DOUBLE-WALL TANK AND AN ASSEMBLING METHOD OF SAID DOUBLE-WALL TANK

    公开(公告)号:US20240084970A1

    公开(公告)日:2024-03-14

    申请号:US18463022

    申请日:2023-09-07

    Abstract: A double-wall tank comprising at least one piping connecting system and to a method for assembling a double-wall tank provided with at least one piping connecting system. An inner connecting part is coupled to an comprises an inner part hole. The inner part hole and an inner wall hole of the inner wall are coincident. An outer connecting part is coupled to an outer wall and comprises an outer part hole. The outer part hole and an outer wall hole of the outer wall are coincident. One or more pipes pass through the outer part hole, the outer wall hole, the inner part hole, the inner wall hole. The pipe is coupled, in a fluid-tight fit, to the inner part hole and the outer part hole.

    HYDROGEN TANK FOR AIRCRAFT
    4.
    发明申请

    公开(公告)号:US20230035247A1

    公开(公告)日:2023-02-02

    申请号:US17872702

    申请日:2022-07-25

    Abstract: A hydrogen tank for aircraft, including an inner vessel configured to contain hydrogen, first and second outer jacket domes having a semi-spherical shape and first L-shaped ends, a first cylindrical outer jacket established on top of the first and second outer jacket domes, a second cylindrical outer jacket established in the bottom of the first and second outer jacket domes. The first and second cylindrical outer jackets include second L-shaped ends. The first and second L-shaped ends form L-shaped junctions to attach the first and second outer jacket domes to the first and second cylindrical outer jackets.

    AIRCRAFT SECTION
    5.
    发明公开
    AIRCRAFT SECTION 审中-公开

    公开(公告)号:US20240343406A1

    公开(公告)日:2024-10-17

    申请号:US18637971

    申请日:2024-04-17

    CPC classification number: B64D37/04 B64C1/061

    Abstract: An aircraft section comprising a fuel storage tank, a first strap, a second strap, at least one anchoring structure and at least one coupling portion; wherein: the first strap comprises two attachment portions anchored to the at least one anchoring structure; the second strap comprises two attachment portions anchored to the at least one anchoring structure; and the first strap and the second strap are arranged under tension such that the tank is maintained pressed against the at least one coupling portion by the first strap and the second strap. Also an aircraft with such a section.

Patent Agency Ranking