一种密封件(1),其被配置为在组装配置中插置于推进组件的第一元件与第二元件之间;密封件(1)具有节段(1A),所述节段具有在密封件(1)的长度的至少一部分上延伸的不规则加强件,并且所述节段具有轮廓,所述轮廓包括第一轮廓部分(10)和第二轮廓部分(20),第一轮廓部分设置有第一加强部分(11),在第二轮廓部分中不存在所述第一加强部分(11),使得:与第一轮廓部分(10)相比,第二轮廓部分(20)具有增加的屈曲敏感性。

    Seal (1) configured to be interposed between a first and a second element of a propulsion assembly, wherein, in an assembled configuration, the seal (1) has a portion (1A) with non-homogeneous reinforcement which extends over at least part of the length of the seal (1) and which has a contour which comprises a first contour part (10) provided with a first reinforcing part (11), and a second contour part (20) in which the first reinforcing part (11) is absent, with the result that the second contour part (20) has an increased liability to buckle in relation to the first contour part (10).


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    Titel :

    推进组件的密封件


    Erscheinungsdatum :

    2024-07-05


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    F16J Kolben , PISTONS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT