Patents Assigned to and Space Administration
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Patent number: 8841698Abstract: A method is disclosed that provides a self-aligned nitrogen-implant particularly suited for a Junction Field Effect Transistor (JFET) semiconductor device preferably comprised of a silicon carbide (SiC). This self-aligned nitrogen-implant allows for the realization of durable and stable electrical functionality of high temperature transistors such as JFETs. The method implements the self-aligned nitrogen-implant having predetermined dimensions, at a particular step in the fabrication process, so that the SiC junction field effect transistors are capable of being electrically operating continuously at 500° C. for over 10,000 hours in an air ambient with less than a 10% change in operational transistor parameters.Type: GrantFiled: April 1, 2011Date of Patent: September 23, 2014Assignee: The United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventor: Philip G. Neudeck
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Publication number: 20140277743Abstract: 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: ApplicationFiled: March 14, 2013Publication date: September 18, 2014Applicants: The U.S.A. As Represented by the Administrator of the National Aeronautics and Space Administration, GM GLOBAL TECHNOLOGY OPERATIONS LLCInventors: Stephen W. Hart, John D. Yamokoski, Brian J. Wightman, Duy Paul Dinh, Dustin R. Gooding
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Publication number: 20140273695Abstract: 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: ApplicationFiled: March 12, 2014Publication date: September 18, 2014Applicant: U.S.A. as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Godfrey Sauti, Jae-Woo Kim, Emilie J. Siochi, Kristopher E. Wise
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Publication number: 20140264325Abstract: 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: ApplicationFiled: March 11, 2014Publication date: September 18, 2014Applicant: U.S.A. as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Yeonjoon Park, Sang Hyouk Choi
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Publication number: 20140262015Abstract: 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: ApplicationFiled: March 12, 2014Publication date: September 18, 2014Applicant: U.S.A. as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Frank L. Palmieri, Vincent B. Cruz, Christopher J. Wohl, JR.
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Publication number: 20140265057Abstract: Methods for making a neutron converter layer are provided. The various embodiment methods enable the formation of a single layer neutron converter material. The single layer neutron converter material formed according to the various embodiments may have a high neutron absorption cross section, tailored resistivity providing a good electric field penetration with submicron particles, and a high secondary electron emission coefficient. In an embodiment method a neutron converter layer may be formed by sequential supercritical fluid metallization of a porous nanostructure aerogel or polyimide film. In another embodiment method a neutron converter layer may be formed by simultaneous supercritical fluid metallization of a porous nanostructure aerogel or polyimide film. In a further embodiment method a neutron converter layer may be formed by in-situ metalized aerogel nanostructure development.Type: ApplicationFiled: March 10, 2014Publication date: September 18, 2014Applicant: U.S.A. as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Cheol Park, Godfrey Sauti, Jin Ho Kang, Sharon E. Lowther, Sheila A. Thibeault, Robert G. Bryant
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Publication number: 20140264459Abstract: An electronic device includes a trigonal crystal substrate defining a (0001) C-plane. The substrate may comprise Sapphire or other suitable material. A plurality of rhomhohedrally aligned SiGe (111)-oriented crystals are disposed on the (0001) C-plane of the crystal substrate. A first region of material is disposed on the rhombohedrally aligned SiGe layer. The first region comprises an intrinsic or doped Si, Ge, or SiGe layer. The first region can be layered between two secondary regions comprising n+doped SiGe or n+doped Ge, whereby the first region collects electrons from the two secondary regions.Type: ApplicationFiled: March 10, 2014Publication date: September 18, 2014Applicant: U.S.A. as represented by the National Aeronautics and Space AdministrationInventors: Sang Hyouk Choi, Yeonjoon Park, Glen C. King, Hyun-Jung Kim, Kunik Lee
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Publication number: 20140262498Abstract: 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: ApplicationFiled: March 13, 2013Publication date: September 18, 2014Applicant: U.S.A. as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
