Patents by Inventor Hyun I. Kim

Hyun I. Kim 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).

  • Patent number: 11940266
    Abstract: Processes for rapidly and accurately measuring the coefficient of moisture expansion for materials, such as adhesives, are disclosed. A replication technique may be used to manufacture highly flat and smooth adhesive samples. Moisture is introduced in a controlled humidity atmosphere, distortion is monitored with an accurate laser interferometer (e.g., ˜1 nanometer (nm) accuracy), and measurements are correlated with moisture content change. Such processes decrease sample size by three orders of magnitude as compared with conventional techniques and have a smaller adhesive mass requirement, which enables measurement of expensive microelectronic adhesives that were previously cost-prohibitive to measure. Also, thinner films allow CME measurements of ultraviolet (UV) cured adhesives that would otherwise have depth of penetration issues. Furthermore, saturation occurs quickly, allowing pre-stabilization at room temperature, which enabled parametric studies as a function of processing or cure state.
    Type: Grant
    Filed: September 21, 2021
    Date of Patent: March 26, 2024
    Assignee: THE AEROSPACE CORPORATION
    Inventors: Geena L. Ferrelli, Hyun I. Kim, Rafael J. Zaldivar
  • Patent number: 11762301
    Abstract: An assembly comprises an exposure chamber configured to receive a structure and identify at least one portion of the structure for further processing. The exposure chamber is further configured to expose the at least one portion of the structure to radiation such that a high cure state and a low residual stress are achieved for the structure. A dosage level of the radiation is determined based, at least in part, on the composition of the structure.
    Type: Grant
    Filed: July 19, 2021
    Date of Patent: September 19, 2023
    Assignee: THE AEROSPACE CORPORATION
    Inventors: Rafael J. Zaldivar, Geena L. Ferrelli, Hyun I. Kim
  • Publication number: 20230091655
    Abstract: Processes for rapidly and accurately measuring the coefficient of moisture expansion for materials, such as adhesives, are disclosed. A replication technique may be used to manufacture highly flat and smooth adhesive samples. Moisture is introduced in a controlled humidity atmosphere, distortion is monitored with an accurate laser interferometer (e.g., ˜1 nanometer (nm) accuracy), and measurements are correlated with moisture content change. Such processes decrease sample size by three orders of magnitude as compared with conventional techniques and have a smaller adhesive mass requirement, which enables measurement of expensive microelectronic adhesives that were previously cost-prohibitive to measure. Also, thinner films allow CME measurements of ultraviolet (UV) cured adhesives that would otherwise have depth of penetration issues. Furthermore, saturation occurs quickly, allowing pre-stabilization at room temperature, which enabled parametric studies as a function of processing or cure state.
    Type: Application
    Filed: September 21, 2021
    Publication date: March 23, 2023
    Applicant: The Aerospace Corporation
    Inventors: Geena L. FERRELLI, Hyun I. KIM, Rafael J. ZALDIVAR
  • Patent number: 11525763
    Abstract: A system includes a curing assembly for low temperature curing and residual stress relief of material substrates. The curing assembly includes a first exposure chamber configured to expose the material substrate to UV radiation, and a second exposure chamber configured to expose the material substrate to Gamma radiation. In some embodiments, a mixing apparatus may mix nano-filler particles into the material substrate prior to exposure to Gamma radiation. The cure assembly may also include a control system for determining exposure dosages and exposure times based at least in part, on the material properties of the material substrate.
    Type: Grant
    Filed: August 31, 2021
    Date of Patent: December 13, 2022
    Assignee: THE AEROSPACE CORPORATION
    Inventors: Rafael J. Zaldivar, Geena L. Ferrelli, Hyun I. Kim
  • Patent number: 11376782
    Abstract: A method of modifying a 3D-printed polymer structure is provided. The method can include providing an initial 3D-printed polymer structure having at least one exposed surface; treating the exposed surface of the initial 3D-printed polymer structure with plasma to obtain a treated 3D-printed polymer structure having a treated surface; administering an adhesive to the treated surface of the treated 3D-printed polymer structure; and contacting a complementary 3D-printed polymer structure with the treated surface of the treated 3D-printed polymer structure to obtain a modified 3D-printed polymer structure.
