Patents Assigned to National Institute of Aerospace Associates
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Patent number: 10607742Abstract: The invention consists of radiation shielding materials for shielding in the most structurally robust combination against galactic cosmic radiation (GCR), neutrons, and solar energetic particles (SEP). Materials for vehicles, space structures, habitats, landers, rovers, and spacesuits must possess functional characteristics of radiation shielding, thermal protection, pressure resistance, and mechanical durability. The materials are tailored to offer the greatest shielding against GCR, neutrons, and SEP in the most structurally robust combination, also capable of shielding against micrometeoriod impact. The boron nitride nanotube (BNNT) is composed entirely of low Z atoms (boron and nitrogen).Type: GrantFiled: November 19, 2012Date of Patent: March 31, 2020Assignees: National Institute of Aerospace Associates, United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Sheila A. Thibeault, Catharine C. Fay, Godfrey Sauti, Jin Ho Kang, Cheol Park
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Patent number: 10435293Abstract: Formation of a boron nitride nanotube nanocomposite film by combining a boron nitride nanotube solution with a matrix such as a polymer or a ceramic to form a boron nitride nanotube/polyimide mixture and synthesizing a boron nitride nanotube/polyimide nanocomposite film as an electroactive layer.Type: GrantFiled: October 13, 2010Date of Patent: October 8, 2019Assignees: National Institute of Aerospace Associates, The United States of America as represented by the Administrator of NASAInventors: Jin Ho Kang, Cheol Park, Joycelyn S. Harrison, Michael W. Smith, Sharon E. Lowther, Jae-Woo Kim, Godfrey Sauti
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Patent number: 10262951Abstract: A novel radiation hardened chip package technology protects microelectronic chips and systems in aviation/space or terrestrial devices against high energy radiation. The proposed technology of a radiation hardened chip package using rare earth elements and mulitlayered structure provides protection against radiation bombardment from alpha and beta particles to neutrons and high energy electromagnetic radiation.Type: GrantFiled: May 16, 2014Date of Patent: April 16, 2019Assignees: National Institute of Aerospace Associates, The United States of America as represented by the Administrator of NASAInventors: Jin Ho Kang, Godfrey Sauti, Cheol Park, Luke Gibbons, Sheila Ann Thibeault, Sharon E. Lowther, Robert G. Bryant
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Patent number: 9845269Abstract: Multifunctional Boron Nitride nanotube-Boron Nitride (BN—BN) nanocomposites for energy transducers, thermal conductors, anti-penetrator/wear resistance coatings, and radiation hardened materials for harsh environments. An all boron-nitride structured BN—BN composite is synthesized. A boron nitride containing precursor is synthesized, then mixed with boron nitride nanotubes (BNNTs) to produce a composite solution which is used to make green bodies of different forms including, for example, fibers, mats, films, and plates. The green bodies are pyrolized to facilitate transformation into BN—BN composite ceramics. The pyrolysis temperature, pressure, atmosphere and time are controlled to produce a desired BN crystalline structure. The wholly BN structured materials exhibit excellent thermal stability, high thermal conductivity, piezoelectricity as well as enhanced toughness, hardness, and radiation shielding properties.Type: GrantFiled: March 29, 2013Date of Patent: December 19, 2017Assignees: National Institute of Aerospace Associates, The United States of America as represented by the Administration of NASAInventors: Jin Ho Kang, Robert G. Bryant, Cheol Park, Godfrey Sauti, Luke Gibbons, Sharon Lowther, Sheila A. Thibeault, Catharine C. Fay
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Patent number: 9137883Abstract: Robust, flexible, lightweight, low profile enhanced performance dielectric barrier discharge actuators (plasma actuators) based on aerogels/nanofoams with controlled pore size and size distribution as well as pore shape. The plasma actuators offer high body force as well as high force to weight ratios (thrust density). The flexibility and mechanical robustness of the actuators allows them to be shaped to conform to the surface to which they are applied. Carbon nanotube (CNT) based electrodes serve to further decrease the weight and profile of the actuators while maintaining flexibility while insulating nano-inclusions in the matrix enable tailoring of the mechanical properties. Such actuators are required for flow control in aeronautics and moving machinery such as wind turbines, noise abatement in landing gear and rotary wing aircraft and other applications.Type: GrantFiled: May 27, 2014Date of Patent: September 15, 2015Assignees: NATIONAL INSTITUTE OF AEROSPACE ASSOCIATES, THE UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONInventors: Godfrey Sauti, Tian-Bing Xu, Emilie J. Siochi, Stephen P. Wilkinson, Mary Ann B. Meador, Haiquan N. Guo
