首页> 外文会议>Congress of the International Council of the Aeronautical Sciences; 20060903-08; Hamburg(DE) >OPTIMISATION OF ENERGY ABSORBING SUBSYSTEMS FOR HELICOPTER VERTICAL CRASHES
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OPTIMISATION OF ENERGY ABSORBING SUBSYSTEMS FOR HELICOPTER VERTICAL CRASHES

机译:直升机垂直碰撞能量吸收子系统的优化

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摘要

The experience gained in the last decades on the development of crashworthiness helicopter structures indicates that occupants' protection can be achieved integrating different energy absorbing systems in landing gears, subfloor and seats. However, the mutual interactions between these different subsystems must be considered to achieve higher overall performances in case of crash events. This work proposes a numerical approach for the evaluation of the overall undercarriage performance, basing on an hybrid multi-body and finite element approach. A hybrid scheme of the subfloor lay-out is integrated with a multi-body model of a crashworthy seat and an anthropomorphic dummy model. The modelling technique has been used to investigate and optimize the effects of local aspects on the overall crashworthy performances of the system such as the subfloor and the seat absorbing devices. Basing on the obtained results, the proposed methodology seems a promising approach to deal with the optimization of integrated structural systems, accounting for the mutual interactions of different subsystems, as well as multiple design and constructive constraints.
机译:过去数十年来在耐撞性直升机结构的开发上获得的经验表明,将不同的能量吸收系统集成在起落架,地板和座椅中可以实现对乘员的保护。但是,在发生碰撞事件时,必须考虑这些不同子系统之间的相互作用,以实现更高的整体性能。这项工作基于混合多体和有限元方法,提出了一种用于评估整体起落架性能的数值方法。底层布局的混合方案与防撞座椅的多体模型和拟人虚拟模型集成在一起。该建模技术已用于调查和优化局部方面对系统(如地板和座椅吸收装置)整体防撞性能的影响。根据获得的结果,所提出的方法似乎是一种有前途的方法,可以解决集成结构系统的优化问题,并考虑到不同子系统之间的相互影响以及多重设计和构造约束。

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