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Publication number: 20140263246Abstract: 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: ApplicationFiled: March 12, 2014Publication date: September 18, 2014Applicant: U.S.A. as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Craig A. Brice
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Patent number: 8834597Abstract: A method of fabricating metallic Cu nanowires with lengths up to about 25 ?m and diameters in a range 20-100 nm, or greater if desired. Vertically oriented or laterally oriented copper oxide structures (CuO and/or Cu2O) are grown on a Cu substrate. The copper oxide structures are reduced with 99+ percent H or H2, and in this reduction process the lengths decrease (to no more than about 25 ?m), the density of surviving nanostructures on a substrate decreases, and the diameters of the surviving nanostructures have a range, of about 20-100 nm. The resulting nanowires are substantially pure Cu and can be oriented laterally (for local or global interconnects) or can be oriented vertically (for standard vertical interconnects).Type: GrantFiled: May 31, 2012Date of Patent: September 16, 2014Assignee: The United Stated of America as Represented by the Administrator of the National Aeronautics & Space Administration (NASA)Inventors: Jin-Woo Han, Meyya Meyyappan
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Patent number: 8827717Abstract: New types of controllers allow players to make inputs to a video game or simulation by moving the entire controller itself. This capability is typically accomplished using a wireless input device having accelerometers, gyroscopes, and an infrared LED tracking camera. The present invention exploits these wireless motion-sensing technologies to modulate the player's movement inputs to the videogame based upon physiological signals. Such biofeedback-modulated video games train valuable mental skills beyond eye-hand coordination. These psychophysiological training technologies enhance personal improvement, not just the diversion, of the user.Type: GrantFiled: June 22, 2011Date of Patent: September 9, 2014Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Alan T. Pope, Chad L. Stephens, Nina Marie Blanson
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Patent number: 8816884Abstract: A rebinning device includes a rebinning engine that transforms signal data from a first format to a second format with vectorized binning. Moreover, a data storage operably coupled to the rebinning engine stores the signal data in the second format. The rebinning device may optionally includes a capturing engine that captures the signal data in the first format and a rendering engine that renders the signal data in the second format.Type: GrantFiled: August 31, 2012Date of Patent: August 26, 2014Assignee: USA as represented by the Administrator of the National Aeronautics Space AdministrationInventors: Bruce H. Dean, Jeffrey S. Smith, David L. Aronstein
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Patent number: 8816273Abstract: Time-to-digital converters adapted to analog and digital inputs and methods of use are described. A time-to-digital converter has an event frame latches and logic module with memory cells, an analog front-end module connected to the memory cells, and a bin increment generator module connected to the memory cells. The bin increment generator is configured to issue bin increments separated by a time increment, and the analog front end is configured to issue a start event followed by a plurality of stop events. Upon receipt of a first time increment following a start event, the event frame latches and logic module updates a first memory cell with a first bit-type; upon receipt of a second time increment following an intervening stop event, the event frame latches and logic module updates a second memory cell with a second bit-type different from the first bit-type.Type: GrantFiled: August 27, 2012Date of Patent: August 26, 2014Assignee: The United States of America as represented by the Administrator of the National Aeronautics Space AdministrationInventors: George Suarez, Jeffrey J. Dumonthier
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Patent number: 8813577Abstract: A device used in making differential measurements of a flow includes a flow obstruction and a support arm. The flow obstruction's forward portion is a nose cone. The flow obstruction's aft portion is coupled to the nose cone. The support arm's first end is coupled to an exterior wall of a conduit, and its second end is coupled to the forward portion of the flow obstruction. The support arm positions the flow obstruction in the conduit such that a flow region is defined around its nose cone, and such that the support arm's first and second end are separated from one another with respect to a length dimension of the conduit. Measurement ports are provided in the support arm and flow obstruction. Manifolds extending through the flow obstruction and support arm couple the ports to points at the exterior wall of the conduit.Type: GrantFiled: November 22, 2011Date of Patent: August 26, 2014Assignee: The United States of America as Represented by the Administrator of the National Aeronautics and Space AdministrationInventors: John Dwight England, Anthony R. Kelley, Raymond J. Cronise
