Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
271097 | Fusion Engineering and Design | 2014 | 6 Pages |
•The load combination method is introduced to thermal–structural analysis for contradictive loads occurred simultaneously.•The one-way coupling analysis also conducted for thermal–structural analysis and its validity is checked by comparing with the load combination.•The dominant load for triangular support bracket is determined as the baking condition.
The triangular support is located on the lower inner shell of vacuum vessel of ITER, which should be designed to withstand various loads such as nuclear heat, coolant pressure and so on. The appropriateness of its design is evaluated under the dominant load that could represent the most conservative condition among the design loads. In order to decide the dominant load, a valid method for thermal–structural analysis is firstly verified considering contradictory behaviors between heat and structural loads.In this paper, two approaches; one-way coupling and load combination, are introduced for thermal–structural analysis. The one-way coupling is a method generally used but has a limit to apply on contradictory conditions. The load combination could give a proper solution since it evaluates each load independently and then adds up each result linearly. Based on the results of each case, structural analysis for another load case, baking condition with incident, is conducted to find out which load is dominant for triangular support.Consequently, it is found that the baking condition is the dominant load for triangular support bracket. The proposed load combination method gives a physically reasonable solution which can be used as a reference for checking the validity of other thermal–structural analysis. It is expected that these results could be applied for manufacturing design of the triangular support under various load conditions.