AIRCRAFT WITH SUSPENDED HYDROGEN TANK
    1.
    发明公开

    公开(公告)号:US20240116650A1

    公开(公告)日:2024-04-11

    申请号:US18480080

    申请日:2023-10-03

    Applicant: Airbus SAS

    CPC classification number: B64D37/30 B64D37/06

    Abstract: An aircraft, including a hydrogen consumer and a hydrogen supply device for supplying the hydrogen consumer with hydrogen, the hydrogen supply device having a cryogenic hydrogen tank for storing liquid hydrogen. In order to lower the weight while improving performance of the hydrogen tank during different flight conditions, embodiments of the aircraft further include a suspension arrangement with suspension elements for suspending the hydrogen tank on a structure of the aircraft, wherein the hydrogen tank includes a tank wall made from fiber reinforced composite material, and wherein the suspension arrangement includes a plurality of first tensile loaded dry fiber suspension elements fixed to load introduction areas on the hydrogen tank such that the suspension elements extend essentially tangential to a surface of the hydrogen tank at the associated load introduction area.

    HYDROGEN TANK ASSEMBLY FOR A VEHICLE, SUCH AS AN AIRCRAFT

    公开(公告)号:US20230027471A1

    公开(公告)日:2023-01-26

    申请号:US17856327

    申请日:2022-07-01

    Applicant: Airbus SAS

    Abstract: A hydrogen tank assembly is provided for use in vehicles, such as aircraft. The hydrogen tank assembly has an inner tank wall, an outer tank wall, and an inert gas source. The inner tank wall defines a hydrogen tank volume that is surrounded by a shroud volume which is defined by the outer tank wall. The hydrogen tank volume is filled with cryogenic hydrogen and has a higher pressure than the shroud volume that is filled with an inert gas, such as helium. The counter-pressure of the inert gas prevents micro-cracks in the inner tank wall and increases the in-service life.

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