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Integration strategy of on-machine measurement (OMM) and numerical control (NC) machining for the large thin-walled parts with surface correlative constraint

机译:具有表面相关约束的大型薄壁零件的机上测量(OMM)和数控(NC)加工的集成策略

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摘要

There is a kind of large thin-walled parts in aerospace industry, the machining target surface of which is tightly associated with another specific surface (named correlative surface). And it is always the primary machining objective. However, the preformed correlative surface is significantly different from its original design model due to large profile and thickness errors. Thus, part-referenced machining is necessary to ensure the correlative constraint accuracy. In this article, an integration strategy of OMM and NC machining for the large thin-walled parts with surface correlative constraint is systematically developed. Generally, the integration process consists of correlative constraint analysis, on-machine measurement, machining target surface redesign, and NC machining. Firstly, an isoplanar-based on-machine scanning method is presented for large surface profile information extraction. Then, a unified target surface redesign model is established according to surfaces accompanying relation analysis. Further, to compensate stress-induced monotonic structural deformation, a partitioned measuring and machining approach has been employed. Finally, the liquid rocket engine nozzle as a typical part was employed to verify the validation of the proposed strategy. Coolant channel machining experiments were conducted on a special dual-spindle machine tools. For a nozzle with machining area about 8 m(2), the correlative accuracy could be controlled in the range of +/- 0.1 mm. It has been proved that incorporating dimensional metrology feedback to machining process could consistently improve machining quality and efficiency of large thin-walled parts.
机译:航空工业中有一种大型的薄壁零件,其加工目标表面与另一个特定表面(称为相关表面)紧密相关。它始终是主要的加工目标。然而,由于较大的轮廓和厚度误差,预先形成的相关表面与其原始设计模型明显不同。因此,必须进行零件参照加工以确保相关约束精度。本文系统地开发了具有表面相关约束的大型薄壁零件的OMM和NC加工的集成策略。通常,集成过程包括相关约束分析,在机测量,加工目标表面重新设计和NC加工。首先,提出了一种基于等平面的在线扫描方法,用于大表面轮廓信息的提取。然后,根据伴随关系分析的曲面,建立统一的目标曲面重新设计模型。此外,为了补偿应力引起的单调结构变形,已采用了分区的测量和加工方法。最后,采用液体火箭发动机喷嘴作为典型部件来验证所提出策略的有效性。在特殊的双主轴机床上进行了冷却液通道加工实验。对于加工面积约为8 m(2)的喷嘴,相关精度可以控制在+/- 0.1 mm的范围内。事实证明,将尺寸计量反馈应用于加工过程可以持续提高大型薄壁零件的加工质量和效率。

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