Spacer grid with anti-snag and cross action for nuclear fuel assemblies
A nuclear fuel assembly and spacer grid technology, which is applied in the fields of reactor fuel elements, nuclear engineering, nuclear power generation, etc., can solve the risk of increasing the local pressure drop of the side grid element, hindering the lateral mixing of the coolant, and the large hook of the spacer grid, etc. The problem is to reduce the local pressure loss, enhance the anti-hook performance, and reduce the blockage.
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Embodiment 1
[0020] Such as figure 1 As shown, the positioning grid with anti-hooking and mixing functions for nuclear fuel assemblies includes a grid composed of several strips interwoven vertically with each other, and the strips are divided into inner strips 4 and outer strips 1 , the outer strip 1 is arranged outside the inner strip 4, and the outer strip 1 is vertically connected with the corresponding inner strip 4, and the upper and lower ends of the outer strip 1 are symmetrically provided with several guide wings 2, and the guide wings The upper part of 2 is provided with a through hole 3, and the guide wing 2 is arranged at the intersection of the inner strip 4 and the outer strip 1. The guide wings 2 on the upper part of the outer strip 1 of the positioning grid are arranged continuously, that is, they are arranged in a completely neat manner similar to the guide wings 2 on the lower part, and the mixing wings 5 on the first inner strip 4 on the inner side are inserted, and th...
Embodiment 2
[0030] Such as figure 2 As shown, the structure of embodiment 2 is basically the same as that of embodiment 1, except that the number of through holes 3 on the guide wing 2 is several, and the guide wing 2 is arranged in a honeycomb shape. After the through-holes 3 are arranged in a honeycomb shape, the individual through-holes 3 have a small diameter, but the overall area increases, which improves the fluid mixing effect.
[0031] The perforated guide vane 2 will not hinder the lateral flow of coolant between adjacent components, and enhance the mixing performance between components. At the same time, the perforated guide vane 2 also reduces the blockage of the flow area of the opposite cell , which is beneficial to reduce local pressure loss and improve thermal safety margin.
[0032] When the number of through holes 3 on the guide wing 2 is arranged in a honeycomb shape, the diameter of each through hole 3 is small. When resisting the passage of the coolant, the coolant...
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