Vibration test system and test method for full missile vibration in rotating state of rotating missile
A technology of vibration test and rotation state, applied in vibration test, machine/structural component test, wave/particle radiation, etc., can solve the problems of insufficient reliability and environmental adaptability assessment of rotating missiles, and achieve the balance of gravity Effect
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Embodiment 1
[0047] The present invention provides a vibration test system for full-bullet vibration under the rotating state of a rotating missile, such as Figure 1-6 As shown, it includes a vibration device 100 , a fixing device 200 and a rotating device 300 . The fixing device 200 fixes the rotating missile 17 on the vibration device 100 , and the end of the rotating missile 17 is connected to the rotating device 300 ; the rotating missile 17 realizes vibration excitation through the vibration device 100 The application of the rotating missile 17 through the fixing device 200 realizes the balance of the gravity of the missile, and the rotating missile 17 realizes the application of the rotating motion through the rotating device 300 .
[0048] The fixing device 200 includes a missile hoisting ring 9, a rubber rope 10 and a gantry 11. The missile hoisting ring 9 is evenly connected to the rotating missile 17 to drive the rotating missile to maintain gravity balance. like Figure 4 As s...
Embodiment 2
[0055] The present invention also provides a test method for the vibration test system of the full-elastic vibration under the rotating state of the rotating missile, which specifically includes the following steps:
[0056] Step 1: use three-dimensional design software, dynamic analysis software, and system simulation software to establish the mapping of the entire test system in the virtual digital space, and conduct virtual experiments in the virtual digital space;
[0057] Step 2: In the virtual digital space, continuously adjust the position of the excitation point and the suspension position, and select the optimal position of the excitation point, suspension position, and vibration control point according to the virtual test results, and obtain the dynamic transfer characteristics of the missile. parameter;
[0058] Step 3: Design the vibration fixture 7, the missile suspension ring 9 and the rotating fixture 12 according to the selected optimal excitation point positio...
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