Patents by Inventor Cliff L. Chin

Cliff L. Chin 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: 9725154
    Abstract: A conjugate damper for a structural panel includes a constraining sheet extending between a first edge and a second edge. Each of the first edge and the second edge is at least partially coupled to a first surface of the structural panel. The conjugate damper also includes a damping layer coupled between the constraining sheet and the first surface such that, when the structural panel is in a compressively deformed state, a thickness of the damping layer in a direction generally normal to the first surface is decreased relative to a baseline state. The damping layer includes a viscoelastic material.
    Type: Grant
    Filed: May 13, 2014
    Date of Patent: August 8, 2017
    Assignee: The Boeing Company
    Inventors: Cliff L. Chin, Joshua M. Montgomery
  • Publication number: 20160185442
    Abstract: A conjugate damper for a structural panel includes a constraining sheet extending between a first edge and a second edge. Each of the first edge and the second edge is at least partially coupled to a first surface of the structural panel. The conjugate damper also includes a damping layer coupled between the constraining sheet and the first surface such that, when the structural panel is in a compressively deformed state, a thickness of the damping layer in a direction generally normal to the first surface is decreased relative to a baseline state. The damping layer includes a viscoelastic material.
    Type: Application
    Filed: May 13, 2014
    Publication date: June 30, 2016
    Applicant: The Boeing Company
    Inventors: Cliff L. Chin, Joshua M. Montgomery
  • Patent number: 9353518
    Abstract: A method and apparatus comprising a composite panel and a number of structures to reduce noise radiation from the composite panel. The composite panel has a first face sheet, a second face sheet, and a core located between the first face sheet and the second face sheet. The number of structures is associated with the first face sheet. The number of structures has a mass with a configuration to reduce a speed of waves propagating in the composite panel such that noise radiating from the composite panel is reduced.
    Type: Grant
    Filed: June 24, 2014
    Date of Patent: May 31, 2016
    Assignee: THE BOEING COMPANY
    Inventors: Gopal Prasad Mathur, Cliff L. Chin
  • Publication number: 20140299409
    Abstract: A method and apparatus comprising a composite panel and a number of structures to reduce noise radiation from the composite panel. The composite panel has a first face sheet, a second face sheet, and a core located between the first face sheet and the second face sheet. The number of structures is associated with the first face sheet. The number of structures has a mass with a configuration to reduce a speed of waves propagating in the composite panel such that noise radiating from the composite panel is reduced.
    Type: Application
    Filed: June 24, 2014
    Publication date: October 9, 2014
    Inventors: Gopal Prasad Mathur, Cliff L. Chin
  • Patent number: 8770343
    Abstract: A method and apparatus comprising a composite panel and a number of structures to reduce noise radiation from the composite panel. The composite panel has a first face sheet, a second face sheet, and a core located between the first face sheet and the second face sheet. The number of structures is associated with the first face sheet. The number of structures has a mass with a configuration to reduce a speed of waves propagating in the composite panel such that noise radiating from the composite panel is reduced.
    Type: Grant
    Filed: November 23, 2011
    Date of Patent: July 8, 2014
    Assignee: The Boeing Company
    Inventors: Gopal Prasad Mathur, Cliff L. Chin
  • Publication number: 20130126267
    Abstract: A method and apparatus comprising a composite panel and a number of structures to reduce noise radiation from the composite panel. The composite panel has a first face sheet, a second face sheet, and a core located between the first face sheet and the second face sheet. The number of structures is associated with the first face sheet. The number of structures has a mass with a configuration to reduce a speed of waves propagating in the composite panel such that noise radiating from the composite panel is reduced.
    Type: Application
    Filed: November 23, 2011
    Publication date: May 23, 2013
    Applicant: The Boeing Company
    Inventors: Gopal Prasad Mathur, Cliff L. Chin