AEROSPACE SHANGHAI, Volume. 41, Issue 3, 167(2024)
Design Optimization and Experimental Verification of Trundle Bearing Mechanisms for Spacecrafts
Fig. 1. Solar-oriented driving mechanisms for small and medium-sized spacecrafts at home and abroad
Fig. 2. Trundle bearing mechanisms for space stations at home and abroad
Fig. 3. Working principle of the trundle bearing mechanism in single pattern
Fig. 4. Design scheme and mechanism principle of the trundle bearing assembly
Fig. 5. Roller-rail kinematic pairs between the trundle bearing assembly and rail
Fig. 6. Schematic diagram of the roller-rail kinematic pair at Roller A
Fig. 8. Status of the trundle bearing assembly and rail before and after clamping
Fig. 9. Principle of the vacuum circular rail test and picture of the test equipment
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Decai YANG, Jianhui LI, Chuankun QU, Daxing HUANG, Zhifei MA, Zhiyi WANG, Zhiyuan QIAN. Design Optimization and Experimental Verification of Trundle Bearing Mechanisms for Spacecrafts[J]. AEROSPACE SHANGHAI, 2024, 41(3): 167
Category: Innovation and Exploration
Received: Jun. 7, 2024
Accepted: --
Published Online: Sep. 3, 2024
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