基于关键测量特性的翼-机身对中测量辅助装配框架

Zhehan Chen, Fuzhou Du, Xiaoqing Tang, Xi Zhang
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引用次数: 18

摘要

大规模数字计量技术的广泛应用促进了飞机数字化装配技术的发展,将传统的翼机身对中工艺转变为基于测量辅助装配(MAA)的高精度、高效的数字化对中工艺。MAA是一种系统技术,它依赖于数字化测量与装配过程的集成,这不仅是操作的集成,而且是从产品设计到数字检测再到部件装配的数据融合和传播。为了指导和支持先进方法在翼机身对准MAA中的应用,提出了一种基于关键测量特性的测量辅助装配方法框架,实现了过程集成和数据融合。首先,给出了知识管理中心的定义、分类和数学模型;然后,在集成过程模型、测量数据模型和数据过程核的基础上构建了该框架。最后,以机翼机身对中仿真为例,说明了测量辅助装配技术在该框架下的应用。[2013年4月28日收到;2014年2月25日修订;接受2014年4月26日]
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A framework of measurement assisted assembly for wing-fuselage alignment based on key measurement characteristics
Wide employments of large scale digital metrologies have promoted the development of digital aircraft assembly technologies, which are changing traditional processes of wing-fuselage alignment to high precision and more efficient digital alignment based on measurement assisted assembly (MAA). MAA is a systematic technique and relies on the integration of digital measurement with assembly process, which is not only the integration of operations, but also data fusion and propagation from product design, through digital inspection to components assembly. In order to direct and support the applications of advanced approaches in MAA for wing-fuselage alignment, a novel framework of measurement assisted assembly methodology is proposed to realise the process integration and data fusion based on key measurement characteristics (KMCs). Firstly, definition, classification and mathematical model of KMCs are presented; then, the framework is constructed on the basis of integrated process model, measurement data model and data process kernel. Finally, a case of wing-fuselage alignment simulation is carried out to illuminate the application of measurement assisted assembly technique with the framework. [Received 28 April 2013; Revised 25 February 2014; Accepted 26 April 2014]
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