    Type: Grant
    Filed: February 5, 2020
    Date of Patent: July 5, 2022
    Assignee: THE AEROSPACE CORPORATION
    Inventors: Rafael J. Zaldivar, Hyun I. Kim, Sara M. Gustafson, Tait DeWitt McLouth
  • Publication number: 20210396638
    Abstract: A system includes a curing assembly for low temperature curing and residual stress relief of material substrates. The curing assembly includes a first exposure chamber configured to expose the material substrate to UV radiation, and a second exposure chamber configured to expose the material substrate to Gamma radiation. In some embodiments, a mixing apparatus may mix nano-filler particles into the material substrate prior to exposure to Gamma radiation. The cure assembly may also include a control system for determining exposure dosages and exposure times based at least in part, on the material properties of the material substrate.
    Type: Application
    Filed: August 31, 2021
    Publication date: December 23, 2021
    Inventors: Rafael J. ZALDIVAR, Geena L. FERRELLI, Hyun I. KIM
  • Publication number: 20210349401
    Abstract: An assembly comprises an exposure chamber configured to receive a structure and identify at least one portion of the structure for further processing. The exposure chamber is further configured to expose the at least one portion of the structure to radiation such that a high cure state and a low residual stress are achieved for the structure. A dosage level of the radiation is determined based, at least in part, on the composition of the structure.
    Type: Application
    Filed: July 19, 2021
    Publication date: November 11, 2021
    Inventors: Rafael J. ZALDIVAR, Geena L. FERRELLI, Hyun I. KIM
  • Patent number: 11161333
    Abstract: A method of accelerating the reduction of residual stress in a bonded structure is provided. The method can include: providing a bonded structure having at least two substructures, wherein the substructures are bonded together with an adhesive; and submitting the bonded structure to a high-humidity environment having a relative humidity of at least 75%. The method can also include a step of submitting the bonded structure to an low-humidity environment having a relative humidity of at most 20%. According to the method, the bonded structure can have a first residual stress at a first time and a second residual stress at a second time, wherein an absolute value of the first residual stress is greater than an absolute value of the second residual stress. According to the method, the residual stress at the second time can be about zero.
    Type: Grant
    Filed: January 28, 2020
    Date of Patent: November 2, 2021
    Assignee: THE AEROSPACE CORPORATION
    Inventors: Rafael J. Zaldivar, Geena Linn Ferrelli, Hyun I Kim
  • Patent number: 11125669
    Abstract: A system includes a curing assembly for low temperature curing and residual stress relief of material substrates. The curing assembly includes a first exposure chamber configured to expose the material substrate to UV radiation, and a second exposure chamber configured to expose the material substrate to Gamma radiation. In some embodiments, a mixing apparatus may mix nano-filler particles into the material substrate prior to exposure to Gamma radiation. The cure assembly may also include a control system for determining exposure dosages and exposure times based at least in part, on the material properties of the material substrate.
    Type: Grant
    Filed: July 23, 2018
    Date of Patent: September 21, 2021
    Assignee: THE AEROSPACE CORPORATION
    Inventors: Rafael J. Zaldivar, Geena L. Ferrelli, Hyun I. Kim
  • Publication number: 20210237337
    Abstract: A method of modifying a 3D-printed polymer structure is provided. The method can include providing an initial 3D-printed polymer structure having at least one exposed surface; treating the exposed surface of the initial 3D-printed polymer structure with plasma to obtain a treated 3D-printed polymer structure having a treated surface; administering an adhesive to the treated surface of the treated 3D-printed polymer structure; and contacting a complementary 3D-printed polymer structure with the treated surface of the treated 3D-printed polymer structure to obtain a modified 3D-printed polymer structure.
