Patents by Inventor Jianbo LYU

Jianbo LYU 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: 20240179246
    Abstract: A hierarchical decoupling, integrated and open communication open system includes a large communication network, a Yunxi platform, and a customer, which are communicatively connected to one another, wherein the Yunxi platform includes a service application layer, a communication capability layer and a resource pool, which are communicatively connected to one another, the large communication network, the communication capability layer and the customer are communicatively connected to one another, and the service application layer is communicatively connected to the customer. The present invention innovates decentralized communication service provision methods, further integrate communication capabilities, encapsulate communication scenarios into flexible and easy-to-use communication modules, and provide a unified and convenient service interface, thereby lowering a user-side access threshold, and deeply integrating communication capabilities with application scenarios of government and enterprise customers.
    Type: Application
    Filed: December 27, 2023
    Publication date: May 30, 2024
    Inventors: Zhaobiao LYU, Wenbo ZHAO, Jianbo LIU, Guoxin ZHANG, Chao CHENG, Junwu LI, Qing XIAO, Zhaojun CUI, Wentong LI
  • Patent number: 11028708
    Abstract: An impeller tube-type nozzle for a gas turbine, with an inlet section, a retraction section and an outlet section. The inlet section is a section of annular channel, the retraction section comprises multiple gas flow channels separated by multiple blades, each gas flow channel is encircled by an outer peripheral wall face, an inner peripheral wall face, a suction face of one of two adjacent blades and a pressure face of the other of the two adjacent blades, and inlets of the gas flow channels have a fan-shaped cross section. For each gas flow channel, along the direction of gas flow from the inlet of the gas flow channel to the outlet the fan-shaped cross section gradually smoothly transitions into a circular cross section.
    Type: Grant
    Filed: July 28, 2017
    Date of Patent: June 8, 2021
    Assignee: AECC COMMERCIAL AIRCRAFT ENGINE CO., LTD.
    Inventors: Jianbo Lyu, Hualing Luo, Shuzhen Hu, Xiande Pan, Guofeng Liu
  • Publication number: 20200149424
    Abstract: An impeller tube-type nozzle for a gas turbine, with an inlet section, a retraction section and an outlet section. The inlet section is a section of annular channel, the retraction section comprises multiple gas flow channels separated by multiple blades, each gas flow channel is encircled by an outer peripheral wall face, an inner peripheral wall face, a suction face of one of two adjacent blades and a pressure face of the other of the two adjacent blades, and inlets of the gas flow channels have a fan-shaped cross section. For each gas flow channel, along the direction of gas flow from the inlet of the gas flow channel to the outlet the fan-shaped cross section gradually smoothly transitions into a circular cross section.
    Type: Application
    Filed: July 28, 2017
    Publication date: May 14, 2020
    Applicant: AECC COMMERCIAL AIRCRAFT ENGINE CO., LTD.
    Inventors: Jianbo LYU, Hualing LUO, Shuzhen HU, Xiande PAN, Guofeng LIU