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Publication number: 20150248941Abstract: The invention consists of radiation shielding materials for shielding in the most structurally robust combination against galactic cosmic radiation (GCR), neutrons, and solar energetic particles (SEP). Materials for vehicles, space structures, habitats, landers, rovers, and spacesuits must possess functional characteristics of radiation shielding, thermal protection, pressure resistance, and mechanical durability. The materials are tailored to offer the greatest shielding against GCR, neutrons, and SEP in the most structurally robust combination, also capable of shielding against micrometeoriod impact. The boron nitride nanotube (BNNT) is composed entirely of low Z atoms (boron and nitrogen).Type: ApplicationFiled: November 19, 2012Publication date: September 3, 2015Applicants: U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration, National Institute of Aerospace AssociatesInventors: National Institute of Aerospace Associates, U.S.A. as represented by the Administrator of the Administrator of the National Aeronautics and Space Administration
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Patent number: 9120677Abstract: A scalable method allows preparation of bulk quantities of holey carbon allotropes with holes ranging from a few to over 100 nm in diameter. Carbon oxidation catalyst nanoparticles are first deposited onto a carbon allotrope surface in a facile, controllable, and solvent-free process. The catalyst-loaded carbons are then subjected to thermal treatment in air. The carbons in contact with the carbon oxidation catalyst nanoparticles are selectively oxidized into gaseous byproducts such as CO or CO2, leaving the surface with holes. The catalyst is then removed via refluxing in diluted nitric acid to obtain the final holey carbon allotropes. The average size of the holes correlates strongly with the size of the catalyst nanoparticles and is controlled by adjusting the catalyst precursor concentration. The temperature and time of the air oxidation step, and the catalyst removal treatment conditions, strongly affect the morphology of the holes.Type: GrantFiled: April 1, 2013Date of Patent: September 1, 2015Assignees: National Institute of Aerospace Associates, The United States of America as represented by the Administration of NASAInventors: Kent Watson, Yi Lin, Sayata Ghose, John Connell
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Publication number: 20140134352Abstract: 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: ApplicationFiled: November 15, 2012Publication date: May 15, 2014Applicants: U.S. as represented by the Administrator of the National Aeronautics and Space Administration, National Institute of Aerospace AssociatesInventors: Jae Woo Kim, Emilie J. Siochi, Kristopher E. Wise, Yi Lin, John Connell
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Patent number: 8680749Abstract: A novel full piezoelectric multilayer stacked hybrid actuation/transduction system. The system demonstrates significantly-enhanced electromechanical performance by utilizing the cooperative contributions of the electromechanical responses of multilayer stacked negative and positive strain components. Both experimental and theoretical studies indicate that for this system, the displacement is over three times that of a same-sized conventional flextensional actuator/transducer. The system consists of at least 2 layers which include electromechanically active components. The layers are arranged such that when electric power is applied, one layer contracts in a transverse direction while the second layer expands in a transverse direction which is perpendicular to the transverse direction of the first layer. An alternate embodiment includes a third layer.Type: GrantFiled: September 3, 2009Date of Patent: March 25, 2014Assignees: National Institute of Aerospace Associates, The United States of America as represented by the Administration of NASAInventors: Tian-Bing Xu, Xiaoning Jiang, Ji Su
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Patent number: 8529825Abstract: A new fabrication method for nanovoids-imbedded bismuth telluride (Bi—Te) material with low dimensional (quantum-dots, quantum-wires, or quantum-wells) structure was conceived during the development of advanced thermoelectric (TE) materials. Bismuth telluride is currently the best-known candidate material for solid-state TE cooling devices because it possesses the highest TE figure of merit at room temperature. The innovative process described here allows nanometer-scale voids to be incorporated in Bi—Te material. The final nanovoid structure such as void size, size distribution, void location, etc. can be also controlled under various process conditions.Type: GrantFiled: December 3, 2010Date of Patent: September 10, 2013Assignees: National Institute of Aerospace Associates, The United States of America as represented by the Administration of NASAInventors: Sang-Hyon Chu, Sang H. Choi, Jae-Woo Kim, Yeonjoon Park, James R. Elliott, Glen C. King, Diane M. Stoakley
