Patents by Inventor Samra S. Sangari

Samra S. Sangari 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: 11117359
    Abstract: Composite laminate parts are made using a gradient cured subset of fiber reinforced thermoset resin plies. A portion of the subset is cured to rigidity to thereby maintain the shape of a part layup, while other plies in the subset are actively cooled to prevent them from curing. Additional plies are laid up on the uncured plies of the subset to complete the layup. The completed layup is then fully cured.
    Type: Grant
    Filed: December 10, 2018
    Date of Patent: September 14, 2021
    Assignee: The Boeing Company
    Inventors: Keith Daniel Humfeld, Samra S Sangari
  • Publication number: 20190111668
    Abstract: Composite laminate parts are made using a gradient cured subset of fiber reinforced thermoset resin plies. A portion of the subset is cured to rigidity to thereby maintain the shape of a part layup, while other plies in the subset are actively cooled to prevent them from curing. Additional plies are laid up on the uncured plies of the subset to complete the layup. The completed layup is then fully cured.
    Type: Application
    Filed: December 10, 2018
    Publication date: April 18, 2019
    Inventors: Keith Daniel Humfeld, Samra S. Sangari
  • Patent number: 10201959
    Abstract: Composite laminate parts are made using a gradient cured subset of fiber reinforced thermoset resin plies. A portion of the subset is cured to rigidity to thereby maintain the shape of a part layup, while other plies in the subset are actively cooled to prevent them from curing. Additional plies are laid up on the uncured plies of the subset to complete the layup. The completed layup is then fully cured.
    Type: Grant
    Filed: January 30, 2015
    Date of Patent: February 12, 2019
    Assignee: The Boeing Company
    Inventors: Keith Daniel Humfeld, Samra S. Sangari
  • Publication number: 20160221319
    Abstract: Composite laminate parts are made using a gradient cured subset of fiber reinforced thermoset resin plies. A portion of the subset is cured to rigidity to thereby maintain the shape of a part layup, while other plies in the subset are actively cooled to prevent them from curing. Additional plies are laid up on the uncured plies of the subset to complete the layup. The completed layup is then fully cured.
    Type: Application
    Filed: January 30, 2015
    Publication date: August 4, 2016
    Inventors: Keith Daniel Humfeld, Samra S. Sangari