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发明公开
CN109987238A 用于飞行器的组件及飞行器 审中-实审

用于飞行器的组件及飞行器
摘要：
本发明涉及针对用于飞行器的组件(1)进行的优化设计，该飞行器包括机翼(2)、发动机附接吊架(4)和装置，所述发动机附接吊架包括主结构件(28)，所述装置用于将主结构件(28)固定至翼盒(14)。这些装置包括两个侧向前部配装件(42)，这些配装件中的每一者包括：固定至前翼梁(16)的第一连接部分(46)；固定至附接吊架的主结构件(28)的第二连接部分(52)；连结第一连接部分和第二连接部分(46、52)的至少一个固定构件(54)，该固定构件(54)通过第一销系统(56)铰接至第一连接部分(46)，所述第一销系统定向为大体平行于前翼梁(16)。
摘要（英）：

The invention relates to an optimization design for an assembly (1) used for an aircraft comprising a wing (2), an engine attachment pylon (4) comprising a primary structure (28) and an arrangement for securing the primary structure (28) to a wing box (14). The arrangement comprises two lateral front fittings (42), each of these fittings comprising a first connecting portion (46) secured to the front wing spar (16), a second connecting portion (52) secured to the primary structure (28) of the attachment pylon, at least one securing member (54) linking the first and second connecting portions (46, 52), this securing member (54) being articulated to the first connecting portion (46) with the aid of a first pin system (56) oriented substantially parallel to the front wing spar (16).

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