Patents Assigned to THE U.S.A. AS REPRESENTED BY THE ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION
  • Publication number: 20140273695
    Abstract: Consolidated carbon nanotube or graphene yarns and woven sheets are consolidated through the formation of a carbon binder formed from the dehydration of sucrose. The resulting materials on a macro-scale are lightweight and of a high specific modulus and/or strength. Sucrose is relatively inexpensive and readily available, and the process is therefore cost-effective.
    Type: Application
    Filed: March 12, 2014
    Publication date: September 18, 2014
    Applicant: U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Godfrey Sauti, Jae-Woo Kim, Emilie J. Siochi, Kristopher E. Wise
  • Publication number: 20140264325
    Abstract: One aspect of the present invention is a double sided hybrid crystal structure including a trigonal Sapphire wafer containing a (0001) C-plane and having front and rear sides. The Sapphire wafer is substantially transparent to light in the visible and infrared spectra, and also provides insulation with respect to electromagnetic radio frequency noise. A layer of crystalline Si material having a cubic diamond structure aligned with the cubic <111> direction on the (0001) C-plane and strained as rhombohedron to thereby enable continuous integration of a selected (SiGe) device onto the rear side of the Sapphire wafer. The double sided hybrid crystal structure further includes an integrated III-Nitride crystalline layer on the front side of the Sapphire wafer that enables continuous integration of a selected III-Nitride device on the front side of the Sapphire wafer.
    Type: Application
    Filed: March 11, 2014
    Publication date: September 18, 2014
    Applicant: U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Yeonjoon Park, Sang Hyouk Choi
  • Publication number: 20140277743
    Abstract: A system for developing distributed robot application-level software includes a robot having an associated control module which controls motion of the robot in response to a commanded task, and a robot task commander (RTC) in networked communication with the control module over a network transport layer (NTL). The RTC includes a script engine(s) and a GUI, with a processor and a centralized library of library blocks constructed from an interpretive computer programming code and having input and output connections. The GUI provides access to a Visual Programming Language (VPL) environment and a text editor. In executing a method, the VPL is opened, a task for the robot is built from the code library blocks, and data is assigned to input and output connections identifying input and output data for each block. A task sequence(s) is sent to the control module(s) over the NTL to command execution of the task.
    Type: Application
    Filed: March 14, 2013
    Publication date: September 18, 2014
    Applicants: The U.S.A. As Represented by the Administrator of the National Aeronautics and Space Administration, GM GLOBAL TECHNOLOGY OPERATIONS LLC
    Inventors: Stephen W. Hart, John D. Yamokoski, Brian J. Wightman, Duy Paul Dinh, Dustin R. Gooding
  • Publication number: 20140263246
    Abstract: Gas is introduced into molten metal during an additive metal fabrication process and/or during a metal fusion process. The gas may comprise a process gas that flows through a tubular feed wire. The amount of process gas introduced can be controlled to vary the composition and/or material properties of metal deposits formed from a molten metal. Material properties such as yield strength, hardness, and fracture toughness can be increased or decreased in specific regions to provide material property gradients that closely correspond to expected requirements of components fabricated utilizing additive and/or fusion processes.
    Type: Application
    Filed: March 12, 2014
    Publication date: September 18, 2014
    Applicant: U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Craig A. Brice
  • Publication number: 20140262015
    Abstract: A soft lithography template or stamp is made by casting a polydimethysiloxane (PDMS) or other suitable elastomeric precursor onto a master pattern. The master pattern may be formed utilizing known micro-fabrication techniques. The PDMS template includes an inverse copy of the micro-structures on the master pattern, and can be placed into a mold used to prepare a carbon-fiber reinforced polymer composite part or other polymer molding systems where a matrix material passes through a fluid state during the cure process. The liquid resin material flows into the structures on the surface of the PDMS template and hardens during the curing cycle. After the part is released from the mold, the PDMS template can be peeled from the surface of the part to reveal the free standing micro structures which are a replica of the master pattern.
    Type: Application
    Filed: March 12, 2014
    Publication date: September 18, 2014
    Applicant: U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Frank L. Palmieri, Vincent B. Cruz, Christopher J. Wohl, JR.
