Patents by Inventor Sheila A. Thibeault

Sheila A. Thibeault has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • Publication number: 20230242704
    Abstract: Various embodiments may include low-creep and low-stress-relaxation polymer composites (or reduced-creep and reduced-stress-relaxation polymer composites) and methods for making low-creep and low-stress-relaxation polymer composites (or reduced-creep and reduced-stress-relaxation polymer composites). Various embodiments may include a polymeric material, comprising: a tetrafunctional epoxy in an epoxy weight amount; an amine hardener in a hardener weight amount, wherein a weight ratio of the epoxy weight amount to the hardener weight amount is 1:0.38 or greater; and an oligomer additive in an additive concentration, the oligomer additive comprising a monomer combined with 4?-hydroxyacetanilide (HAA).
    Type: Application
    Filed: January 31, 2022
    Publication date: August 3, 2023
    Inventors: Jeffrey A. Hinkley, Jin Ho Kang, Keith L. Gordon, Sheila A. Thibeault
  • Publication number: 20230042672
    Abstract: Disclosed herein are composite materials comprising a siliconized carbon fiber fabric and polymeric sizing. In one embodiment, the polymeric sizing can be bismaleimide, an epoxy resin, or both. In another embodiment, the composite materials possess mechanical strength and durability and acceptable performance after extended periods of time in storage. In another embodiment, disclosed herein is a method for making the composite materials, the method including at least the steps of (a) siliconizing the carbon fiber fabric to produce a siliconized carbon fiber fabric; and (b) applying a polymeric sizing material to the siliconized carbon fiber fabric to create the composite material. In yet another embodiment, disclosed herein are composite materials formed by the disclosed process and articles comprising the composite materials including, but not limited to, camping equipment, military equipment, clothing, sporting equipment, aerospace equipment, wrinkle-free fabric, or any combination thereof.
    Type: Application
    Filed: August 5, 2022
    Publication date: February 9, 2023
    Inventors: Jin Ho Kang, Keith L. Gordon, Jeffrey A. Hinkley, Sheila A. Thibeault
  • Patent number: 10607742
    Abstract: 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: Grant
    Filed: November 19, 2012
    Date of Patent: March 31, 2020
    Assignees: National Institute of Aerospace Associates, United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Sheila A. Thibeault, Catharine C. Fay, Godfrey Sauti, Jin Ho Kang, Cheol Park
  • Patent number: 9845269
    Abstract: 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: Grant
    Filed: March 29, 2013
    Date of Patent: December 19, 2017
    Assignees: National Institute of Aerospace Associates, The United States of America as represented by the Administration of NASA
    Inventors: Jin Ho Kang, Robert G. Bryant, Cheol Park, Godfrey Sauti, Luke Gibbons, Sharon Lowther, Sheila A. Thibeault, Catharine C. Fay
  • Patent number: 9449723
    Abstract: 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: Grant
    Filed: March 10, 2014
    Date of Patent: September 20, 2016
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Cheol Park, Godfrey Sauti, Jin Ho Kang, Sharon E. Lowther, Sheila A. Thibeault, Robert G. Bryant
  • Publication number: 20150069588
    Abstract: 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: Application
    Filed: May 16, 2014
    Publication date: March 12, 2015
    Inventors: Jin Ho Kang, Godfrey Sauti, Cheol Park, Luke Gibbons, Sheila A. Thibeault, Sharon E. Lowther, Robert G. Bryant
  • Publication number: 20140265057
    Abstract: 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: Application
    Filed: March 10, 2014
    Publication date: September 18, 2014
    Applicant: U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Cheol Park, Godfrey Sauti, Jin Ho Kang, Sharon E. Lowther, Sheila A. Thibeault, Robert G. Bryant
  • Publication number: 20130119316
    Abstract: 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: Application
    Filed: May 9, 2011
    Publication date: May 16, 2013
    Applicants: National Institute of Aerospace Associates, Thomas Jefferson National Accelerator Facility, and Space Administration
    Inventors: 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