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首页> 外文期刊>International journal of micro air vehicles >The Energy Benefits of the Pantograph Wing Mechanism in Flapping Flight: Case Study of a Gull
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The Energy Benefits of the Pantograph Wing Mechanism in Flapping Flight: Case Study of a Gull

机译:受电弓翼机构在拍打飞行中的能量收益:以海鸥为例

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摘要

Bird wings generally contain a 4-bar pantograph mechanism in the forearm that enables the wrist joint to be actuated from the elbow joint thus reducing the number of wing muscles and hence reducing the wing inertia and inertial drag. In this paper we develop a theoretical model of inertial power for flapping flight to estimate the advantage of the 4-bar pantograph mechanism by comparing the inertial power required for the case where wrist muscles are present in the forearm with the case where wrist muscles are not present in the forearm. It is difficult to predict how wrist muscles would look when there is no pantograph mechanism. Therefore a lower bound and upper bound case are defined. The lower bound case involves redistributing the elbow muscles with no increase in wing mass. The upper bound case involves replicating the biceps-triceps muscles near the wrist joint. At minimum power speed the model estimates that the 4-bar pantograph mechanism reduces the inertial power for the gull from between 6.1%-12.3% and reduces the overall power by 0.6%-1.2%. When account is taken of the tight margins involved in the design of a flying vehicle, the energy savings produced by the pantograph mechanism are significant. A ring-billed gull was chosen for the case study and an adult specimen was obtained to gather morphometric data. Lessons for the design of flapping micro air vehicles are discussed.
机译:鸟的翅膀通常在前臂中包含一个4杆受电弓机构,该腕部使肘关节从腕关节致动,从而减少了机翼肌肉的数量,从而减少了机翼惯性和惯性阻力。在本文中,我们通过比较前臂中存在腕部肌肉和不存在腕部肌肉的情况下所需的惯性力,开发了一种用于扑翼飞行的惯性力理论模型,以估算4杆受电弓机构的优势。存在于前臂中。没有受电弓机制时,很难预测手腕肌肉的外观。因此,定义了下限和上限情况。下限情况涉及重新分配肘部肌肉,但不增加机翼质量。上限情况涉及复制腕关节附近的二头肌-肱三头肌。在最小功率速度下,模型估计4杆缩放机构将海鸥的惯性功率从6.1%-12.3%之间减小,并将总功率减小0.6%-1.2%。考虑到飞行器设计中的紧缩余量,受电弓机构产生的能量节省是可观的。选择环嘴鸥进行案例研究,并获得成年标本以收集形态学数据。讨论了拍打式微型飞行器的设计课程。

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  • 来源
    《International journal of micro air vehicles》 |2015年第3期|275-283|共9页
  • 作者单位

    Univ Bristol, Dept Mech Engn, Bristol BS8 1TH, Avon, England.;

    Univ Bristol, Dept Mech Engn, Bristol BS8 1TH, Avon, England.;

    Univ Bristol, Dept Mech Engn, Bristol BS8 1TH, Avon, England.;

    Liberty Univ, Dept Biol & Chem, Lynchburg, VA USA.;

    Liberty Univ, Dept Biol & Chem, Lynchburg, VA USA.;

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