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Publication number: 20130119316Abstract: Effective radiation shielding is required to protect crew and equipment in various fields including aerospace, defense, medicine and power generation. Light elements and in particular hydrogen are most effective at shielding against high-energy particles including galactic cosmic rays, solar energetic particles and fast neutrons. However, pure hydrogen is highly flammable, has a low neutron absorption cross-section, and cannot be made into structural components. Nanocomposites containing the light elements Boron, Nitrogen, Carbon and Hydrogen as well dispersed boron nano-particles, boron nitride nanotubes (BNNTs) and boron nitride nano-platelets, in a matrix, provide effective radiation shielding materials in various functional forms. Boron and nitrogen have large neutron absorption cross-sections and wide absorption spectra.Type: ApplicationFiled: May 9, 2011Publication date: May 16, 2013Applicants: National Institute of Aerospace Associates, Thomas Jefferson National Accelerator Facility, and Space AdministrationInventors: Godfrey Sauti, Cheol Park, Jin Ho Kang, Jae-Woo Kim, Joycelyn S. Harrison, Michael W. Smith, Kevin Jordan, Sharon E. Lowther, Peter T. Lillehei, Sheila A. Thibeault
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Publication number: 20120186742Abstract: Boron nitride nanotubes (BNNTs), boron nitride nanoparticles (BNNPs), carbon nanotubes (CNTs), graphites, or combinations, are incorporated into matrices of polymer, ceramic or metals. Fibers, yarns, and woven or nonwoven mats of BNNTs are used as toughening layers in penetration resistant materials to maximize energy absorption and/or high hardness layers to rebound or deform penetrators. They can be also used as reinforcing inclusions combining with other polymer matrices to create composite layers like typical reinforcing fibers such as Kevlar®, Spectra®, ceramics and metals. Enhanced wear resistance and usage time are achieved by adding boron nitride nanomaterials, increasing hardness and toughness. Such materials can be used in high temperature environments since the oxidation temperature of BNNTs exceeds 800° C. in air.Type: ApplicationFiled: July 26, 2011Publication date: July 26, 2012Applicants: National Institute of Aerospace Associates, Thomas Jefferson National Accelerator Facility, Space AdministrationInventors: Jin Ho Kang, Cheol Park, Godfrey Sauti, Michael W. Smith, Kevin C. Jordan, Sharon E. Lowther, Robert George Bryant
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Patent number: 8217143Abstract: Metal nanoshells are fabricated by admixing an aqueous solution of metal ions with an aqueous solution of apoferritin protein molecules, followed by admixing an aqueous solution containing an excess of an oxidizing agent for the metal ions. The apoferritin molecules serve as bio-templates for the formation of metal nanoshells, which form on and are bonded to the inside walls of the hollow cores of the individual apoferritin molecules. Control of the number of metal atoms which enter the hollow core of each individual apoferritin molecule provides a hollow metal nonparticle, or nanoshell, instead of a solid spherical metal nanoparticle.Type: GrantFiled: July 12, 2007Date of Patent: July 10, 2012Assignees: National Institute of Aerospace Associates, The United States of America as represented by the Administration of NASAInventors: Jae-Woo Kim, Sang H. Choi, Peter T. Lillehei, Sang-Hyon Chu, Yeonjoon Park, Glen C. King, James R. Elliott, Jr.
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Patent number: 8206674Abstract: Boron nitride nanotubes are prepared by a process which includes: (a) creating a source of boron vapor; (b) mixing the boron vapor with nitrogen gas so that a mixture of boron vapor and nitrogen gas is present at a nucleation site, which is a surface, the nitrogen gas being provided at a pressure elevated above atmospheric, e.g., from greater than about 2 atmospheres up to about 250 atmospheres; and (c) harvesting boron nitride nanotubes, which are formed at the nucleation site.Type: GrantFiled: May 14, 2008Date of Patent: June 26, 2012Assignees: National Institute of Aerospace Associates, The United States of America as represented by the Administration of NASAInventors: Michael W. Smith, Kevin Jordan, Cheol Park
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Patent number: 8083986Abstract: A novel method to prepare an advanced thermoelectric material has hierarchical structures embedded with nanometer-sized voids which are key to enhancement of the thermoelectric performance. Solution-based thin film deposition technique enables preparation of stable film of thermoelectric material and void generator (voigen). A subsequent thermal process creates hierarchical nanovoid structure inside the thermoelectric material. Potential application areas of this advanced thermoelectric material with nanovoid structure are commercial applications (electronics cooling), medical and scientific applications (biological analysis device, medical imaging systems), telecommunications, and defense and military applications (night vision equipments).Type: GrantFiled: December 4, 2008Date of Patent: December 27, 2011Assignees: National Institute of Aerospace Associates, The United States of America as represented by the Adminstration of NASAInventors: Sang Hyouk Choi, Yeonjoon Park, Sang-Hyon Chu, James R. Elliott, Glen C. King, Jae-Woo Kim, Peter T. Lillehei, Diane M. Stoakley
