The invention relates to an aircraft air inlet comprising:-a lip (44); an inner panel (48) comprising a front edge (48.1) connected to the lip (44); a front frame (50) comprising an outer edge (50.1) and an inner edge (50.2) connected to the lip (44) and/or the inner panel (48); a rear frame (52) comprising an outer edge connected directly or indirectly to the lip (44) and an inner edge (52.2) connected to the rear edge (48.2) of the inner panel (48); -at least one connecting piece (64) connecting the outer edges (50.1, 52.1) of the front frame (50) and the rear frame (52). In contrast to the prior art, the front frame (50) is not connected to the lip (44), such that the air inlet does not include any connection flush with the lip (44) in alignment with the front frame (50).

    本发明涉及一种飞行器进气口,包括:‑唇部(44);‑内面板(48),其包括连接至唇部(44)的前边缘(48.1);‑前框架(50),其包括外边缘(50.1)和连接至唇部(44)和/或内面板(48)的内边缘(50.2);‑后框架(52),其包括直接或间接地连接至唇部(44)的外边缘以及连接至内面板(48)的后边缘(48.2)的内边缘(52.2);‑至少一个连接件(64),其连接前框架(50)和后框架(52)的外边缘(50.1,52.1)。与现有技术相反,前框架(50)未连接至唇部(44),从而使得进气口在与前框架(50)对齐处不包括与唇部(44)齐平的任何连接件。


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    Titel :

    Aircraft air inlet and aircraft comprising same


    Weitere Titelangaben:

    飞行器进气口及包括其的飞行器


    Beteiligte:

    Erscheinungsdatum :

    14.02.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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