首页> 外国专利> Connecting rod for aircraft controls - has metal bushes bonded to conical ends of rods formed of carbon fibre embedded in synthetic resin

Connecting rod for aircraft controls - has metal bushes bonded to conical ends of rods formed of carbon fibre embedded in synthetic resin

机译:飞机控制系统的连杆-金属衬套与嵌入合成树脂中的碳纤维制成的连杆的圆锥形末端相连

摘要

The connecting rod for aircraft control systems is in the form of a tube made of carbon fibres embedded in a suitable synthetic resin. The ends of the tube are reduced in diameter to form cones with an undulating surface. As the diameter decreases the wall thickness increases in order to maintain the same number of fibres. A threaded metal bush with a flared end is bonded inside the conical end and is secured by circumferential winding of additional fibres. The fibres are enclosed in a collet which fits flush with the flange of the bush.
机译:飞机控制系统的连杆采用碳纤维管制成,该碳纤维嵌入合适的合成树脂中。管的末端直径减小以形成具有起伏表面的锥体。随着直径减小,壁厚增加,以保持相同数量的纤维。带有喇叭口的带螺纹金属衬套粘接在圆锥形端部内,并通过圆周缠绕其他纤维固定。纤维被包在夹头中,该夹头与衬套的凸缘齐平。

著录项

  • 公开/公告号FR2371598B2

    专利类型

  • 公开/公告日1982-10-29

    原文格式PDF

  • 申请/专利权人 DASSAULT BREGUET AVIATION;

    申请/专利号FR19760034912

  • 发明设计人

    申请日1976-11-19

  • 分类号F16C7/02;G05G1/00;

  • 国家 FR

  • 入库时间 2022-08-22 12:32:04

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