Ball hinge support structure of large caliber reflector of space remote sensor
A technology for large-diameter mirrors and space remote sensors, which is applied in the field of space remote sensing, can solve problems such as affecting imaging quality, difficulty in assembly, and affecting the surface shape of reflecting mirrors, and achieves the effect of satisfying task requirements, easy assembly, and avoiding assembly stress.
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[0015] The invention presses figure 2 The structure shown is implemented. Among them, the mirror support assembly 9 presses image 3 , Figure 4 with Figure 5 The structure shown is implemented.
[0016] Among them, the main mirror 7 is made of SiC material with a size of Φ676mm in diameter and 99.7mm in thickness. The backplane 8 is made of 4J32 material, and the size is 402x461x38mm. The mirror assembly repairing pad 10 is made of 4J32 material, and the size is 151x90x2mm. The protective cover 11 is made of 2A12 material, with a size of Φ72mm in diameter and 1mm in thickness. The third screw 14 is made of 30CrMnsi. The first screw 12 and the second screw 13 are made of TB3 material. The cone sleeve 15 is made of 4J32 material, and the size is Φ79mm in diameter and 58mm in height. The connecting flange 17 is made of 4J32 material, and its size is Φ82mm in diameter and 18mm in height. The first cylindrical pin 23 and the second cylindrical pin 24 are made of TC4 material....
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