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EC135 PITCH HORN IN INFUSION TECHNOLOGY

机译:EC135音调技术

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In current dynamic parts on rotorcrafts, such as blades, the prepreg technology has been the primary selected method as the process can be controlled via incoming inspections (material properties) and the complete manufacturing process is easy to be followed via Quality Assurance (QA). To increase the in house created value and process quality validation, a LCM process for a critical part, the pitch horn of the EC135 main rotor blade, has been investigated via the research project PreCarBi and finally serialized. During the serialisation phase, as a prerequisite, the primary functions (transfer of loads and stiffness) of the pitch horn have to be maintained and all the attachment/junction areas must be mirrored to the existing prepreg part. Finally, all the qualification steps of part and materials, as well as the whole new process have to be performed. And in a serialisation phase the stability proven and the process implemented.
机译:在旋翼飞机上当前的动态零件(例如叶片)中,预浸料技术已成为首选方法,因为可以通过进货检验(材料特性)控制过程,并且可以通过质量保证(QA)轻松地跟踪整个制造过程。为了增加内部创造的价值和过程质量验证,通过研究项目PreCarBi对关键部分的LCM工艺(EC135主旋翼桨叶的变桨角)进行了研究,并最终进行了序列化。在序列化阶段,作为先决条件,必须保持变角器的主要功能(载荷传递和刚度),并且所有附接/接合区域都必须镜像到现有的预浸料零件。最后,必须执行零件和材料的所有鉴定步骤以及整个新过程。并在序列化阶段证明了稳定性并执行了过程。

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