Patents by Inventor Teresa MARCHIONE

Teresa MARCHIONE 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: 11187414
    Abstract: A fuel nozzle for a turbomachine includes a centerbody that extends axially with respect to a centerline of the fuel nozzle. A confining tube is positioned radially outward of the centerbody. A plurality of swirler vanes is disposed between the centerbody and the confining tube. Each of the plurality of swirler vanes includes a radially inner base and a radially outer tip. Each of the swirler vanes further includes an upstream portion that extends generally axially from a leading edge. A downstream portion extends from the upstream portion to a trailing edge. The downstream portion defines a bend length between the upstream portion and the trailing edge. The bend length at the radially outer tip is greater than the bend length at the radially inner base.
    Type: Grant
    Filed: March 31, 2020
    Date of Patent: November 30, 2021
    Assignee: General Electric Company
    Inventors: Fernando Biagioli, Sebastiano Sorato, Teresa Marchione
  • Publication number: 20210302021
    Abstract: A fuel nozzle for a turbomachine includes a centerbody that extends axially with respect to a centerline of the fuel nozzle. A confining tube is positioned radially outward of the centerbody. A plurality of swirler vanes is disposed between the centerbody and the confining tube. Each of the plurality of swirler vanes includes a radially inner base and a radially outer tip. Each of the swirler vanes further includes an upstream portion that extends generally axially from a leading edge. A downstream portion extends from the upstream portion to a trailing edge. The downstream portion defines a bend length between the upstream portion and the trailing edge. The bend length at the radially outer tip is greater than the bend length at the radially inner base.
    Type: Application
    Filed: March 31, 2020
    Publication date: September 30, 2021
    Inventors: Fernando Biagioli, Sebastiano Sorato, Teresa Marchione
  • Publication number: 20160237916
    Abstract: A method of controlling the fuel distribution among different stages of a gas turbine combustion chamber is disclosed. The combustion chamber has at least two stages for fuel supply, and the fuel distribution between the stages is determined according to the load or one or more parameters indicative of the load. In reply to a fast load change being faster than a load change during a regular transient operation, the fuel distribution is determined according to an adjusted load or one or more parameters indicative of an adjusted load.
    Type: Application
    Filed: February 11, 2016
    Publication date: August 18, 2016
    Applicant: General Electric Technology GmbH
    Inventors: Theodoros FERREIRA-PROVIDAKIS, Richard Lewis Rollo SMITH, Thiemo MEEUWISSEN, Teresa MARCHIONE