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    AIRCRAFT WITH AIRCRAFT SECTION
    95.
    发明公开
    AIRCRAFT WITH AIRCRAFT SECTION 审中-公开

    公开(公告)号：US20240351676A1

    公开(公告)日：2024-10-24

    申请号：US18421130

    申请日：2024-01-24

    申请人： Airbus Operations GmbH

    发明人： Carsten PAUL ,  Cord HAACK ,  Sergej KAUFMANN

    IPC分类号： B64C1/06 ,  B64D37/04 ,  B64D37/30

    CPC分类号： B64C1/069 ,  B64D37/04 ,  B64D37/30

    摘要： An aircraft section for aircraft. The aircraft section comprises at least one flight component, such as a wing assembly and a tail assembly, and a first fuselage component. The flight component is mounted on the first fuselage component. The first fuselage component has a first coupling point designed for releasable connection to a second coupling point on a second fuselage component, in order to form an integrated fuselage of an aircraft when in a coupled state. The first coupling point provides a mechanical coupling with a second coupling point, forms a system infrastructure interface, and provides a data transmission device for integrity checking when the aircraft section is coupled to another aircraft section. The first coupling point likewise provides positioning sensors for guided docking of the aircraft section with another aircraft section in a target position.

    HYDROGEN AIRCRAFT
    96.
    发明公开
    HYDROGEN AIRCRAFT 审中-公开

    公开(公告)号：US20240270401A1

    公开(公告)日：2024-08-15

    申请号：US18645409

    申请日：2024-04-25

    申请人： KAWASAKI JUKOGYO KABUSHIKI KAISHA

    发明人： Yoshitaka KONDO ,  Takahiro TOYODA ,  Takeshi NAKAGAWA ,  Kenta KUMADA ,  Yosuke UENO ,  Kazuki NOMURA

    IPC分类号： B64D37/30 ,  B64C1/10 ,  B64D37/04

    CPC分类号： B64D37/30 ,  B64D37/04 ,  B64C1/10

    摘要： A hydrogen aircraft includes: an airframe including a fuselage and a wing; at least one propulsion system fixed to the airframe; a pressurized chamber disposed inside the fuselage; a pressure bulkhead that is disposed at a rear part of the pressurized chamber and has strength to withstand pressurization of the pressurized chamber; a hydrogen tank that is disposed in an accommodation section and stores liquid hydrogen, the accommodation section being installed behind the pressure bulkhead, outside the pressurized chamber, and inside the fuselage; and a supply line that supplies the liquid hydrogen stored in the hydrogen tank to the propulsion system.

    AIRCRAFT COMPRISING A STRUCTURE, A TANK AND MEANS FOR FASTENING THE TANK TO THE STRUCTURE
    98.
    发明公开
    AIRCRAFT COMPRISING A STRUCTURE, A TANK AND MEANS FOR FASTENING THE TANK TO THE STRUCTURE 审中-公开

    公开(公告)号：US20240116648A1

    公开(公告)日：2024-04-11

    申请号：US18363426

    申请日：2023-08-01

    申请人： Airbus Operations SAS

    发明人： Anthony MERTES

    IPC分类号： B64D37/04

    CPC分类号： B64D37/04

    摘要： An aircraft comprising a structure, a tank housed in the fuselage, and fastening means which comprise a front fastening system, a rear fastening system and a lateral fastening system. The front system comprises a front plate, two lateral connecting rods and a central connecting rod that are fastened between the front plate and the tank. The rear system comprises a rear plate and a rear connecting rod fastened between the rear plate and the tank. The lateral system comprises a lateral connecting rod fastened between the structure and the tank, wherein one of the connection points is behind the other connection point.