar cross section of advanced aircraft.
    Type: Grant
    Filed: February 7, 1990
    Date of Patent: November 19, 1991
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Ganesan Nagasubramanian, Salvador DiStefano, Ranty H. Liang
  • Patent number: 5063747
    Abstract: The present invention relates to a cryogenic Joule-Thomson refrigeration capable of pumping multicomponent gases with a single stage sorption compressor system. Alternative methods of pumping a multicomponent gas with a single stage compressor are disclosed. In a first embodiment, the sorbent geometry is such that a void is defined near the output of the sorption compressor. When the sorbent is cooled, the sorbent primarily adsorbs the higher boiling point gas such that the lower boiling point gas passes through the sorbent to occupy the void. When the sorbent is heated, the higher boiling point gas is desorbed at high temperature and pressure and thereafter propels the lower boiling point gas out of the sorption compressor. A mixing chamber is provided to remix the constituent gases prior to expansion of the gas through a Joule-Thomson valve. Other methods of pumping multicomponent gas are disclosed.
    Type: Grant
    Filed: June 28, 1990
    Date of Patent: November 12, 1991
    Assignee: United States of America as represented by the United States National Aeronautics and Space Administration
    Inventors: Jack A. Jones, S. Walter Petrick, Steven Bard
  • Patent number: 5065236
    Abstract: Methods for providing stereoscopic image presentation and stereoscopic configurations using stereoscopic viewing systems having converged or parallel cameras may be set up to reduce or eliminate erroneously perceived accelerations and decelerations by proper selection of parameters, such as an image magnification factor q and intercamera distance 2w. For converged cameras, q is selected to be equal to Ve-qwl=0, where V is the camera convergence distance, e is half the interocular distance of an observer, w is half the intercamera distance and l is the actual distance from said first nodal point of each camera to said convergence point, and for parallel cameras, q is selected to be equal to e/w.
    Type: Grant
    Filed: November 2, 1990
    Date of Patent: November 12, 1991
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Daniel B. Diner
  • Patent number: 5062693
    Abstract: A single material (not a multi-element structure) spatial light modulator (50) may be written to (30), as well as read out from (80), using light (20). The device has tailorable rise and hold times dependent on the composition and concentration of the molecular species used as the active components. The spatial resolution of this device is limited only by light diffraction as in volume holograms. The device may function as a two-dimensional mask (transmission or reflection) or as a three-dimensional volume holographic medium. This device, based on optically-induced electron transfer, is able to perform incoherent to coherent image conversion or wavelength conversion over a wide spectral range (ultraviolet, visible, or near-infrared regions).
    Type: Grant
    Filed: February 15, 1990
    Date of Patent: November 5, 1991
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Administration
    Inventors: David N. Beratan, Joseph W. Perry
  • Patent number: 5059581
    Abstract: The surface of high temperature superconductors such as YBa.sub.2 Cu.sub.3 O.sub.7-x are passivated by reacting the native Y, Ba and Cu metal ions with an anion such as sulfate or oxalate to form a surface film that is impervious to water and has a solubility in water of no more than 10.sup.-3 M. The passivating treatment is preferably conducted by immersing the surface in dilute aqueous acid solution since more soluble species dissolve into the solution. The treatment does not degrade the superconducting properties of the bulk material.
    Type: Grant
    Filed: June 28, 1990
    Date of Patent: October 22, 1991
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Richard P. Vasquez
  • Patent number: 5057843
    Abstract: A polarization filter can maximize the signal-to-noise ratio of a polarimetric SAR and help discriminate between targets or enhance image features, e.g., enhance contract between different types of target. The method disclosed is based on the Stokes matrix/Stokes vector representation, so the targets of interest can be extended targets, and the method can also be applied to the case of bistatic polarimetric radars.