  • Publication number: 20140262498
    Abstract: An interconnect device forms an electrical and mechanical connection between electrical connections pads on an integrated circuit and those on a printed circuit board. The device is a coil with a first portion of its turns at one axial end of the coil having at least two turns in axial contact with one another, a second portion of its turns at an opposing axial end of the coil having at least two turns in axial contact with one another, and a third portion of the turns disposed between and contiguous with the first and second portions. The third portion is defined by at least two of the turns in a spaced apart axial relationship. The coil is made from a spring material and is electrically conductive. Each of the coil's first portion and second portion is coated with a solder material.
    Type: Application
    Filed: March 13, 2013
    Publication date: September 18, 2014
    Applicant: U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
  • Publication number: 20140222199
    Abstract: A grasp assist device includes a glove with first and second tendon-driven fingers, a tendon, and a sleeve with a shared tendon actuator assembly. Tendon ends are connected to the respective first and second fingers. The actuator assembly includes a drive assembly having a drive axis and a tendon hook. The tendon hook, which defines an arcuate surface slot, is linearly translatable along the drive axis via the drive assembly, e.g., a servo motor thereof. The flexible tendon is routed through the surface slot such that the surface slot divides the flexible tendon into two portions each terminating in a respective one of the first and second ends. The drive assembly may include a ball screw and nut. An end cap of the actuator assembly may define two channels through which the respective tendon portions pass. The servo motor may be positioned off-axis with respect to the drive axis.
    Type: Application
    Filed: February 7, 2014
    Publication date: August 7, 2014
    Applicants: The U.S.A. As Represented by the Administrator of the National Aeronautics and Space Administration, GM GLOBAL TECHNOLOGY OPERATIONS LLC
    Inventors: Chris A. Ihrke, Bryan J. Bergelin, Lyndon Bridgwater
  • Publication number: 20140217762
    Abstract: A robotic system includes a tendon-driven end effector, a linear actuator, a flexible tendon, and a plate assembly. The linear actuator assembly has a servo motor and a drive mechanism, the latter of which translates linearly with respect to a drive axis of the servo motor in response to output torque from the servo motor. The tendon connects to the end effector and drive mechanism. The plate assembly is disposed between the linear actuator assembly and the tendon-driven end effector and includes first and second plates. The first plate has a first side that defines a boss with a center opening. The second plate defines an arcuate through-slot having tendon guide channels. The first plate defines a through passage for the tendon between the center opening and a second side of the first plate. A looped end of the flexible tendon is received within the tendon guide channels.
    Type: Application
    Filed: February 7, 2014
    Publication date: August 7, 2014
    Applicants: The U.S.A. As Represented by the Administrator of the National Aeronautics and Space Administration, GM GLOBAL TECHNOLOGY OPERATIONS LLC
    Inventors: Chris A. Ihrke, Myron A. Diftler, Lyndon Bridgwater, Vienny Nguyen, Alexander Millerman
  • Publication number: 20140173887
    Abstract: A process and apparatus for collecting data for nondestructive evaluation of the quality of a crimped wire connector are provided. The process involves providing a crimping tool having an anvil and opposing jaw for crimping a terminal onto a stranded wire, moving the jaw relative to the anvil to close the distance between the jaw and the anvil and thereby compress the terminal against the wire, while transmitting ultrasonic waves that are propagated through the terminal wire combination and received at a receiving ultrasonic transducer as the jaw is moved relative to the anvil, and detecting and recording the position of the jaw relative to the anvil as a function of time and detecting and recording the amplitude of the ultrasonic wave that is received at the receiving ultrasonic transducer as a function of time as the jaw is moved relative to the anvil.
    Type: Application
    Filed: February 28, 2014
    Publication date: June 26, 2014
    Applicants: Tyco Electronics Corporation, U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: William T. Yost, Karl E. Cramer, Daniel F. Perey, Keith A. Williams
  • Publication number: 20140180524
    Abstract: An amorphous robot includes a compartmented bladder containing fluid, a valve assembly, and an outer layer encapsulating the bladder and valve assembly. The valve assembly draws fluid from a compartment(s) and discharges the drawn fluid into a designated compartment to displace the designated compartment with respect to the surface. Another embodiment includes elements each having a variable property, an outer layer that encapsulates the elements, and a control unit. The control unit energizes a designated element to change its variable property, thereby moving the designated element. The elements may be electromagnetic spheres with a variable polarity or shape memory polymers with changing shape and/or size. Yet another embodiment includes an elongated flexible tube filled with ferrofluid, a moveable electromagnet, an actuator, and a control unit. The control unit energizes the electromagnet and moves the electromagnet via the actuator to magnetize the ferrofluid and lengthen the flexible tube.