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Publication number: 20110192016Abstract: Electroactive actuation characteristics of novel BNNT based materials are described. Several series of BNNT based electroactive materials including BNNT/polyimide composites and BNNT films are prepared. The BNNT based electroactive materials show high piezoelectric coefficients, d13, about 14.80 pm/V as well as high electrostrictive coefficients, M13, 3.21×10?16 pm2N2. The BNNT based electroactive materials will be used for novel electromechanical energy conversion devices.Type: ApplicationFiled: October 13, 2010Publication date: August 11, 2011Applicants: National Institute of Aerospace Associates, USA as represented by the Administrator of the National Aeronautics and Space Administration, Jefferson Science Associates, LLCInventors: Jin Ho Kang, Cheol Park, Joycelyn S. Harrison, Michael W. Smith, Sharon E. Lowther, Jae-Woo Kim, Godfrey Sauti
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Publication number: 20110117690Abstract: A new fabrication method for nanovoids-imbedded bismuth telluride (Bi—Te) material with low dimensional (quantum-dots, quantum-wires, or quantum-wells) structure was conceived during the development of advanced thermoelectric (TE) materials. Bismuth telluride is currently the best-known candidate material for solid-state TE cooling devices because it possesses the highest TE figure of merit at room temperature. The innovative process described here allows nanometer-scale voids to be incorporated in Bi—Te material. The final nanovoid structure such as void size, size distribution, void location, etc. can be also controlled under various process conditions.Type: ApplicationFiled: December 3, 2010Publication date: May 19, 2011Applicants: National Institute of Aerospace Associates, and Space AdministrationInventors: Sang-Hyon Chu, Sang Hyouk Choi, Jae-Woo Kim, Yeonjoon Park, James R. Elliott, JR., Glen C. King, Diane M. Stoakley
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Publication number: 20110068291Abstract: A novel method to develop highly conductive functional materials which can effectively shield various electromagnetic effects (EMEs) and harmful radiations. Metallized nanotube polymer composites (MNPC) are composed of a lightweight polymer matrix, superstrong nanotubes (NT), and functional nanoparticle inclusions. MNPC is prepared by supercritical fluid infusion of various metal precursors (Au, Pt, Fe, and Ni salts), incorporated simultaneously or sequentially, into a solid NT-polymer composite followed by thermal reduction. The infused metal precursor tends to diffuse toward the nanotube surface preferentially as well as the surfaces of the NT-polymer matrix, and is reduced to form nanometer-scale metal particles or metal coatings. The conductivity of the MNPC increases with the metallization, which provides better shielding capabilities against various EMEs and radiations by reflecting and absorbing EM waves more efficiently.Type: ApplicationFiled: November 26, 2008Publication date: March 24, 2011Applicant: National Institute of Aerospace AssociatesInventors: Cheol Park, Joycelyn S. Harrison, Negin Nazem, Larry T. Taylor, Jin Ho Kang, Jae-Woo Kim, Godfrey Sauti, Peter T. Lillehei, Sharon E. Lowther
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Patent number: 7704553Abstract: A process for depositing nanometer-sized metal particles onto a substrate in the absence of aqueous solvents, organic solvents, and reducing agents, and without any required pre-treatment of the substrate, includes preparing an admixture of a metal compound and a substrate by dry mixing a chosen amount of the metal compound with a chosen amount of the substrate; and supplying energy to the admixture in an amount sufficient to deposit zero valance metal particles onto the substrate. This process gives rise to a number of deposited metallic particle sizes which may be controlled. The compositions prepared by this process are used to produce polymer composites by combining them with readily available commodity and engineering plastics. The polymer composites are used as coatings, or they are used to fabricate articles, such as free-standing films, fibers, fabrics, foams, molded and laminated articles, tubes, adhesives, and fiber reinforced articles.Type: GrantFiled: February 23, 2007Date of Patent: April 27, 2010Assignees: National Institute of Aerospace Associates, The United States of America as represented by the Administrator of NASAInventors: Kent A. Watson, Michael J. Fallbach, Sayata Ghose, Joseph G. Smith, Donavon M. Delozier, John W. Connell
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Publication number: 20100096949Abstract: A novel full piezoelectric multilayer stacked hybrid actuation/transduction system. The system demonstrates significantly-enhanced electromechanical performance by utilizing the cooperative contributions of the electromechanical responses of multilayer stacked negative and positive strain components. Both experimental and theoretical studies indicate that for this system, the displacement is over three times that of a same-sized conventional flextensional actuator/transducer. The system consists of at least 2 layers which include electromechanically active components. The layers are arranged such that when electric power is applied, one layer contracts in a transverse direction while the second layer expands in a transverse direction which is perpendicular to the transverse direction of the first layer. An alternate embodiment includes a third layer.Type: ApplicationFiled: September 3, 2009Publication date: April 22, 2010Applicants: National Institute of Aerospace Associates, Space AdministrationInventors: Tian-Bing Xu, Xiaoning Jing, Ji Su