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Patent number: 8815603Abstract: A chemochromic indicator is provided that includes a hypergolic fuel sensing chemochromic pigment that change from a first color to a second color in the presence of a hypergolic fuel. In a first embodiment, a chemochromic indicator is provided for detecting the presence of a hypergolic fuel such that the irreversible hypergolic fuel sensing chemochromic pigment includes potassium tetrachloroaurate (KAuCl4). There are several types of chemochromic indicators, for example, the article used to form the chemochromic indicators include, but are not limited to, wipe materials, silicone/TEFLON tape, manufactured parts, fabrics, extruded parts, and paints.Type: GrantFiled: July 11, 2012Date of Patent: August 26, 2014Assignee: The United States of America as Represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Luke B. Roberson, Robert W. DeVor, Janine E. Captain, Edgardo Santiago-Maldonado
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Patent number: 8810255Abstract: An in-situ system for detecting damage in an electrically conductive wire. The system includes a substrate at least partially covered by a layer of electrically conductive material forming a continuous or non-continuous electrically conductive layer connected to an electrical signal generator adapted to delivering electrical signals to the electrically conductive layer. Data is received and processed to identify damage to the substrate or electrically conductive layer. The electrically conductive material may include metalized carbon fibers, a thin metal coating, a conductive polymer, carbon nanotubes, metal nanoparticles or a combination thereof.Type: GrantFiled: July 26, 2010Date of Patent: August 19, 2014Assignee: The United States of America as Represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Martha K. Williams, Luke B. Roberson, Lanetra C. Tate, Trent M. Smith, Tracy L. Gibson, Scott T. Jolley, Pedro J. Medelius
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Publication number: 20140222199Abstract: 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: ApplicationFiled: February 7, 2014Publication date: August 7, 2014Applicants: The U.S.A. As Represented by the Administrator of the National Aeronautics and Space Administration, GM GLOBAL TECHNOLOGY OPERATIONS LLCInventors: Chris A. Ihrke, Bryan J. Bergelin, Lyndon Bridgwater
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Publication number: 20140217762Abstract: 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: ApplicationFiled: February 7, 2014Publication date: August 7, 2014Applicants: The U.S.A. As Represented by the Administrator of the National Aeronautics and Space Administration, GM GLOBAL TECHNOLOGY OPERATIONS LLCInventors: Chris A. Ihrke, Myron A. Diftler, Lyndon Bridgwater, Vienny Nguyen, Alexander Millerman
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Patent number: 8795147Abstract: An apparatus and method to modify the genetic regulation of mammalian tissue, bone, or any combination.Type: GrantFiled: October 7, 2010Date of Patent: August 5, 2014Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Thomas J. Goodwin, Linda C. Shackelford
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Patent number: 8790773Abstract: A dielectric material includes a network of nanosubstrates, such as but not limited to nanotubes, nanosheets, or other nanomaterials or nanostructures, a polymer base material or matrix, and nanoparticles constructed at least partially of an elemental metal. The network has a predetermined nanosubstrate loading percentage by weight with respect to a total weight of the dielectric material, and a preferential or predetermined longitudinal alignment with respect to an orientation of an incident electrical field. A method of forming the dielectric material includes depositing the metal-based nanoparticles onto the nanosubstrates and subsequently mixing these with a polymer matrix. Once mixed, alignment can be achieved by melt extrusion or a similar mechanical shearing process. Alignment of the nanosubstrate may be in horizontal or vertical direction with respect to the orientation of an incident electrical field.Type: GrantFiled: July 16, 2008Date of Patent: July 29, 2014Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Kenneth L. Dudley, Holly A Elliott, John W. Connell, Joseph G. Smith, Sayata Ghose, Kent A. Watson, Donavon Mark Delozier