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首页> 外文期刊>INCAS Bulletin >Design, Aerodynamic Calculation and Manufacturing using CFRP and Additive Manufacturing of a small Tilt-Rotor UAV for Railway Inspection
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Design, Aerodynamic Calculation and Manufacturing using CFRP and Additive Manufacturing of a small Tilt-Rotor UAV for Railway Inspection

机译:使用CFRP的设计,空气动力学计算和制造,以及用于铁路检查的小型倾斜式无人机的添加剂制造

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The present paper aims to develop a small scale Unmanned Aerial Vehicle for railway inspection. The development process and structure manufacturing aimed at a low complexity technological process both to meet market requirements and to be economically efficient. To define the architectural structure and its components in the design process, a NACA 0024 aerodynamic profile was selected out of two proposed airfoils. The novelty of this concept is the double benefit of the wing, which serves as a cargo bay while uses a low-cost manufacturing technology, incorporating the 3D printing process. Further, a simplified preliminary aerodynamic calculation was performed, the model was manufactured using composite materials reinforced with carbon fibre while other key components have been obtained using the 3D printing technology. In the end, the manufacturing process was a success and the unmanned aerial vehicle was designed and manufactured specifically that its flight envelope meets the requirements of the mission.
机译:本文旨在为铁路检验开发一辆小型无人驾驶车辆。开发过程和结构制造旨在满足市场要求的低复杂性技术过程,经济效率。为了在设计过程中定义架构结构及其组件,选择了一个NACA 0024空气动力学曲线,其中包括两个提出的翼型。这种概念的新颖性是机翼的双重效益,它用作货架湾,而使用低成本的制造技术,包括3D打印过程。此外,进行简化的初步空气动力学计算,使用用碳纤维增强的复合材料制造模型,而使用3D打印技术获得了其他关键部件。最后,制造过程是成功,无人驾驶的航空公司是专门设计和制造的,其飞行信封满足了使命的要求。

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