Patents by Inventor Zhiqiang Meng

Zhiqiang Meng 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: 11698320
    Abstract: A rotor balancing method for a gas turbine on a balancing machine, includes performing a base run by running the rotor at an intended balance speed and measuring the vibrations at a first pedestal; carrying out partial balancing; performing a first influence run by fitting a first balancing weight to a first correction plane in order to reduce vibrations at the first pedestal; performing a second influence run by fitting a first calibration weight to a second correction plane, running the rotor at the intended balance speed and measuring the vibrations at the first pedestal and the second pedestal, and removing the first calibration weight; and carrying out final balancing of the rotor by fitting a final balancing weight to the first correction plane and a second balancing weight to the second correction plane dependent on vibrations measured as part of the first influence run and the second influence run.
    Type: Grant
    Filed: April 18, 2019
    Date of Patent: July 11, 2023
    Assignee: Siemens Energy Global GmbH & Co. KG
    Inventor: Zhiqiang Meng
  • Patent number: 11499428
    Abstract: A rotor balancing method for a gas turbine having a rotor with a first correction plane and a second correction plane, wherein a first balancing weight is attached to the first correction plane. The method includes performing a first influence run wherein first balancing weight remains fitted for the subsequent second influence run; fitting a first calibration weight to the second correction plane using a reference influence vector; performing a second influence run; removing the first calibration weight from the rotor and calculating an influence vector of the second correction plane using a first set of vibration measurements and a second set of vibration measurements taken during the first influence run and the second influence run, respectively; and carrying out balancing of the rotor by fitting a final balancing weight to the first correction plane and a second balancing weight to the second correction plane using the calculated influence vectors.
    Type: Grant
    Filed: April 18, 2019
    Date of Patent: November 15, 2022
    Assignee: Siemens Energy Global GmbH & Co. KG
    Inventor: Zhiqiang Meng
  • Publication number: 20210372283
    Abstract: A rotor balancing method for a gas turbine having a rotor with a first correction plane and a second correction plane, wherein a first balancing weight is attached to the first correction plane. The method includes performing a first influence run wherein first balancing weight remains fitted for the subsequent second influence run; fitting a first calibration weight to the second correction plane using a reference influence vector; performing a second influence run; removing the first calibration weight from the rotor and calculating an influence vector of the second correction plane using a first set of vibration measurements and a second set of vibration measurements taken during the first influence run and the second influence run, respectively; and carrying out balancing of the rotor by fitting a final balancing weight to the first correction plane and a second balancing weight to the second correction plane using the calculated influence vectors.
    Type: Application
    Filed: April 18, 2019
    Publication date: December 2, 2021
    Applicant: Siemens Energy Global GmbH & Co. KG
    Inventor: Zhiqiang Meng
  • Publication number: 20210156757
    Abstract: A rotor balancing method for a gas turbine on a balancing machine, includes performing a base run by running the rotor at an intended balance speed and measuring the vibrations at a first pedestal; carrying out partial balancing; performing a first influence run by fitting a first balancing weight to a first correction plane in order to reduce vibrations at the first pedestal; performing a second influence run by fitting a first calibration weight to a second correction plane, running the rotor at the intended balance speed and measuring the vibrations at the first pedestal and the second pedestal, and removing the first calibration weight; and carrying out final balancing of the rotor by fitting a final balancing weight to the first correction plane and a second balancing weight to the second correction plane dependent on vibrations measured as part of the first influence run and the second influence run.
    Type: Application
    Filed: April 18, 2019
    Publication date: May 27, 2021
    Applicant: Siemens Gas and Power GmbH & Co. KG
    Inventor: Zhiqiang Meng
  • Patent number: 10961852
    Abstract: A method for low-speed balancing of a rotor having at least one compressor stage blades assembly includes a row of blades circumferentially arranged with circumferential clearance. Two or more blades are located blades, each having an angular position in the assembly, at which the located blades are maintained. The located blades define sectors. Each sector includes movable blades and sectoral circumferential clearances. The movable blades, for each sector, are circumferentially adjusted such that the sectoral circumferential clearance of the sector moves circumferentially downstream relative to the movable blades with respect to a rotational direction when the assembly is rotated. Relative position of the sectoral circumferential clearances and the movable blades within each sector is maintained by inserts. A measure of unbalance is determined for the rotor in low-speed balancing conditions.
    Type: Grant
    Filed: September 4, 2017
    Date of Patent: March 30, 2021
    Assignee: SIEMENS ENERGY GLOBAL GMBH & CO. KG
    Inventor: Zhiqiang Meng
  • Publication number: 20190211682
    Abstract: A method for low-speed balancing of a rotor having at least one compressor stage blades assembly includes a row of blades circumferentially arranged with circumferential clearance. Two or more blades are located blades, each having an angular position in the assembly, at which the located blades are maintained. The located blades define sectors. Each sector includes movable blades and sectoral circumferential clearances. The movable blades, for each sector, are circumferentially adjusted such that the sectoral circumferential clearance of the sector moves circumferentially downstream relative to the movable blades with respect to a rotational direction when the assembly is rotated. Relative position of the sectoral circumferential clearances and the movable blades within each sector is maintained by inserts. A measure of unbalance is determined for the rotor in low-speed balancing conditions.
    Type: Application
    Filed: September 4, 2017
    Publication date: July 11, 2019
    Applicant: Siemens Aktiengesellschaft
    Inventor: Zhiqiang Meng