Patents by Inventor Jahanzeb Tareen

Jahanzeb Tareen 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: 11820500
    Abstract: A method of curing an aircraft component including applying a temperature sensitive adhesive to a surface of a component, the surface having a contour; positioning a heating tool including a manifold with a ventilation path such that the ventilation path is adjacent to the surface by aligning the ventilation path to the contour of the component; and heating the surface of the component with uniform airflow from the ventilation path; wherein the manifold includes a chamber with a diverging portion configured to provide uniform airflow through the ventilation path to provide heating to the surface.
    Type: Grant
    Filed: October 11, 2021
    Date of Patent: November 21, 2023
    Assignee: Textron Innovations Inc.
    Inventors: Tom S. Chiang, Bruce B. Bacon, Frank S. Allen, Jahanzeb Tareen, Christopher L. Gravelle
  • Publication number: 20220024081
    Abstract: A method of curing an aircraft component including applying a temperature sensitive adhesive to a surface of a component, the surface having a contour; positioning a heating tool including a manifold with a ventilation path such that the ventilation path is adjacent to the surface by aligning the ventilation path to the contour of the component; and heating the surface of the component with uniform airflow from the ventilation path; wherein the manifold includes a chamber with a diverging portion configured to provide uniform airflow through the ventilation path to provide heating to the surface.
    Type: Application
    Filed: October 11, 2021
    Publication date: January 27, 2022
    Applicant: Bell Textron Inc.
    Inventors: Tom S. Chiang, Bruce B. Bacon, Frank S. Allen, Jahanzeb Tareen, Christopher L. Gravelle
  • Patent number: 11142297
    Abstract: In one aspect, a heating tool includes a heat source having a discharge outlet; and a manifold including an intake conduit configured to releasably connect to the discharge outlet of the heat source and a chamber coupled to the intake conduit having a ventilation path. The chamber includes a diverging portion configured to provide uniform airflow through the ventilation path to provide heating to a surface. In an embodiment, the chamber has a first portion and a second portion configured for assembly and disassembly. A method of curing an aircraft component is provided.
    Type: Grant
    Filed: February 3, 2017
    Date of Patent: October 12, 2021
    Assignee: Bell Helicopter Textron Inc.
    Inventors: Tom S. Chiang, Bruce B. Bacon, Frank S. Allen, Jahanzeb Tareen, Christopher L. Gravelle
  • Publication number: 20170225366
    Abstract: In one aspect, a heating tool includes a heat source having a discharge outlet; and a manifold including an intake conduit configured to releasably connect to the discharge outlet of the heat source and a chamber coupled to the intake conduit having a ventilation path. The chamber includes a diverging portion configured to provide uniform airflow through the ventilation path to provide heating to a surface. In an embodiment, the chamber has a first portion and a second portion configured for assembly and disassembly. A method of curing an aircraft component is provided.
    Type: Application
    Filed: February 3, 2017
    Publication date: August 10, 2017
    Applicant: Bell Helicopter Textron Inc.
    Inventors: Tom S. Chiang, Bruce B. Bacon, Frank S. Allen, Jahanzeb Tareen, Christopher L. Gravelle