    Type: Application
    Filed: February 5, 2020
    Publication date: August 5, 2021
    Inventors: Rafael J. Zaldivar, Hyun I. Kim, Sara M. Gustafson, Tait DeWitt McLouth
  • Publication number: 20210229413
    Abstract: A method of accelerating the reduction of residual stress in a bonded structure is provided. The method can include: providing a bonded structure having at least two substructures, wherein the substructures are bonded together with an adhesive; and submitting the bonded structure to a high-humidity environment having a relative humidity of at least 75%. The method can also include a step of submitting the bonded structure to an low-humidity environment having a relative humidity of at most 20%. According to the method, the bonded structure can have a first residual stress at a first time and a second residual stress at a second time, wherein an absolute value of the first residual stress is greater than an absolute value of the second residual stress. According to the method, the residual stress at the second time can be about zero.
    Type: Application
    Filed: January 28, 2020
    Publication date: July 29, 2021
    Inventors: Rafael J. Zaldivar, Geena Linn Ferrelli, Hyun I Kim
  • Patent number: 10562209
    Abstract: A deposition assembly generally comprises a first deposition apparatus that is configured to receive a substrate, such as a glass mandrel. The first deposition apparatus is further configured to deposit a plurality of first monolayer molecules onto at least a surface of the substrate to generate a first coating structure on the substrate. A second deposition apparatus is coupled to the first deposition apparatus, and wherein the second deposition apparatus is configured to deposit a plurality of second monolayer molecules onto at least the surface of the substrate such that the second monolayer molecules are diffused through the first coating structure and at least one aperture is filled by at least one of the second monolayer molecules to generate at least one mold release layer on at least the surface of the substrate.
    Type: Grant
    Filed: February 4, 2016
    Date of Patent: February 18, 2020
    Assignee: The Aerospace Corporation
    Inventors: Hyun I. Kim, Rafael J. Zaldivar, James M. Helt
  • Publication number: 20200025663
    Abstract: A system includes a curing assembly for low temperature curing and residual stress relief of material substrates. The curing assembly includes a first exposure chamber configured to expose the material substrate to UV radiation, and a second exposure chamber configured to expose the material substrate to Gamma radiation. In some embodiments, a mixing apparatus may mix nano-filler particles into the material substrate prior to exposure to Gamma radiation. The cure assembly may also include a control system for determining exposure dosages and exposure times based at least in part, on the material properties of the material substrate.
    Type: Application
    Filed: July 23, 2018
    Publication date: January 23, 2020
    Inventors: Rafael J. ZALDIVAR, Geena L. FERRELLI, Hyun I. KIM
  • Patent number: 10022747
    Abstract: A fabrication assembly comprises an apparatus that receives a composite substrate and a glass substrate having a surface with a release coating layer. A resin layer is deposited between the composite and glass substrates such that a first portion of the resin layer is positioned adjacent to a surface of the composite substrate and a second portion of the resin layer is positioned adjacent to the surface with the release coating layer to prevent aperture(s) from forming. A curing of the resin layer is conducted using electromagnetic radiation. A post-processing chamber receives the resin layer positioned between the composite substrate and the glass substrate and conducts another curing of the resin layer. The resin layer and the composite substrate are released from the glass substrate. Another deposition apparatus receives the resin layer and the composite substrate. A metallic coating is deposited to form a composite mirror object.
    Type: Grant
    Filed: December 18, 2017
    Date of Patent: July 17, 2018
    Assignee: The Aerospace Corporation
    Inventors: Rafael J. Zaldivar, Geena L. Ferrelli, Hyun I. Kim, Dhruv N. Patel
  • Patent number: 9956587
    Abstract: A fabrication assembly comprises an apparatus that receives a composite substrate and a glass substrate having a surface with a release coating layer. A resin layer is deposited between the composite and glass substrates such that a first portion of the resin layer is positioned adjacent to a surface of the composite substrate and a second portion of the resin layer is positioned adjacent to the surface with the release coating layer to prevent aperture(s) from forming. A curing of the resin layer is conducted using electromagnetic radiation. A post-processing chamber receives the resin layer positioned between the composite substrate and the glass substrate and conducts another curing of the resin layer. The resin layer and the composite substrate are released from the glass substrate. Another deposition apparatus receives the resin layer and the composite substrate. A metallic coating is deposited to form a composite mirror object.
