Flexible aerofoil vibration detecting and control device based on high-speed camera and method thereof
A technology of vibration detection and high-speed camera, which is applied in the direction of mechanical vibration control, measuring device, vibration test, etc., can solve the problem that vibration information cannot be fed back to the driver, etc., and achieve the effect of suppressing multi-mode vibration, excellent performance, and improving reliability
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Embodiment 1
[0033] Such as figure 1 , image 3 and Figure 4 As shown, the present embodiment provides a flexible wing vibration detection and control device based on a high-speed camera, including a flexible wing body part, a vibration detection part, a vibration control part, a signal processing module and a computer (15), the flexible wing The wing body part includes the wing (1), base (5) and exciter (6), and the wing (1) is composed of 11 ribs (4) and 6 beams (3) to form a support (wing The internal structure diagram is as follows figure 2 shown), and is composed of a layer of skin (2) on the outside, the wing (1) is 1500mm long, the length of the wing root is about 500mm, and the length of the wing tail is about 400mm, which is installed through the base (5) On the test stand (12), the surface of the wing (1) is parallel to the test stand (12), and the left and right wing (1) upper surfaces are respectively provided with marker points for vibration detection (mark points on the ...
Embodiment 2
[0039] This embodiment provides a method for detecting and controlling the vibration of a flexible wing based on a high-speed camera, the method comprising the following steps:
[0040] Step 1. The signal generator (18) sends out a vibration signal, which is amplified by the power amplifier (19) and then sent to the two exciters (6). Wing (1) produces multi-modal vibrations. During the vibration process of left and right wings (1), two pairs of binocular vision systems composed of high-speed camera Ⅰ (8) and high-speed camera Ⅱ (9) respectively monitor the left and right wings ( 1) Synchronous shooting is carried out, and the photos are transmitted to the computer (15), and after image processing, the vibration information of the left and right wings (1) is obtained, and at the same time, the vibration information measured by the acceleration sensor (10) is amplified by the charge amplifier (13) After being converted by the A / D converter (16), it is input into the computer (15...
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