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Aerospace Panels Fixtureless Inspection Methods with Restraining Force Requirements; A Technology Review

机译:航空航天面板可固定的检测方法具有抑制力要求; 技术评论

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Aerospace panels are commonly restrained on complex inspection fixture jigs during the measurement process. Forces used to restrain the part are also monitored because of the part functional requirements. Given the difficulties in measuring these types of parts, this paper reviews the available fixtureless inspection methods with a focus on the challenges of their implementation and their aptitude to be used to estimate the part profile and the necessary restraining forces of an aerospace panel. To perform this investigation, finite element analysis is used to predict the constrained shape of four (4) simulated free state aerospace panel, with two different type of boundary condition, in five scenarios. From those analyses, the importance and limits of current finite element boundary setting method embedded in fixtureless inspection methods for nonrigid parts are highlighted.
机译:航空航天面板通常在测量过程中抑制复杂的检查夹具夹具。 由于零件功能要求,还监测用于抑制该部件的力量。 鉴于测量这些类型的零件困难,本文审查了可用的无限无线检测方法,重点关注其实施的挑战及其用于估计部分轮廓和航空航天面板的必要抑制力的挑战。 为了进行这一调查,有限元分析用于预测四(4)个模拟的自由状态航空航天面板的受约束形状,具有两种不同类型的边界条件,五种情况。 从那些分析中,突出了无限零件固定检测方法中嵌入了当前有限元边界设置方法的重要性和限制。

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