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A Co-modeling Method Based on Component Features for Mechatronic Devices in Aero-engines

机译:基于机电发动机机电装置的组件特征的共造型方法

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Data-fused and user-friendly design of aero-engine accessories is required because of their structural complexity and stringent reliability. This paper gives an overview of a typical aero-engine control system and the development process of key mechatronic devices used. Several essential aspects of modeling and simulation in the process are investigated. Considering the limitations of a single theoretic model, feature-based co-modeling methodology is suggested to satisfy the design requirements and compensate for diversity of component sub-models for these devices. As an example, a stepper motor controlled Fuel Metering Unit (FMU) is modeled in view of the component physical features using two different software tools. An interface is suggested to integrate the single discipline models into the synthesized one. Performance simulation of this device using the co-model and parameter optimization for its key components are discussed. Comparison between delivery testing and the simulation shows that the co-model for the FMU has a high accuracy and the absolute superiority over a single model. Together with its compatible interface with the engine mathematical model, the feature-based co-modeling methodology is proven to be an effective technical measure in the development process of the device.
机译:由于其结构复杂性和严格的可靠性,因此需要数据融合和用户友好的航空发动机配件设计。本文概述了典型的航空发动机控制系统和所使用的关键机电装置的开发过程。研究了在该过程中建模和模拟的几个基本方面。考虑到单个理论模型的局限性,建议基于特征的共造型方法来满足设计要求,并补偿这些设备的组件子模型的多样性。例如,考虑到使用两种不同的软件工具的组件物理特征,建模步进电机控制燃料计量单元(FMU)。建议将单个学科模型集成到合成的接口。讨论了使用COM模型和参数优化的该设备的性能模拟。交付测试与仿真之间的比较表明,FMU的共模在单个型号上具有高精度和绝对优势。与其与发动机数学模型的兼容接口一起,已被证明是基于特征的共造型方法是设备开发过程中的有效技术措施。

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