    Type: Application
    Filed: February 25, 2014
    Publication date: June 26, 2014
    Applicant: U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Arthur T. Bradley
  • Publication number: 20140156039
    Abstract: The invention is an apparatus and method of biofeedback training for attaining a physiological state optimally consistent with the successful performance of a task, wherein the probability of successfully completing the task is made is inversely proportional to a physiological difference value, computed as the absolute value of the difference between at least one physiological signal optimally consistent with the successful performance of the task and at least one corresponding measured physiological signal of a trainee performing the task. The probability of successfully completing the task is made inversely proportional to the physiological difference value by making one or more measurable physical attributes of the environment in which the task is performed, and upon which completion of the task depends, vary in inverse proportion to the physiological difference value.
    Type: Application
    Filed: January 13, 2014
    Publication date: June 5, 2014
    Applicant: U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Lawrence J. Prinzel, III, Alan T. Pope, Olafur S. Palsson, Marsha J. Turner
  • Publication number: 20140134352
    Abstract: A method for joining or repairing boron nitride nanotubes (BNNTs). In joining BNNTs, the nanotube structure is modified with amorphous carbon deposited by controlled electron beam irradiation to form well bonded hybrid a-C/BNNT structures. In repairing BNNTs, the damaged site of the nanotube structure is modified with amorphous carbon deposited by controlled electron beam irradiation to form well bonded hybrid a-C/BNNT structures at the damage site.
    Type: Application
    Filed: November 15, 2012
    Publication date: May 15, 2014
    Applicants: U.S. as represented by the Administrator of the National Aeronautics and Space Administration, National Institute of Aerospace Associates
    Inventors: Jae Woo Kim, Emilie J. Siochi, Kristopher E. Wise, Yi Lin, John Connell
  • Publication number: 20140053654
    Abstract: Shape of a multi-core optical fiber is determined by positioning the fiber in an arbitrary initial shape and measuring strain over the fiber's length using strain sensors. A three-coordinate p-vector is defined for each core as a function of the distance of the corresponding cores from a center point of the fiber and a bending angle of the cores. The method includes calculating, via a controller, an applied strain value of the fiber using the p-vector and the measured strain for each core, and calculating strain due to bending as a function of the measured and the applied strain values. Additionally, an apparent local curvature vector is defined for each core as a function of the calculated strain due to bending. Curvature and bend direction are calculated using the apparent local curvature vector, and fiber shape is determined via the controller using the calculated curvature and bend direction.
    Type: Application
    Filed: August 22, 2012
    Publication date: February 27, 2014
    Applicant: U.S.A as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Matthew D. Rogge, Jason P. Moore
  • Publication number: 20140036252
    Abstract: A Doppler lidar sensor system includes a laser generator that produces a highly pure single frequency laser beam, and a frequency modulator that modulates the laser beam with a highly linear frequency waveform. A first portion of the frequency modulated laser beam is amplified, and parts thereof are transmitted through at least three separate transmit/receive lenses. A second portion of the laser beam is used as a local oscillator beam for optical heterodyne detection. Radiation from the parts of the laser beam transmitted via the transmit/receive lenses is received by the respective transmit/receive lenses that transmitted the respective part of the laser beam. The received reflected radiation is compared with the local oscillator beam to calculate the frequency difference therebetween to determine various navigational data.
    Type: Application
    Filed: August 3, 2012
    Publication date: February 6, 2014
    Applicant: U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Farzin Amzajerdian, Diego F. Pierrottet
  • Publication number: 20140028132
    Abstract: Flywheel systems are disclosed that provide increased energy density and operational effectiveness. A first bearingless motor and a second bearingless motor may be configured to simultaneously suspend the central rotor in a radial direction and to rotate the central rotor. However, certain implementations may have one motor or more than two motors, depending on the design. A plurality of the flywheel systems may be collectively controlled to perform community energy storage with higher storage capacities than individual flywheel systems.
