Patents by Inventor Tab Hunter Crooks

Tab Hunter Crooks 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: 11780781
    Abstract: Adhesive compositions and methods for bonding materials with different thermal expansion coefficients is provided. The adhesive is formulated using a flux material, a low flux material, and a filler material, where the filler material comprises particulate from at least one of the two components being bonded together. A thickening agent can also be used as part of the adhesive composition to aid in applying the adhesive and establishing a desired bond thickness. The method of forming a high strength bond using the disclosed adhesive does not require the use of intermediary layer or the use of high cure temperatures that could damage one or both of the components being bonded together.
    Type: Grant
    Filed: December 16, 2020
    Date of Patent: October 10, 2023
    Assignee: THE BOEING COMPANY
    Inventors: Tab Hunter Crooks, MaryAnn S. Muench
  • Patent number: 11376543
    Abstract: Methods and systems of collecting carbon dioxide are disclosed. In one example, a method includes removing water from atmospheric air with a condenser and a desiccant material to produce dry air, adsorbing carbon dioxide to a material from the dry air, releasing the adsorbed carbon dioxide to a vacuum chamber, and transitioning the released carbon dioxide from a gas to a solid in the vacuum chamber.
    Type: Grant
    Filed: October 1, 2018
    Date of Patent: July 5, 2022
    Assignee: The Boeing Company
    Inventors: Anthony M. DiCenzo, Joseph P. Bruschi, James G. Parlett, Douglas Anthony Galasso, Tab Hunter Crooks
  • Publication number: 20210261472
    Abstract: Adhesive compositions and methods for bonding materials with different thermal expansion coefficients is provided. The adhesive is formulated using a flux material, a low flux material, and a filler material, where the filler material comprises particulate from at least one of the two components being bonded together. A thickening agent can also be used as part of the adhesive composition to aid in applying the adhesive and establishing a desired bond thickness. The method of forming a high strength bond using the disclosed adhesive does not require the use of intermediary layer or the use of high cure temperatures that could damage one or both of the components being bonded together.
    Type: Application
    Filed: December 16, 2020
    Publication date: August 26, 2021
    Inventors: Tab Hunter Crooks, MaryAnn S. Muench
  • Patent number: 11028020
    Abstract: A method of making a ceramic composite comprises forming a wet ceramic composition comprising a plurality of discrete ceramic components and a fluxing agent dissolved in a solvent. At least a portion of the solvent is removed from the wet ceramic composition to form a dried ceramic composition comprising the plurality of discrete ceramic components coated with the fluxing agent. The dried ceramic composition is sintered to form the ceramic composite, the sintering being carried out at a sinter temperature sufficient to fuse the discrete ceramic components at bridging sites formed where two or more of the discrete ceramic components coated with fluxing agent are in physical contact.
    Type: Grant
    Filed: September 26, 2018
    Date of Patent: June 8, 2021
    Assignee: THE BOEING COMPANY
    Inventors: Tab Hunter Crooks, MaryAnn S. Muench
  • Patent number: 10894747
    Abstract: Adhesive compositions and methods for bonding materials with different thermal expansion coefficients is provided. The adhesive is formulated using a flux material, a low flux material, and a filler material, where the filler material comprises particulate from at least one of the two components being bonded together. A thickening agent can also be used as part of the adhesive composition to aid in applying the adhesive and establishing a desired bond thickness. The method of forming a high strength bond using the disclosed adhesive does not require the use of intermediary layer or the use of high cure temperatures that could damage one or both of the components being bonded together.
    Type: Grant
    Filed: May 21, 2018
    Date of Patent: January 19, 2021
    Assignee: The Boeing Company
    Inventors: Tab Hunter Crooks, MaryAnn S. Muench
  • Publication number: 20200095172
    Abstract: A method of making a ceramic composite comprises forming a wet ceramic composition comprising a plurality of discrete ceramic components and a fluxing agent dissolved in a solvent. At least a portion of the solvent is removed from the wet ceramic composition to form a dried ceramic composition comprising the plurality of discrete ceramic components coated with the fluxing agent. The dried ceramic composition is sintered to form the ceramic composite, the sintering being carried out at a sinter temperature sufficient to fuse the discrete ceramic components at bridging sites formed where two or more of the discrete ceramic components coated with fluxing agent are in physical contact.
    Type: Application
    Filed: September 26, 2018
    Publication date: March 26, 2020
    Inventors: Tab Hunter Crooks, MaryAnn S. Muench
  • Publication number: 20190030478
    Abstract: Methods and systems of collecting carbon dioxide are disclosed. In one example, a method includes removing water from atmospheric air with a condenser and a desiccant material to produce dry air, adsorbing carbon dioxide to a material from the dry air, releasing the adsorbed carbon dioxide to a vacuum chamber, and transitioning the released carbon dioxide from a gas to a solid in the vacuum chamber.