    Type: Grant
    Filed: June 25, 1990
    Date of Patent: October 15, 1991
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Pascale C. Dubois, Jakob J. vanZyl
  • Patent number: 5057473
    Abstract: Efficient, regenerable sorbents for removal of H.sub.2 S from fluid hydrocarbons such as diesel fuel at moderate condition comprise a porous, high surface area aluminosilicate support, suitably a synthetic zeolite, and most preferably a zeolite having a free lattice opening of at least 6 Angstroms containing from 0.1 to 0.5 moles of copper ions, lanthanum ions or their mixtures. The sorbent removes sulfur from the hydrocarbon fuel in high efficiency and can be repetitively regenerated without loss of activity.
    Type: Grant
    Filed: April 12, 1990
    Date of Patent: October 15, 1991
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Gerald E. Voecks, Pramod K. Sharma
  • Patent number: 5055240
    Abstract: A method is described for forming hollow particles, or shells, of extremely small size. The shell material is heated to a molten temperature in the presence of a gas that is at least moderately soluble in the shell material, to form a solution of the molten shell material and the soluble gas. The solution is atomized to form a multiplicity of separate droplets that are cooled while in free fall. Cooling of a droplet from the outside traps the dissolved gas and forces it to form a gas bubble at the center of the droplet which now forms a gas-filled shell. The shell is reheated and then cooled in free fall, in an environment having a lower pressure than the gas pressure in the shell. This causes expansion of the shell, to form a shell having a small wall thickness compared to its diameter.
    Type: Grant
    Filed: April 30, 1986
    Date of Patent: October 8, 1991
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Mark C. Lee, Christopher H. Schilling, Taylor G. Wang
  • Patent number: 5056037
    Abstract: This is a recurrent or feedforward analog neural network processor having a multi-level neuron array and a synaptic matrix for storing weighted analog values of synaptic connection strengths which is characterized by temporarily changing one connection strength at a time to determine its effect on system output relative to the desired target. That connection strength is then adjusted based on the effect, whereby the processor is taught the correct response to training examples connection by connection.
    Type: Grant
    Filed: December 28, 1989
    Date of Patent: October 8, 1991
    Assignee: The United States of America as represented by the administrator of the National Aeronautics and Space Administration
    Inventor: Silvio P. Eberhardt
  • Patent number: 5049796
    Abstract: Model-based and performance-based control techniques are combined for an electrical robotic control system. Thus, two distinct and separate design philosophies have been merged into a single control system having a control law formulation including two distinct and separate components, each of which yields a respective signal component that is combined into a total command signal for the system. Those two separate system components include a feedforward controller and a feedback controller. The feedforward controller is model-based and contains any known part of the manipulator dynamics that can be used for on-line control to produce a nominal feedforward component of the system's control signal. The feedback controller is performance-based and consists of a simple adaptive PID controller which generates an adaptive control signal to complement the nominal feedforward signal.
    Type: Grant
    Filed: May 17, 1989
    Date of Patent: September 17, 1991
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Homayoun Seraji
  • Patent number: 5048023
    Abstract: A memory system is provided, of the type which includes an error-correcting circuit that detects and corrects errors, which more efficiently utilizes the capacity of a memory formed of groups of binary cells whose states can be inadvertently switched by ionizing radiation. Each memory cell has an asymmetric geometry, so that ionizing radiation causes a significantly greater probability of errors in one state than in the opposite state (e.g., an erroneous switch from "1" to "0" is far more likely than a switch from "0" to "1"). An asymmetric error-correcting coding circuit can be used with the asymmetric memory cells, which requires fewer bits than an efficient symmetric error-correcting code.
    Type: Grant
    Filed: February 16, 1989
    Date of Patent: September 10, 1991
    Assignee: The United States of America as represented by the Administrator, National Aeronautics and Space Administration
    Inventors: Martin G. Buehler, Marvin Perlman
  • Patent number: 5047700
    Abstract: A control system for a multi-motor system such as a space telerobot having a remote computational node and a local computational node inter-connected with one another by a high speed data link is described. A Universal Computer Control System (UCCS) for the telerobot motors is located at each node. Each node is provided with a multibus computer system which is characterized by a plurality of processors with all processors being connected to a common bus leading to a command processor. The command processor controls joint hardware and/or software for a plurality of direct current torque motors of the type used in telerobot joints and telerobot hand-held controllers. The motors are connected to the joint processor cards and respond to digital control signals from the joint command processor and a joint motor control card.
