Patents by Inventor Jadeed Beita

Jadeed Beita 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).

  • Combustion system control
    Patent number: 11274610
    Abstract: A method of controlling a combustion system of a gas turbine engine which has a combustor with a primary combustion zone, of which a condition in the primary combustion zone is defined by a primary zone control parameter. The method includes controlling the primary zone control parameter to be substantially constant value over a range of values of compressor inlet air temperature.
    Type: Grant
    Filed: March 29, 2019
    Date of Patent: March 15, 2022
    Assignee: SIEMENS ENERGY GLOBAL GMBH & CO. KG
    Inventors: Jadeed Beita, Andrew Dawson
  • Controller and method
    Patent number: 11261802
    Abstract: A controller for a gas turbine is arranged to supply a load L. The gas turbine includes a fuel supply arranged to supply fuel at a fuel flow rate FF to a combustor, wherein the fuel supply includes a first fuel supply and a second fuel supply. The controller is arranged to determine one or more ratios R of one or more combustor operating parameters COP respectively at the load L to respective reference combustor operating parameters COPR at a reference load LR. The controller is further arranged to control a proportion P of the fuel flow rate FF supplied via the first fuel supply based, at least in part, on the determined one or more ratios R. A gas turbine with the controller and a method controls the gas turbine.
    Type: Grant
    Filed: September 12, 2018
    Date of Patent: March 1, 2022
    Assignee: SIEMENS ENERGY GLOBAL GMBH & CO. KG
    Inventors: Jadeed Beita, Ghenadie Bulat
  • COMBUSTION SYSTEM CONTROL
    Publication number: 20210140376
    Abstract: A method of controlling a combustion system of a gas turbine engine which has a combustor with a primary combustion zone, of which a condition in the primary combustion zone is defined by a primary zone control parameter. The method includes controlling the primary zone control parameter to be substantially constant value over a range of values of compressor inlet air temperature.
    Type: Application
    Filed: March 29, 2019
    Publication date: May 13, 2021
    Applicant: Siemens Aktiengesellschaft
    Inventors: Jadeed Beita, Andrew Dawson
  • CONTROLLER AND METHOD
    Publication number: 20210071590
    Abstract: A controller for a gas turbine is arranged to supply a load L. The gas turbine includes a fuel supply arranged to supply fuel at a fuel flow rate FF to a combustor, wherein the fuel supply includes a first fuel supply and a second fuel supply. The controller is arranged to determine one or more ratios R of one or more combustor operating parameters COP respectively at the load L to respective reference combustor operating parameters COPR at a reference load LR. The controller is further arranged to control a proportion P of the fuel flow rate FF supplied via the first fuel supply based, at least in part, on the determined one or more ratios R. A gas turbine with the controller and a method controls the gas turbine.
    Type: Application
    Filed: September 12, 2018
    Publication date: March 11, 2021
    Applicant: Siemens Aktiengesellschaft
    Inventors: Jadeed Beita, Ghenadie Bulat