首页> 外国专利> PRIMARY STRUCTURE OF A STRUT FOR BEARING AN AIRCRAFT POWER PLANT, THE REAR PART OF WHICH IS FORMED BY A SET OF CONNECTING RODS

PRIMARY STRUCTURE OF A STRUT FOR BEARING AN AIRCRAFT POWER PLANT, THE REAR PART OF WHICH IS FORMED BY A SET OF CONNECTING RODS

机译:用于承托飞机电站的支柱的主要结构,其后部由一组连接杆组成

摘要

A primary structure of a strut for bearing an aircraft power plant including a front part intended to be joined to an aircraft power plant and a rear part intended to be joined to a structure of the aircraft, the front part being formed from a box including an upper longitudinal member, a lower longitudinal member, and lateral panels. A main rib is located at an interface between the front part and the rear part. The rear part is formed from a set of four connecting rods. The first end of each connecting rod is joined to the front part of the primary structure and the second end of each connecting rod is joined to a separate interface for fastening to the structure of the aircraft. This allows a substantial simplification of the primary structure of a strut for bearing an aircraft power plant, which can have advantages in particular in terms of cost, mass, and simplicity of implementation and integration.
机译:用于承载飞机动力装置的支柱的主要结构,其包括打算与飞机动力装置连接的前部和打算与飞机结构连接的后部,该前部由包括一个箱的箱形成。上部纵向构件,下部纵向构件和侧板。主肋位于前部和后部之间的界面处。后部由一组四个连杆组成。每个连杆的第一端连接到主要结构的前部,每个连杆的第二端连接到单独的接口,用于固定到飞机的结构。这允许大大简化用于支承飞机动力装置的支柱的主要结构,这尤其在成本,质量以及实施和集成的简便性方面可以具有优点。

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