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Model of multidisciplinary simulation integration in helicopter rotor blade design process

机译:直升机旋翼设计过程中的多学科仿真集成模型

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摘要

The design of the helicopter rotor blade is subjected to several discipline influence during the design process that cause substantial changes in its structure properties and dynamical properties. Therefore, it is important to consider different discipline tool effects on the helicopter rotor blade design process. In this article, a model of multidisciplinary simulation integration (MSI) is established and used to solve the problem of process integration and resources share of different discipline tools in the rotor blade design process. First, the numerical process of rotor blade design is analysed and a flow framework model of two-level flows and a group of nodes is proposed to integrate different discipline tools in the rotor blade design process to act as an integration mechanism. Then, some key enabling technologies of MSI are discussed by analysing integration relations of different discipline tools. Integrated work model of different type of discipline tools is given to realise the proposed flow framework. In the end, the model of MSI is realised based on Visual C++ 6.0, OpenGL and SQL SERVER database. Examples show that the proposed flow framework and the established model are satisfied for improving design efficiency and sharing simulation resources in the rotor blade design process.
机译:直升机旋翼桨叶的设计在设计过程中会受到多种学科的影响,从而导致其结构特性和动力学特性发生重大变化。因此,重要的是要考虑到直升机旋翼桨叶设计过程中不同学科工具的影响。本文建立了一个多学科仿真集成模型(MSI),用于解决转子叶片设计过程中过程集成和不同学科工具资源共享的问题。首先,分析了转子叶片设计的数值过程,提出了两级流动和一组节点的流动框架模型,以在转子叶片设计过程中整合不同的学科工具,作为一种集成机制。然后,通过分析不同学科工具的集成关系,讨论了MSI的一些关键实现技术。给出了不同类型学科工具的集成工作模型,以实现所提出的流程框架。最后,基于Visual C ++ 6.0,OpenGL和SQL SERVER数据库实现了MSI模型。实例表明,所提出的流框架和所建立的模型能够满足提高转子叶片设计过程中设计效率和共享仿真资源的要求。

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