首页> 外国专利> The rear part of an airplane comprising a fuselage-through engine support structure connected to the fuselage by at least one connecting rod

The rear part of an airplane comprising a fuselage-through engine support structure connected to the fuselage by at least one connecting rod

机译:飞机的后部,包括通过至少一个连杆连接到机身的直通发动机支撑结构

摘要

A rear part of an aircraft including a support structure for supporting engines, extending through the fuselage, through a first opening and a second opening. A connection structure connects 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 connection structure also includes at least one effort recovery connecting rod, the first end of which is mounted on the support structure and the opposite end is mounted on the fuselage, at a distance from the first and second openings.
机译:飞机的后部,包括用于支撑发动机的支撑结构,该支撑结构延伸穿过机身,穿过第一开口和第二开口。连接结构将支撑结构连接到机身,包括将支撑结构连接到形成第一开口的第一壳体的第一连接机构和将支撑结构连接到形成第二开口的第二壳体的第二连接机构。该连接结构还包括至少一个力恢复连杆,该力恢复连杆的第一端安装在支撑结构上,而相对端安装在机身上,与第一和第二开口相距一定距离。

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