Volume 38 Issue 12
Dec.  2023
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REN Haoyuan, WANG Yi, WANG Liang, et al. Mechanical model of locking mechanisms of folding wing for spacecraft[J]. Journal of Aerospace Power, 2023, 38(12):3009-3019 doi: 10.13224/j.cnki.jasp.20220032
Citation: REN Haoyuan, WANG Yi, WANG Liang, et al. Mechanical model of locking mechanisms of folding wing for spacecraft[J]. Journal of Aerospace Power, 2023, 38(12):3009-3019 doi: 10.13224/j.cnki.jasp.20220032

Mechanical model of locking mechanisms of folding wing for spacecraft

doi: 10.13224/j.cnki.jasp.20220032
  • Received Date: 2022-01-19
    Available Online: 2023-09-12
  • To model the plug-in locking mechanism, the plane strain assumption and superposition principles were used for dimensionality reduction and simplification, and an analytical model of connection stiffness considering the effect of gap was established. Firstly, the energy method was used to solve the indeterminate problem caused by contact friction, and the normal and tangential contact forces were obtained. Then, the equivalent contact stiffness was calculated by using Hertz’s theory, and the bending deformation of elastic pins was calculated through beam model. To validate the applicability of the method, the analytical results were compared with the experimental results from the reference paper. Finally, the parameter influence analysis was carried out, and the effect of load and clearance on connection stiffness was proposed. The results showed that when the load changed from 20 N·m to 50 N·m, the connection stiffness of the locking mechanism increased by about 3%—5%, demonstrating a hardening spring nonlinear effect. With the increase of the clearance, the connection stiffness showed a downward trend, owing to the fact that the fit size affected the relative attitude of the elastic pin and the hole.

     

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