Patents by Inventor NILESHPURI GOSWAMI

NILESHPURI GOSWAMI 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).

  • System and method for preventing icing in the combustion inlet air path of a gas turbine system
    Patent number: 11846231
    Abstract: A system and method for preventing icing in the combustion inlet air path of a gas turbine system. An air intake system of the gas turbine system supplies intake air to a gas turbine engine. The air intake system includes an air filter inlet house to filter the intake air. The air filter inlet house includes at least one filter stage having an array of pulse filters, with each of the pulse filters being hydrophobic. A combustion inlet air path is in fluid communication with the air intake system and the gas turbine engine. The combustion inlet air path receives the filtered air from the air filter inlet house and supplies the filtered air as combustion inlet air to an inlet of the gas turbine engine. A surface of at least one component in the combustion inlet air path includes an anti-icing coating to prevent ice from forming thereon.
    Type: Grant
    Filed: December 23, 2021
    Date of Patent: December 19, 2023
    Assignee: GENERAL ELECTRIC COMPANY
    Inventors: William Stanley Adams, Victor Alfonso Gonzalez Tellez, Jametra Stitt, Nileshpuri Goswami
  • SYSTEM AND METHOD FOR PREVENTING ICING IN THE COMBUSTION INLET AIR PATH OF A GAS TURBINE SYSTEM
    Publication number: 20230203990
    Abstract: A system and method for preventing icing in the combustion inlet air path of a gas turbine system. An air intake system of the gas turbine system supplies intake air to a gas turbine engine. The air intake system includes an air filter inlet house to filter the intake air. The air filter inlet house includes at least one filter stage having an array of pulse filters, with each of the pulse filters being hydrophobic. A combustion inlet air path is in fluid communication with the air intake system and the gas turbine engine. The combustion inlet air path receives the filtered air from the air filter inlet house and supplies the filtered air as combustion inlet air to an inlet of the gas turbine engine. A surface of at least one component in the combustion inlet air path includes an anti-icing coating to prevent ice from forming thereon.
    Type: Application
    Filed: December 23, 2021
    Publication date: June 29, 2023
    Applicant: GENERAL ELECTRIC COMPANY
    Inventors: WILLIAM STANLEY ADAMS, VICTOR ALFONSO GONZALEZ TELLEZ, JAMETRA STITT, NILESHPURI GOSWAMI