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- W4384341068 abstract "Abstract In order to realize a stable clamping of the large cabin part, this paper studied the optimization of the clamping force for the clamping mechanism of the large-mass and large-size cabin part. Firstly, three kinds of contact models are introduced. Then a clamping matrix is constructed for a particular clamping configuration and the nonlinear friction cone constraint at the contact point is transformed into a linear affine constraint in a smooth Riemannian manifold by using the special structure of the positive definite symmetric matrix. Finally, a large cabin part in the aerospace field is used as an example for calculation and simulation of the clamping force optimization. Different optimization algorithms are used to calculate the initial value which will be put into the gradient flow optimization method of the clamping force for optimization calculation. The numerical results and curves show that the gradient flow optimization method of the clamping force can quickly complete the clamping force optimization of the large-mass and large-size cabin part. The distribution of the normal force of the clamping mechanisms and the convergence value of the clamping force for each clamping mechanism can provide some references for determining the output clamping force of the clamping mechanism and confirming a reasonable distribution of the clamping mechanism. It also proved the feasibility and effectiveness of this method applied in the clamping force optimization for the large axial part." @default.
- W4384341068 created "2023-07-15" @default.
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- W4384341068 date "2023-07-14" @default.
- W4384341068 modified "2023-09-25" @default.
- W4384341068 title "Optimization Method of The Clamping Force for Large Cabin Parts" @default.
- W4384341068 doi "https://doi.org/10.21203/rs.3.rs-2913930/v1" @default.
- W4384341068 hasPublicationYear "2023" @default.
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