The invention relates to an aircraft comprising: a fuselage (32); -a wing (34); -at least one turbine (40) operating with hydrogen and generating thrust at a thruster assembly (36) separate from the fuselage (32); -at least one fuel container (46) positioned in the fuselage (32) and configured to store hydrogen in a cryogenic state; -at least one hydrogen supply connecting the fuel container (46) and the turbine (40), the at least one hydrogen supply comprising: o at least one pump (50) positioned in the fuselage (32) near the fuel container (46); and o at least one hydrogen heating system (52) positioned in the fuselage (32) proximate the pump (50). This solution allows for a reduction in the length of complex double-layer conduits configured to direct hydrogen in a cryogenic state between the fuel container and the hydrogen heating system.

    本发明涉及一种飞行器,包括:‑机身(32);‑机翼(34);‑至少一个涡轮机(40),其以氢运行并在与机身(32)分离的推进器组件(36)处产生推力;‑至少一个燃料容器(46),其定位于机身(32)中并构造成以低温状态储存氢;‑至少一个氢供应装置,其连接燃料容器(46)和涡轮机(40),至少一个氢供应装置包括:o至少一个泵(50),其在靠近燃料容器(46)处定位于机身(32)中;以及o至少一个氢加热系统(52),其在靠近泵(50)处定位于机身(32)中。这种解决方案允许减少复杂的双层导管的长度,这些导管被构造为能够在燃料容器和氢加热系统之间引导处于低温状态的氢。


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    Titel :

    Aircraft comprising hydrogen supply device integrated with hydrogen heating system positioned in fuselage of aircraft


    Weitere Titelangaben:

    包括集成定位于飞行器的机身中的氢加热系统的氢供应装置的飞行器


    Beteiligte:
    CHAPRA LAKSHMI (Autor:in) / ABERAI AMIR (Autor:in) / TIBELL BRIAN (Autor:in) / PISAVAN ANDREI (Autor:in) / VERMA ALOK (Autor:in) / FORBES ANDREW (Autor:in) / CARRETERO BENIGNOS JUAN ANTONIO (Autor:in) / BAMMER BERND (Autor:in)

    Erscheinungsdatum :

    2023-02-17


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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