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A KBE Application for Automatic Aircraft Wire Harness Routing

机译:KBE在飞机自动线束布线中的应用

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摘要

Wire harness design is an increasingly complex task. Knowledge Based Engineering (KBE) and optimization techniques can be used to support designers in handling this complexity. The wire harness design process can be divided in three main parts, namely electrical design, configuration design and geometrical routing. This paper describes the latest progress in the development of a KBE application aiming at the automation of the routing phase. Discrete optimization techniques are used to design shortest path harnesses, while complying with different type of constraints. Some preliminary results have been presented in a previous paper, where only geometrical constraints were addressed. However, wire harness design is affected also by other types of rules and constraints, which need to be accounted to obtain more realistic design results from the optimization process. This paper describes some new developments in the routing application to account for the presence of critical zones inside the aircraft. As study case, the presence of heat sources inside the airframe is considered, which either force the harness to be routed elsewhere, or require the use of wire protections, with obvious consequences on weight and manufacturing. First, some mathematic transformation techniques are used to model the presence of heat sources inside the routing environment. Then the A* algorithm is used for compute the 3D routing, aiming at minimum wire harness weight. The main architecture of the routing application is presented and its functionality is demonstrated with samples of wire harness routing inside a wing. The results show that the proposed KBE application can automate the routing of wire harness while taking into account different rules and constraints. The modeling approach for a heat source can be generalized and extended to address other criticality such as abrasion, electromagnetic interference, corrosion, etc. The achieved level of automation relieves designers from the repetitive work associated with the frequent changes affecting the design environment.
机译:线束设计是一项日益复杂的任务。基于知识的工程(KBE)和优化技术可用于支持设计人员处理这种复杂性。线束设计过程可分为三个主要部分,即电气设计,配置设计和几何布线。本文介绍了针对路由阶段自动化的KBE应用程序开发的最新进展。离散优化技术用于设计最短路径约束,同时遵守不同类型的约束。在先前的论文中已经介绍了一些初步结果,其中仅解决了几何约束。但是,线束设计还受到其他类型的规则和约束的影响,必须考虑这些规则和约束,才能从优化过程中获得更实际的设计结果。本文介绍了选路应用程序中的一些新进展,以说明飞机内部关键区域的存在。作为研究案例,考虑了机身内部是否存在热源,这些热源要么迫使线束布线到其他地方,要么需要使用电线保护装置,这对重量和制造造成明显影响。首先,一些数学转换技术用于对路由环境内部热源的存在进行建模。然后将A *算法用于计算3D布线,以最小的线束重量为目标。介绍了路由应用程序的主要架构,并通过机翼内部的线束路由示例演示了其功能。结果表明,提出的KBE应用程序可以在考虑不同规则和约束的情况下自动进行线束布线。可以推广并扩展热源的建模方法,以解决其他关键问题,例如磨损,电磁干扰,腐蚀等。达到的自动化水平使设计人员摆脱了与影响设计环境的频繁更改相关的重复工作。

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