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Bioinspired Low-Noise Wing Design for a Two-Winged Flapping-Wing Micro Air Vehicle

机译:具有生物启发的低噪声双翼扑翼双翼微型飞行器设计

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摘要

This work investigates the acoustic and thrust performances of different wing designs for a two-winged flapping-wing micro air vehicle (FW-MAV). The reference wings, made of a Mylar film membrane supported by carbon-fiber rods, produce a perceived overall noise of about 68.8 dBA when operating at the flapping frequency of 10 Hz typically required for flying such a flapping wing vehicle. This noise is much higher than the value of the environmental background. Wings of various materials and structural configurations are designed and tested in order to reduce the flapping-wing noise. Sound and force measurements are used to assess their acoustic and lift capabilities. It is found that a wing made with a highly elastic dielectric elastomer membrane can reduce the overall perceived noise of the flapping wing by 12 dBA while slightly increasing the thrust. The mechanisms leading to this noise reduction and their potential applications in quiet FW-MAVs are discussed.
机译:这项工作研究了两翼襟翼微飞行器(FW-MAV)的不同机翼设计的声学和推力性能。由机翼由碳纤维杆支撑的聚酯薄膜薄膜制成的参考机翼,在以这种拍翼飞行器通常需要的10 Hz拍振频率工作时,会产生约68.8 dBA的感知总噪声。这种噪声远高于环境本底值。设计并测试了各种材料和结构构造的机翼,以减少襟翼的噪音。声音和力的测量值用于评估其声学和升力能力。发现用高弹性的介电弹性体膜制成的机翼可以将襟翼的总感知噪声降低12 dBA,同时略微增加推力。讨论了导致这种噪音减少的机制及其在安静的FW-MAV中的潜在应用。

著录项

  • 来源
    《AIAA Journal》 |2018年第12期|4697-4705|共9页
  • 作者单位

    Natl Univ Singapore, Temasek Labs, Singapore 117411, Singapore;

    Cranfield Univ, Ctr Def Engn, Swindon SN6 8LA, Wilts, England;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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