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The rear part of the aircraft with a structure for supporting the engine, which is connected to the fuselage by at least one block element under compressive load

机译:飞机的后部具有用于支撑发动机的结构,该发动机的后部在压缩载荷下通过至少一个块状元件连接到机身。

摘要

A rear part of an aircraft including a support structure for supporting engines, passing through the fuselage, through first and second openings. The rear part includes a connection structure connecting the support structure to the fuselage, including a first connection mechanism connecting the support structure to a first casing forming the first opening and a second connection mechanism connecting the support structure to a second casing forming the second opening. The first and second connection mechanisms each include at least one blocking element of the support structure, under compression loading by being applied to the casing and to the support structure.
机译:飞机的后部,包括用于支撑发动机的支撑结构,该支撑结构穿过机身,穿过第一开口和第二开口。后部包括将支撑结构连接至机身的连接结构,包括第一连接机构,其将支撑结构连接至形成第一开口的第一壳体,以及第二连接机构,其将支撑结构连接至形成第二开口的第二壳体。第一连接机构和第二连接机构各自包括在施加到壳体和支撑结构上的压缩载荷下的支撑结构的至少一个阻挡元件。

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