Measurement and monitoring method for centroid skewing permitted interference of multi-axis support air floating platform
An air-floating platform and a technology that allows interference. It is applied in the direction of non-electric variable control, supporting machines, machine platforms/supports, etc., and can solve problems such as limited leveling state of the supporting platform, interference, and narrow application range.
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specific Embodiment approach 1
[0048] Specific implementation mode one: the following combination Figure 1 to Figure 10 Describe this embodiment, the method for measuring and monitoring the allowable interference of the center of mass offset of the multi-axis supported air flotation platform described in this embodiment, the multi-axis supported air flotation platform includes a bearing platform 1, three support legs 2, and three air pontoons 3 and three gas feet 4,
[0049] The bearing platform 1 is a circular platform, and the bearing platform 1 is supported by three support legs 2, and the three connection points between the three support legs 2 and the lower surface of the bearing platform 1 form an equilateral triangle, and the center of the equilateral triangle is aligned with the bearing platform. The center of the circle of 1 coincides;
[0050] The end of each support leg 2 is connected to an air buoy 3, and the bottom end of each air buoy 3 is connected to an air foot 4 through an air buoyancy b...
specific Embodiment approach 2
[0092] Specific implementation mode two: the following combination Figure 1 to Figure 10 Describe this embodiment, this embodiment will further explain Embodiment 1 or 2, the radius of carrying platform 1 described in this embodiment is 2 meters, three support legs and three connection points on the lower surface of carrying platform 1 constitute equilateral The distance between the apex of the triangle and the center of the bearing platform 1 is 1.4 meters.
[0093] image 3 As shown, the line connecting the support legs 2 of the multi-axis support air bearing platform and the three connection points A, B, and C on the lower surface of the bearing platform 1 forms an equilateral triangle whose side length is L=2424mm. The air foot 4 relies on compressed air to form an air film between the air-floating ball bearing and the ball sleeve to achieve approximately frictionless motion to simulate the dynamic environment in which the spacecraft is subjected to a minimal disturbance...
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