Patents by Inventor Supriya Balachander

Supriya Balachander 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: 10730604
    Abstract: The present disclosure relates to inserts for use with sandwich panels, such as composite panels, and related methods. Presently disclosed inserts may include a retention feature and/or an anti-rotation feature that may be configured to retain the insert in place within a bore formed in the sandwich panel. In this manner, presently disclosed inserts may be secured without the use of adhesive compounds, which may increase efficiency and/or reduce costs in manufacturing apparatus that include one or more sandwich panels having one or more inserts placed therein. Presently disclosed methods of installing an insert into a sandwich panel may include rotating the insert with respect to the sandwich panel as the insert is installed, such that a portion of the insert may be positioned under the skin of the sandwich panel (e.g., a portion of the insert may be positioned between the skin and the core of the sandwich panel).
    Type: Grant
    Filed: September 5, 2018
    Date of Patent: August 4, 2020
    Assignee: The Boeing Company
    Inventors: Michael Steven Lewis, Brad Jeremy Reeves, James S. Bradley, Christopher John Mills, Supriya Balachander, Brian M. Wilkie
  • Publication number: 20190009880
    Abstract: The present disclosure relates to inserts for use with sandwich panels, such as composite panels, and related methods. Presently disclosed inserts may include a retention feature and/or an anti-rotation feature that may be configured to retain the insert in place within a bore formed in the sandwich panel. In this manner, presently disclosed inserts may be secured without the use of adhesive compounds, which may increase efficiency and/or reduce costs in manufacturing apparatus that include one or more sandwich panels having one or more inserts placed therein. Presently disclosed methods of installing an insert into a sandwich panel may include rotating the insert with respect to the sandwich panel as the insert is installed, such that a portion of the insert may be positioned under the skin of the sandwich panel (e.g., a portion of the insert may be positioned between the skin and the core of the sandwich panel).
    Type: Application
    Filed: September 5, 2018
    Publication date: January 10, 2019
    Inventors: Michael Steven Lewis, Brad Jeremy Reeves, James S. Bradley, Christopher John Mills, Supriya Balachander, Brian M. Wilkie
  • Patent number: 10099767
    Abstract: The present disclosure relates to inserts for use with sandwich panels, such as composite panels, and related methods. Presently disclosed inserts may include a retention feature and/or an anti-rotation feature that may be configured to retain the insert in place within a bore formed in the sandwich panel. In this manner, presently disclosed inserts may be secured without the use of adhesive compounds, which may increase efficiency and/or reduce costs in manufacturing apparatus that include one or more sandwich panels having one or more inserts placed therein. Presently disclosed methods of installing an insert into a sandwich panel may include rotating the insert with respect to the sandwich panel as the insert is installed, such that a portion of the insert may be positioned under the skin of the sandwich panel (e.g., a portion of the insert may be positioned between the skin and the core of the sandwich panel).
    Type: Grant
    Filed: August 4, 2015
    Date of Patent: October 16, 2018
    Assignee: The Boeing Company
    Inventors: Michael Steven Lewis, Brad Jeremy Reeves, James S. Bradley, Christopher John Mills, Supriya Balachander, Brian M. Wilkie
  • Publication number: 20170036750
    Abstract: The present disclosure relates to inserts for use with sandwich panels, such as composite panels, and related methods. Presently disclosed inserts may include a retention feature and/or an anti-rotation feature that may be configured to retain the insert in place within a bore formed in the sandwich panel. In this manner, presently disclosed inserts may be secured without the use of adhesive compounds, which may increase efficiency and/or reduce costs in manufacturing apparatus that include one or more sandwich panels having one or more inserts placed therein. Presently disclosed methods of installing an insert into a sandwich panel may include rotating the insert with respect to the sandwich panel as the insert is installed, such that a portion of the insert may be positioned under the skin of the sandwich panel (e.g., a portion of the insert may be positioned between the skin and the core of the sandwich panel).
    Type: Application
    Filed: August 4, 2015
    Publication date: February 9, 2017
    Applicant: The Boeing Company
    Inventors: Michael Steven Lewis, Brad Jeremy Reeves, James S. Bradley, Christopher John Mills, Supriya Balachander, Brian M. Wilkie