A support structure combining a fixed-hinge heavy-duty scissor adjustment mechanism with large-bend-radius high-pressure pipes is proposed for high-heat-flux testing of tonne-scale plasma-facing components. Rigid-body kinematics, finite-element analysis, conjugate heat transfer, and thermo-structural coupling were used to evaluate posture control, structural strength, cooling performance, and pipe response. Under a 10 kN load, maximum mechanism deformations were 0.16, 0.37, and 0.51 mm in the lowered, horizontal, and raised postures, respectively, while the maximum angular flexibility correction was 0.0197°. At 10 MW/m², the coolant temperature rise was 0.77 K, and the combined pressure loss of the two pipes was 90.87 kPa, or 1.82% of the 5 MPa operating pressure. The classified primary membrane-plus-bending stress and combined primary-plus-secondary stress were 88.344 and 105.8 MPa, below their respective limits of 150 and 300 MPa. Maximum pipe and heated-surface deformations were 0.22 and 0.15 mm, confirming adequate static performance of the system under the specified conditions.
No takes yet. Share an insight, caveat, or question.
Wang et al. (2026) studied this question.
Synapse has enriched 5 closely related papers on similar clinical questions. Consider them for comparative context: