Differential pressure distribution measurement of a free-flying butterfly wing
Differential pressure distribution measurement of a free-flying butterfly wing
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DOI：
10.1109/transducers.2011.5969207
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发表时间：
2011-06
期刊：
影响因子：
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通讯作者：
H. Takahashi;K. Matsumoto;I. Shimoyama
中科院分区：
文献类型：
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作者：
H. Takahashi;K. Matsumoto;I. Shimoyama
利用MEMS差压传感器测量自由飞行蝶翼的差压分布。压阻悬臂梁被用作差压传感器。传感器芯片的尺寸分别为1.0 mm × 1.0 mm × 0.3 mm，重量为0.7 mg，因此它不会干扰翅膀的运动。使用一只蝴蝶（凤蝶protenor）与传感器芯片连接到机翼表面，在起飞过程中，在翼展方向上的五个点在前翼和一个点在后翼的中心的分布进行了测量。结果表明，机翼上产生的最大气动力是作用在机身上的重力的3倍。
This paper reports on differential pressure distribution measurement of a free-flying butterfly wing with a MEMS differential pressure sensor. A piezoresistive cantilever was used as a differential pressure sensor. The sensor chip was 1.0 mm × 1.0 mm × 0.3 mm in size and 0.7 mg in weight, respectively, so that it did not interfere with wing motion. Using a butterfly (Papilio protenor) with a sensor chip attached to the wing surface, the distribution of five points to the spanwise direction at the forewing and one point at the center of the hindwing was measured during takeoff. As a result, it was clarified that the maximum aerodynamic force generated on the wing was 3 times larger than the gravity acting on the body.