首页> 外国专利> Controlled crumple, anti-crash composite structure for aircraft has two-layer walls of composition material, intermediate layer and corrugated core

Controlled crumple, anti-crash composite structure for aircraft has two-layer walls of composition material, intermediate layer and corrugated core

机译:用于飞机的可控的防撞,防撞复合结构,具有两层组成材料的壁,中间层和波纹状芯

摘要

The composite structure consists of transverse (18B) and lengthwise (18) walls, each comprising two layers (19) of composition material and an intermediate layer (20), with at least one of the outer layers having a corrugated inner core. The core's corrugations extend parallel to the outer layers for enhanced impact energy absorption capacity, and at least one of the outer layers has a weakened area (45) that leads to a controlled degradation of the layer in the event of an impact.
机译:该复合结构由横向壁(18B)和纵向壁(18)组成,每个壁包括两层组合材料(19)和一个中间层(20),其中至少一个外层具有波纹状的内芯。芯的波纹平行于外层延伸以增强冲击能量吸收能力,并且外层中的至少一层具有弱化区域(45),该弱化区域在发生冲击时导致层的受控降解。

著录项

  • 公开/公告号FR2896768A1

    专利类型

  • 公开/公告日2007-08-03

    原文格式PDF

  • 申请/专利权人 EUROCOPTER SOCIETE PAR ACTIONS SIMPLIFIEE;

    申请/专利号FR20060000771

  • 发明设计人 PAYEN HERVE;

    申请日2006-01-27

  • 分类号B64C1/06;B29C70/04;B29D99;B32B3/12;B32B3/28;B64C27/04;

  • 国家 FR

  • 入库时间 2022-08-21 20:26:47

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