    Type: Application
    Filed: October 1, 2018
    Publication date: January 31, 2019
    Applicant: The Boeing Company
    Inventors: Anthony M. DiCenzo, Joseph P. Bruschi, James G. Parlett, Douglas Anthony Galasso, Tab Hunter Crooks
  • Patent number: 10118122
    Abstract: Methods and systems of collecting carbon dioxide are disclosed. In one example, a method includes removing water from atmospheric air with a condenser and a desiccant material to produce dry air, adsorbing carbon dioxide to a material from the dry air, releasing the adsorbed carbon dioxide to a vacuum chamber, and transitioning the released carbon dioxide from a gas to a solid in the vacuum chamber.
    Type: Grant
    Filed: August 29, 2011
    Date of Patent: November 6, 2018
    Assignee: The Boeing Company
    Inventors: Anthony M. DiCenzo, Joseph P. Bruschi, James G. Parlett, Douglas Anthony Galasso, Tab Hunter Crooks
  • Publication number: 20180265418
    Abstract: Adhesive compositions and methods for bonding materials with different thermal expansion coefficients is provided. The adhesive is formulated using a flux material, a low flux material, and a filler material, where the filler material comprises particulate from at least one of the two components being bonded together. A thickening agent can also be used as part of the adhesive composition to aid in applying the adhesive and establishing a desired bond thickness. The method of forming a high strength bond using the disclosed adhesive does not require the use of intermediary layer or the use of high cure temperatures that could damage one or both of the components being bonded together.
    Type: Application
    Filed: May 21, 2018
    Publication date: September 20, 2018
    Inventors: Tab Hunter Crooks, MaryAnn S. Muench
  • Patent number: 9994489
    Abstract: Adhesive compositions and methods for bonding materials with different thermal expansion coefficients is provided. The adhesive is formulated using a flux material, a low flux material, and a filler material, where the filler material comprises particulate from at least one of the two components being bonded together. A thickening agent can also be used as part of the adhesive composition to aid in applying the adhesive and establishing a desired bond thickness. The method of forming a high strength bond using the disclosed adhesive does not require the use of intermediary layer or the use of high cure temperatures that could damage one or both of the components being bonded together.
    Type: Grant
    Filed: December 30, 2014
    Date of Patent: June 12, 2018
    Assignee: The Boeing Company
    Inventors: Tab Hunter Crooks, MaryAnn S. Muench
  • Publication number: 20160264478
    Abstract: Adhesive compositions and methods for bonding materials with different thermal expansion coefficients is provided. The adhesive is formulated using a flux material, a low flux material, and a filler material, where the filler material comprises particulate from at least one of the two components being bonded together. A thickening agent can also be used as part of the adhesive composition to aid in applying the adhesive and establishing a desired bond thickness. The method of forming a high strength bond using the disclosed adhesive does not require the use of intermediary layer or the use of high cure temperatures that could damage one or both of the components being bonded together.
    Type: Application
    Filed: December 30, 2014
    Publication date: September 15, 2016
    Inventors: Tab Hunter Crooks, MaryAnn S. Muench
  • Publication number: 20160207840
    Abstract: An extrudable ceramic composite includes a matrix comprising a refractory ceramic and a plurality of particles embedded in the matrix. The plurality of particles have an aspect ratio ranging from about 1 to about 100, the plurality of particles comprising at least one particle type chosen from structurally reinforcing particles and thermal conductivity modifying particles. Methods of making the ceramic composite are also disclosed.
    Type: Application
    Filed: January 21, 2015
    Publication date: July 21, 2016
    Inventors: Tab Hunter Crooks, Sangvavann Heng
  • Patent number: 8957303
    Abstract: In an embodiment of the disclosure, there is provided a strain isolation layer assembly. The assembly has a rigid solar layer; a strain isolation layer having a discontinuous configuration, a vertical rigidity, and a horizontal shear flexibility; and an underlying substrate layer. The strain isolation layer is coupled between the rigid solar layer and the underlying substrate layer to form a strain isolation layer assembly, such that the strain isolation layer isolates the rigid solar layer to reduce one or more strains induced on the rigid solar layer.
    Type: Grant
    Filed: October 31, 2011
    Date of Patent: February 17, 2015
    Assignee: The Boeing Company
    Inventors: Robert Erik Grip, Blaine Knight Rawdon, Tab Hunter Crooks, Michael F. Stoia
  • Publication number: 20130104966
    Abstract: In an embodiment of the disclosure, there is provided a strain isolation layer assembly. The assembly has a rigid solar layer; a strain isolation layer having a discontinuous configuration, a vertical rigidity, and a horizontal shear flexibility; and an underlying substrate layer. The strain isolation layer is coupled between the rigid solar layer and the underlying substrate layer to form a strain isolation layer assembly, such that the strain isolation layer isolates the rigid solar layer to reduce one or more strains induced on the rigid solar layer.
    Type: Application
    Filed: October 31, 2011
    Publication date: May 2, 2013
    Applicant: The Boeing Company
    Inventors: Robert Erik Grip, Blaine Knight Rawdon, Tab Hunter Crooks, Michael F. Stola