Patents by Inventor Jifei YE

Jifei YE 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: 12258150
    Abstract: The present disclosure belongs to the technical field of space satellite propulsion, and particularly relates to a digital filter based method for measuring thrust response time of a satellite-borne micro-thruster.
    Type: Grant
    Filed: October 12, 2022
    Date of Patent: March 25, 2025
    Assignee: Aerospace Engineering University of the People's Liberation Army (PLA) Strategic Support Force
    Inventors: Yanji Hong, Xiaohui Feng, Xing Jin, Jifei Ye, Haichao Cui, Gaoping Feng
  • Patent number: 11925956
    Abstract: Provided is a preparation method for a double-layer working medium target tape with a plasma-enhanced interfacial bonding force for a micro laser thruster. Aiming at the problem that in an existing micro laser thruster, when a working medium is ablated by a laser beam, due to a weak interlayer interfacial bonding force between a transparent film substrate and the coating working medium, sputtering or bulging occurs, which remarkably reduces propulsive performance, a method for treating a surface of a transparent film substrate with a low-temperature plasma is used to increase surface energy of a film and an adhesive force of a working medium layer on a surface of the film, thereby enhancing the interlayer interfacial bonding force. According to the method in the present disclosure, the transparent film substrate is treated with the low-temperature plasma.
    Type: Grant
    Filed: October 12, 2022
    Date of Patent: March 12, 2024
    Assignee: Space Engineering University
    Inventors: Jifei Ye, Baoyu Xing, Yanji Hong, Sibo Wang, Nanlei Li
  • Publication number: 20240033778
    Abstract: Provided is a preparation method for a double-layer working medium target tape with a plasma-enhanced interfacial bonding force for a micro laser thruster. Aiming at the problem that in an existing micro laser thruster, when a working medium is ablated by a laser beam, due to a weak interlayer interfacial bonding force between a transparent film substrate and the coating working medium, sputtering or bulging occurs, which remarkably reduces propulsive performance, a method for treating a surface of a transparent film substrate with a low-temperature plasma is used to increase surface energy of a film and an adhesive force of a working medium layer on a surface of the film, thereby enhancing the interlayer interfacial bonding force. According to the method in the present disclosure, the transparent film substrate is treated with the low-temperature plasma.
    Type: Application
    Filed: October 12, 2022
    Publication date: February 1, 2024
    Inventors: Jifei YE, Baoyu XING, Yanji HONG, Sibo WANG, Nanlei LI
  • Publication number: 20230150696
    Abstract: The present disclosure belongs to the technical field of space satellite propulsion, and particularly relates to a digital filter based method for measuring thrust response time of a satellite-borne micro-thruster.
    Type: Application
    Filed: October 12, 2022
    Publication date: May 18, 2023
    Inventors: Yanji HONG, Xiaohui FENG, Xing JIN, Jifei YE, Haichao CUI, Gaoping FENG