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发明公开
CN106323582A 一种超微尺寸飞行器风洞实验台的装置 有权

一种超微尺寸飞行器风洞实验台的装置
摘要：
本发明提供一种超微尺寸飞行器风洞实验台装置，包括一体化飞行器实验架、实验段、实验段支撑架、整流栅格、CPU可调转速器、CPU可调转速器固定架、导轨、微型飞行器，其中：一体化飞行器实验架与三个整流栅格相接触；一体化飞行器实验架与实验段支撑架相接触；一体化飞行器实验架与两个CPU可调转速器固定架相接触；两个CPU可调转速器固定架分别与两个CPU可调转速器相接触并将两个CPU可调转速器固定；实验段支撑架与实验段相接触并将实验段固定；实验段内部有导轨；微型飞行器在导轨上。本发明实现了对微型风洞的实验装置的设计，实现了微型飞行器空气动力学的测量，实现了小飞机的拍打频率与流场的关系的检测。
摘要（英）：

The invention provides an ultramicro-size aircraft wind tunnel experiment table device, and the device comprises an integrated aircraft experiment frame, an experiment segment, an experiment segment support, rectification grids, CPU adjustable tachometers, CPU adjustable tachometer fixing frames, a guide rail and a miniature aircraft, wherein the integrated aircraft experiment frame contacts with three rectification grids. The integrated aircraft experiment frame contacts with the experiment segment support. The integrated aircraft experiment frame contacts with two CPU adjustable tachometer fixing frames. The two CPU adjustable tachometer fixing frames respectively contact with two CPU adjustable tachometers, and enable the two CPU adjustable tachometers to be fixed. The experiment segment support contacts with the experiment segment, and enables the experiment segment to be fixed. The interior of the experiment segment is provided with the guide rail. The miniature aircraft is disposed on the guide rail. The device achieves the design of an experiment device for a miniature wind tunnel, achieves the aerodynamic measurement of a miniature aircraft, and achieves the detection of relation between the beat frequency and flow field of a small plane.

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