Patents by Inventor Yevhen Sedochenko

Yevhen Sedochenko 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).

  • UAV structural elements quick release fastening system
    Patent number: 12129057
    Abstract: The UAV structural elements' quick-release fastening system, which includes at least two tail booms coupling with a center wing section/fuselage of a UAV and a tail assembly by at least two quick-release coupling elements from the center wing's section side and at least two coupling elements from tail assembly's side, the UAV wiring elements. The docking chucks are used as the quick-release coupling elements. Coupling and fixing the tail booms with a tail assembly realized by the tail assembly docking chucks and a bayonet mount. Coupling and fixing the tail booms with a center wing section/fuselage of a UAV is realized by the center wing section docking chucks and the center wing section fixing pins or by the center wing section docking chucks and bayonet mount. The system is generally used in a UAV design with integral or dismountable tail assembly.
    Type: Grant
    Filed: March 25, 2021
    Date of Patent: October 29, 2024
    Inventors: Maksym Makarchuk, Roman Franchuk, Yevhen Sedochenko, Yevhenii Doroshenko, Hryhorii Yehoshyn, Dmytro Vrachynskyi
  • UAV STRUCTURAL ELEMENTS QUICK RELEASE FASTENING SYSTEM
    Publication number: 20230166828
    Abstract: The UAV structural elements' quick-release fastening system, which includes at least two tail booms coupling with a center wing section/fuselage of a UAV and a tail assembly by at least two quick-release coupling elements from the center wing's section side and at least two coupling elements from tail assembly's side, the UAV wiring elements. The docking chucks are used as the quick-release coupling elements. Coupling and fixing the tail booms with a tail assembly realized by the tail assembly docking chucks and a bayonet mount. Coupling and fixing the tail booms with a center wing section/fuselage of a UAV is realized by the center wing section docking chucks and the center wing section fixing pins or by the center wing section docking chucks and bayonet mount. The system is generally used in a UAV design with integral or dismountable tail assembly.
    Type: Application
    Filed: March 25, 2021
    Publication date: June 1, 2023
    Applicant: UKRSPECSYSTEMS Limited Liability Company
    Inventors: Maksym Makarchuk, Roman Franchuk, Yevhen Sedochenko, Yevhenii Doroshenko, Hryhorii Yehoshyn, Dmytro Vrachynskyi