    Type: Application
    Filed: December 21, 2012
    Publication date: January 30, 2014
    Applicant: U.S.A., as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Ralph H. Jansen, Larry M. Trase, Timothy P. Dever, Peter E. Kascak, Kraft G. Thomas
  • Publication number: 20140011145
    Abstract: A flame holder system includes a modified torch body and a ceramic flame holder. Catch pin(s) are coupled to and extend radially out from the torch body. The ceramic flame holder has groove(s) formed in its inner wall that correspond in number and positioning to the catch pin(s). Each groove starts at one end of the flame holder and is can be shaped to define at least two 90° elbows. Each groove is sized to receive one catch pin therein when the flame holder is fitted over the end of the torch body. The flame holder is then manipulated until the catch pin(s) butt up against the end of the groove(s).
    Type: Application
    Filed: September 9, 2013
    Publication date: January 9, 2014
    Applicant: U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Henry H. Haskin, Peter Vasquez
  • Publication number: 20130289945
    Abstract: Embodiments of the invention may provide the ability for infrastructure managers to readily assess current organizational space allocation, to determine overcrowded and/or underutilized facilities, to propose options for improving and/or optimizing space usage in a facility, and to visualize current and proposed utilization. Embodiments of the invention may also provide the ability to reduce operational costs by more efficiently utilizing available space. Embodiments of the invention may comprise optimization algorithms to help redistribute organizational slots based on a variety of user-defined criteria (e.g., lab/technical space constraints, organizational synergy constraints, move minimizations, etc.).
    Type: Application
    Filed: April 27, 2012
    Publication date: October 31, 2013
    Applicant: U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: William B. Ball, Robert L. Gage, Raymond L. Gates
  • Publication number: 20130273371
    Abstract: A process for producing highly monodisperse polystyrene particles includes steps of mixing water and styrene in a reactor, optionally adding an electrolyte to the mixture, purging the mixture of oxygen, adding a polymerization initiator while agitating and heating the mixture, and maintaining agitation and heating for a time sufficient to achieve a desired yield of monodisperse polystyrene particles having a particle size from 0.25 microns to 2.5 microns and a statistical quality factor greater than 10.
    Type: Application
    Filed: April 11, 2012
    Publication date: October 17, 2013
    Applicant: U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Pacita I. Tiemsin, Donald M. Oglesby, Jacqueline L. Schryer
  • Publication number: 20130219586
    Abstract: A grasp assist system includes a glove and a flexible sleeve. The glove includes a digit such as a finger or thumb, a force sensor configured to measure a grasping force applied to an object by an operator wearing the glove, and adjustable phalange rings positioned with respect to the digit. A saddle is positioned with respect to the finger. A flexible tendon is looped at one end around the saddle. A conduit contains the tendon. A conduit anchor secured within a palm of the glove receives the conduit. The sleeve has pockets containing an actuator assembly connected to another end of the tendon and a controller. The controller is in communication with the force sensor, and calculates a tensile force in response to the measured grasping force. The controller commands the tensile force from the actuator assembly to tension the tendon and thereby move the finger.
    Type: Application
    Filed: February 29, 2012
    Publication date: August 29, 2013
    Applicants: The U.S.A. As Represented by the Administrator of the National Aeronautics and Space Administration, GM GLOBAL TECHNOLOGY OPERATIONS LLC
    Inventors: Chris A. Ihrke, Donald R. Davis, Douglas Martin Linn, Bryan J. Bergelin, Lyndon B.J. Bridgwater, Heather Bibby, Judy Schroeder, Craig Erkkila
  • Publication number: 20130219585
    Abstract: A grasp assist system includes a glove, actuator assembly, and controller. The glove includes a digit, i.e., a finger or thumb, and a force sensor. The sensor measures a grasping force applied to an object by an operator wearing the glove. Phalange rings are positioned with respect to the digit. A flexible tendon is connected at one end to one of the rings and is routed through the remaining rings. An exoskeleton positioned with respect to the digit includes hinged interconnecting members each connected to a corresponding ring, and/or a single piece of slotted material. The actuator assembly is connected to another end of the tendon. The controller calculates a tensile force in response to the measured grasping force, and commands the tensile force from the actuator assembly to thereby pull on the tendon. The exoskeleton offloads some of the tensile force from the operator's finger to the glove.
    Type: Application
    Filed: February 29, 2012
    Publication date: August 29, 2013
    Applicants: The U.S.A. as Represented by the Administrator of the National Aeronautics and Space Administration, GM GLOBAL TECHNOLOGY OPERATIONS LLC
    Inventors: Bryan J. Bergelin, Chris A. Ihrke, Donald R. Davis, Douglas Martin Linn, Lyndon B.J. Bridgwater