Supercritical carbon dioxide reactor microsphere fuel assembly
A carbon dioxide, spherical fuel technology, applied in the direction of reactor fuel elements, reactors, fuel elements, etc., can solve problems such as difficult to have practical operability, and achieve the effect of solving application feasibility, reducing pressure drop, and achieving significant effects
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Embodiment 1
[0025] A microspherical fuel assembly for a supercritical carbon dioxide reactor mainly includes an upper nozzle 1 , a fuel section, and a lower nozzle 7 . Among them, the fuel section includes a coolant inlet 5, a fuel microsphere placement area, and a coolant outlet 6 arranged in sequence from the inside to the outside, and the fuel section constitutes an annular "sandwich biscuit" with "internal and external cavities and middle heat release" geometry, such as figure 1 shown. The coolant inlet 5, the fuel microsphere placement area, and the coolant outlet opening 6 can be arranged coaxially or not, as long as the fuel microsphere placement area is socketed outside the coolant inlet opening 5, the coolant outlet opening 6 It only needs to be socketed on the outside of the fuel microsphere placement area. In this embodiment, it is preferably coaxially arranged, such as figure 1 shown.
[0026] In this embodiment, the fuel microsphere placement area is alternately arranged a...
Embodiment 2
[0030] The difference between this embodiment and Embodiment 1 is that in this embodiment, the structural setting of the annular release zone is mainly optimized, as follows:
[0031] The axial cross-section of the annular heat dissipation zone is a trapezoidal structure, and the side of the annular heat dissipation zone adjacent to the coolant inlet 5 is the long side of the trapezoidal structure.
[0032] At the same time, the arrangement of the supporting structures 2 is also optimized in the present invention. In this embodiment, 3 to 8 supporting structures 2 are arranged at intervals of 200 mm to 400 mm along the axial direction of the fuel microsphere placement area. In this embodiment, the axial interval of the support structure 2 is set to 300mm, the number of support structures 2 is arranged as 4, and there are 3 annular cooling zones arranged alternately with the support structure 2, as figure 1 shown.
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