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Automation of the surface finishing of rotorcraft blades.

机译:旋翼飞机叶片表面精加工的自动化。

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Most automated surface finishing done today is on parts with simple geometry and parts made of only one material, usually metal. Although greater flexibility was achieved in previous research, the process was not applied to the surface finishing of metallic/fiberglass junctures, such as seams and raised steps when smoothed over with a filling material. Further, unlike single material fairing, where no filling material needs to be shaped and ground, the dispensing and forming methods need to be developed so as to compliment the grinding methods. This document presents the developed processes for filling and forming with special emphasis on the fairing of joints, seams, and ridges of fiberglass/metal interfaces when filled with filling material. The specific case study presented is the automation of the filling, forming, and fairing of rotorcraft blades. Additional material is included on factory implementation of the process.
机译:如今,大多数自动表面精加工都是在具有简单几何形状的零件和仅由一种材料(通常为金属)制成的零件上进行的。尽管在先前的研究中获得了更大的灵活性,但是该方法并未应用于金属/玻璃纤维接合处的表面精加工,例如在使用填充材料进行平滑处理时的接缝和凸起台阶。此外,与单一材料整流罩不同,在该单一材料整流罩中,不需要成形和研磨填充材料,需要开发分配和成形方法以补充研磨方法。该文件介绍了填充和成形的开发过程,特别强调了填充填充材料时玻璃纤维/金属界面的接缝,接缝和脊的光洁度。提出的具体案例研究是旋翼飞机叶片的填充,成型和整流的自动化。该过程的工厂实施中包含其他材料。

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