    Type: Grant
    Filed: March 23, 1988
    Date of Patent: September 10, 1991
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Zoltan F. Szakaly
  • Patent number: 5038089
    Abstract: A master six-degree-freedom Force Reflecting Hand Controller ("FRHC") is available at a master site where a received image displays, in essentially real-time, a remote robotic manipulator which is being controlled in the corresponding six-degree-freedom by command signals which are transmitted to the remote site in accordance with the movement of the FRHC at the master site. Software is user-initiated at the master site in order to establish the basic system conditions and then a physical movement of the FRHC in Cartesean space is reflected at the master site by six absolute numbers that are sensed, translated, and computed as a difference signal relative to the earlier position. The change in position is then transmitted in that differential signal form over a high speed synchronized bilateral communication channel which simultaneously returns robot-sensed response information to the master site as forces applied to the FRHC so that the FRHC reflects the "feel" of what is taking place at the remote site.
    Type: Grant
    Filed: October 28, 1988
    Date of Patent: August 6, 1991
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Zoltan F. Szakaly
  • Patent number: 5031689
    Abstract: A flexible heat transfer apparatus used to flexibly connect and thermally couple a thermoelectric cooler to an object to be cooled. The flexible heat transfer apparatus consists of a pair of flexible corrugated sheets made from high thermal conductivity materials such as copper, aluminum, gold, or silver. The ridges of the corrugated sheets are oriented perpendicular to one another and bonded sandwich-fashion between three plates to define an upper section and a lower section. The upper section provides X flexure, the lower section provides Y flexure, and both sections together provide Z flexure.
    Type: Grant
    Filed: July 31, 1990
    Date of Patent: July 16, 1991
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Jack A. Jones, S. Walter Petrick, Steven Bard
  • Patent number: 5031089
    Abstract: In a distributed heterogeneous computer system having a plurality of computer nodes each operatively connected through a network interface to a network to provide for communications and transfers of data between the nodes and wherein the nodes each have a queue for containing jobs to be performed, an improvement for dynamically reallocating the system's resources for optimized job performance. There is first logic at each node for dynamically and periodically calculating and saving a workload value as a function of the number of jobs on the node's queue. Second logic is provided at each node for transfering the node's workload value to other nodes on the network at the request of the other nodes. Finally, there is third logic at each node operable at the completion of each job.
    Type: Grant
    Filed: December 30, 1988
    Date of Patent: July 9, 1991
    Assignee: United States of America as represented by the Administrator, National Aeronautics and Space Administration
    Inventors: Howard T. Liu, John A. Silvester
  • Patent number: 5031234
    Abstract: A reference frequency distribution system for transmitting a reference frequency from a reference unit to a remote unit while keeping the reference frequency at the reference unit and remote unit in phase. A fiber optic cable connects the reference unit to the remote unit. A frequency source at the reference unit produces a reference frequency having an adjustable phase. A fiber optic transmitter at the reference unit modulates a light beam with the reference frequency and transmits the light beam into the fiber optic cable. A 50/50 reflector at the remote unit reflects a first portion of the light beam from the reference unit back into the fiber optic cable to the reference unit. A first fiber optic receiver disposed at the remote unit receives a second portion of the light beam and demodulates the reference frequency therefrom to be used at the remote unit.
    Type: Grant
    Filed: May 31, 1989
    Date of Patent: July 9, 1991
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Lori E. Primas, Richard L. Sydnor, George F. Lutes
  • Patent number: 5026008
    Abstract: An improved fluid actuating system for imparting motion to a body such as a spacecraft is disclosed. The fluid actuating system consists of a fluid mass that may be controllably accelerated through at least one fluid path whereby an opposite acceleration is experienced by the spacecraft. For full control of the spacecraft's orientation, the system would include a plurality of fluid paths. The fluid paths may be circular or irregular, and the fluid paths may located on the interior or exterior of the spacecraft.
    Type: Grant
    Filed: January 31, 1990
    Date of Patent: June 25, 1991
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Boris J. Lurie, J. Alan Schier, Theodore C. Iskenderian