Patents by Inventor Qiming Song

Qiming Song 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).

  • Thrust reverser assembly and method of operating
    Patent number: 11378037
    Abstract: An apparatus and method of operating a translating cowl for a turbine engine. The translating cowl is moveable between a first position and a second position. The translating cowl includes a fixed cascade element located within and a blocker door that is operably coupled to die translating cowl. Hie blocker door is movable between a stowed position and a deployed position.
    Type: Grant
    Filed: March 27, 2018
    Date of Patent: July 5, 2022
    Assignee: MRA SYSTEMS, LLC
    Inventor: Qiming Song
  • THRUST REVERSER ASSEMBLY AND METHOD OF OPERATING
    Publication number: 20210108594
    Abstract: An apparatus and method of operating a translating cowl for a turbine engine. The translating cowl is moveable between a first position and a second position. The translating cowl includes a fixed cascade element located within and a blocker door that is operably coupled to die translating cowl. Hie blocker door is movable between a stowed position and a deployed position.
    Type: Application
    Filed: March 27, 2018
    Publication date: April 15, 2021
    Inventor: Qiming Song
  • Engine door with burst seal
    Patent number: 10634060
    Abstract: A method and apparatus for a gas turbine engine including a core engine a nacelle surrounding at least a portion of the core engine and defining an interior with an opening. An access door for the opening to provide selective access to the opening where the access door provides pressure relief for the interior.
    Type: Grant
    Filed: November 20, 2016
    Date of Patent: April 28, 2020
    Assignee: MRA SYSTEMS, LLC
    Inventor: Qiming Song
  • ENGINE DOOR WITH BURST SEAL
    Publication number: 20180142624
    Abstract: A method and apparatus for a gas turbine engine including a core engine a nacelle surrounding at least a portion of the core engine and defining an interior with an opening. An access door for the opening to provide selective access to the opening where the access door provides pressure relief for the interior.
    Type: Application
    Filed: November 20, 2016
    Publication date: May 24, 2018
    Inventor: Qiming Song