Patents by Inventor Dilip N. Shah

Dilip N. Shah 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: 11313242
    Abstract: Aspects of the disclosure are directed to a seal configured to interface with at least a first component and a second component of a gas turbine engine. A method for forming the seal includes obtaining an ingot of a fine grained, or a coarse grained, or a columnar grained or a single crystal material from a precipitation hardened nickel base superalloy containing at least 40% by volume of the precipitate of the form Ni3(Al, X), where X is a metallic or refractory element, and processing the ingot to generate a sheet of the material, where the sheet has a thickness within a range of 0.010 inches and 0.050 inches inclusive.
    Type: Grant
    Filed: September 18, 2019
    Date of Patent: April 26, 2022
    Assignee: Raytheon Technologies Corporation
    Inventors: Alan D. Cetel, Dilip N. Shah, Eric A. Hudson, Raymond Surace
  • Publication number: 20200141255
    Abstract: Aspects of the disclosure are directed to a seal configured to interface with at least a first component and a second component of a gas turbine engine. A method for forming the seal includes obtaining an ingot of a fine grained, or a coarse grained, or a columnar grained or a single crystal material from a precipitation hardened nickel base superalloy containing at least 40% by volume of the precipitate of the form Ni3(Al, X), where X is a metallic or refractory element, and processing the ingot to generate a sheet of the material, where the sheet has a thickness within a range of 0.010 inches and 0.050 inches inclusive.
    Type: Application
    Filed: September 18, 2019
    Publication date: May 7, 2020
    Inventors: Alan D. Cetel, Dilip N. Shah, Eric A. Hudson, Raymond Surace
  • Patent number: 6637500
    Abstract: Concepts for fabricating improved cores for investment casting are described. The cores are composite which include refractory metal elements and ceramic elements. The refractory metal elements are provided to enhance the mechanical properties of the core and/or to permit the fabrication of cores having shapes and geometries that could not otherwise be achieved. In one embodiment, the entire core may be made of refractory metal components. The cores may be used to investment cast gas turbine superalloy components.
    Type: Grant
    Filed: October 24, 2001
    Date of Patent: October 28, 2003
    Assignee: United Technologies Corporation
    Inventors: Dilip N. Shah, James Thompson Beals, John Joseph Marcin, Jr., Stephen Douglas Murray
  • Patent number: 5232996
    Abstract: A two-part adhesive composition useful for bonding various materials including plastic or thermoplastic substrates. The first part of the adhesive contains an epoxy compound and an acrylate-terminated polyurethane while the second part of the adhesive contains an amine hardener. The presence of the acrylate-terminated polyurethane allows the adhesive composition to be applied to unprepared substrates to form a bond having high strength.
    Type: Grant
    Filed: May 7, 1992
    Date of Patent: August 3, 1993
    Assignee: Lord Corporation
    Inventors: Dilip N. Shah, Terrance H. Dawdy