    Type: Grant
    Filed: August 29, 2016
    Date of Patent: May 1, 2018
    Assignee: The Aerospace Corporation
    Inventors: Rafael J. Zaldivar, Geena L. Ferrelli, Hyun I. Kim, Dhruv N. Patel
  • Publication number: 20180099310
    Abstract: A fabrication assembly comprises an apparatus that receives a composite substrate and a glass substrate having a surface with a release coating layer. A resin layer is deposited between the composite and glass substrates such that a first portion of the resin layer is positioned adjacent to a surface of the composite substrate and a second portion of the resin layer is positioned adjacent to the surface with the release coating layer to prevent aperture(s) from forming. A curing of the resin layer is conducted using electromagnetic radiation. A post-processing chamber receives the resin layer positioned between the composite substrate and the glass substrate and conducts another curing of the resin layer. The resin layer and the composite substrate are released from the glass substrate. Another deposition apparatus receives the resin layer and the composite substrate. A metallic coating is deposited to form a composite mirror object.
    Type: Application
    Filed: December 18, 2017
    Publication date: April 12, 2018
    Inventors: Rafael J. ZALDIVAR, Geena L. FERRELLI, Hyun I. KIM, Dhruv N. PATEL
  • Publication number: 20180056327
    Abstract: A fabrication assembly comprises an apparatus that receives a composite substrate and a glass substrate having a surface with a release coating layer. A resin layer is deposited between the composite and glass substrates such that a first portion of the resin layer is positioned adjacent to a surface of the composite substrate and a second portion of the resin layer is positioned adjacent to the surface with the release coating layer to prevent aperture(s) from forming. A curing of the resin layer is conducted using electromagnetic radiation. A post-processing chamber receives the resin layer positioned between the composite substrate and the glass substrate and conducts another curing of the resin layer. The resin layer and the composite substrate are released from the glass substrate. Another deposition apparatus receives the resin layer and the composite substrate. A metallic coating is deposited to form a composite mirror object.
    Type: Application
    Filed: August 29, 2016
    Publication date: March 1, 2018
    Inventors: Rafael J. ZALDIVAR, Geena L. FERRELLI, Hyun I. KIM, Dhruv N. PATEL
  • Publication number: 20170225365
    Abstract: A deposition assembly generally comprises a first deposition apparatus that is configured to receive a substrate, such as a glass mandrel. The first deposition apparatus is further configured to deposit a plurality of first monolayer molecules onto at least a surface of the substrate to generate a first coating structure on the substrate. A second deposition apparatus is coupled to the first deposition apparatus, and wherein the second deposition apparatus is configured to deposit a plurality of second monolayer molecules onto at least the surface of the substrate such that the second monolayer molecules are diffused through the first coating structure and at least one aperture is filled by at least one of the second monolayer molecules to generate at least one mold release layer on at least the surface of the substrate.
    Type: Application
    Filed: February 4, 2016
    Publication date: August 10, 2017
    Inventors: Hyun I. Kim, Rafael J. Zaldivar, James M. Helt
  • Patent number: 8916067
    Abstract: A method and composition wherein carbonaceous nano-scaled filler material is subjected to atmospheric plasma treatment using carbon monoxide as the active gas. The treatment with carbon monoxide plasma has been found to significantly increase the incorporation of oxygen groups on the surface of the filler material without degrading the surface and thus serves to increase wettability and dispersion throughout the matrix. The composite that incorporates the treated filler material has enhanced mechanical and electrical properties.
    Type: Grant
    Filed: October 19, 2011
    Date of Patent: December 23, 2014
    Assignee: The Aerospace Corporation
    Inventors: Rafael J. Zaidivar, James P. Nokes, Hyun I. Kim
  • Publication number: 20130099170
    Abstract: A method and composition wherein carbonaceous nano-scaled filler material is subjected to atmospheric plasma treatment using carbon monoxide as the active gas. The treatment with carbon monoxide plasma has been found to significantly increase the incorporation of oxygen groups on the surface of the filler material without degrading the surface and thus serves to increase wettability and dispersion throughout the matrix. The composite that incorporates the treated filler material has enhanced mechanical and electrical properties.
    Type: Application
    Filed: October 19, 2011
    Publication date: April 25, 2013
    Applicant: THE AEROSPACE CORPORATION
    Inventors: RAFAEL J. ZALDIVAR, James P. Nokes, Hyun I. Kim