Patents by Inventor Naveena K P

Naveena K P 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).

  • Publication number: 20240352865
    Abstract: Clearance control systems with thermal actuators are disclosed. An example thermally-actuated clearance control system for a gas turbine engine includes a compliant material; a high-conductive material coupled to a first surface of the compliant material, the high-conductive material thermally coupling the compliant material to a heated substance, the compliant material to expand radially-inward toward a fan blade when the high-conductive material provides heat; and an abradable material coupled to a second surface of the compliant material facing the fan blade.
    Type: Application
    Filed: July 1, 2024
    Publication date: October 24, 2024
    Inventors: Naveena K.P., Ravindra Shankar Ganiger, Kishore Budumuru, Kudum Shinde
  • Patent number: 12025011
    Abstract: Clearance control systems with thermal actuators are disclosed. An example thermally-actuated clearance control system for a gas turbine engine includes a compliant material; a high-conductive material coupled to a first surface of the compliant material, the high-conductive material thermally coupling the compliant material to a heated substance, the compliant material to expand radially-inward toward a fan blade when the high-conductive material provides heat; and an abradable material coupled to a second surface of the compliant material facing the fan blade.
    Type: Grant
    Filed: January 3, 2023
    Date of Patent: July 2, 2024
    Assignee: General Electric Company
    Inventors: Naveena K. P., Ravindra Shankar Ganiger, Kishore Budumuru, Kudum Shinde
  • Publication number: 20240167392
    Abstract: Clearance control systems with thermal actuators are disclosed. An example thermally-actuated clearance control system for a gas turbine engine includes a compliant material; a high-conductive material coupled to a first surface of the compliant material, the high-conductive material thermally coupling the compliant material to a heated substance, the compliant material to expand radially-inward toward a fan blade when the high-conductive material provides heat; and an abradable material coupled to a second surface of the compliant material facing the fan blade.
    Type: Application
    Filed: January 3, 2023
    Publication date: May 23, 2024
    Inventors: Naveena K.P., Ravindra Shankar Ganiger, Kishore Budumuru, Kudum Shinde
  • Patent number: 11808157
    Abstract: Disclosed herein are example variable flowpath casings for blade tip clearance control. An example casing for a turbine engine includes an annular substrate extending along an axial direction, the annular substrate defining a cavity at a radially inward surface of the annular substrate, and a smart structure coupled to the annular substrate, the smart structure including a support structure; an actuator structure to at least one of expand or contract in response to a change in temperature of the actuator structure, and a variable surface coupled to the support structure, the support structure to move the variable surface in a radial direction.
    Type: Grant
    Filed: August 30, 2022
    Date of Patent: November 7, 2023
    Assignee: General Electric Company
    Inventors: Naveena K P, Ravindra Shankar Ganiger, Domala Uma Maheshwar, Kishore Budumuru, Kudum Shinde, Abhishek Goverdhan