Drag reduction surface structure of underwater vehicle shell
A technology of underwater vehicle and surface structure, which is applied in the direction of hull, ship construction, hull design, etc., can solve the problems of high navigation resistance and unsatisfactory effect of the vehicle, so as to improve the navigation speed and stability and reduce energy consumption , Significant economic and environmental benefits
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Embodiment 1
[0037] This embodiment is used to manufacture the novel underwater vehicle shell that adopts the drag-reducing surface, and selects the method of stencil printing to construct the drag-reducing structure on the surface of the shell, such as figure 2 As shown, the feather-shaped drag-reducing structure forming the feather-shaped drag-reducing structure array is composed of a rachis structure 2 and a barb structure 3, the rachis structure 2 is composed of ravines, the barb structure 3 is composed of protrusions, and the barb structure 3 The included angle with the fluid flow direction is 45 degrees. The cross-sectional shapes of rachis and protrusions are circular, rachis structure 2 and barb structure 3 are linear, and the width ratio of rachis structure and barb structure is 3:1. The feather-shaped drag-reducing structure is evenly distributed on the upper surface of the aircraft shell, and the structural size is fixed and uniformly distributed. As the depth increases, the de...
Embodiment 2
[0044] This embodiment is used to manufacture a new type of underwater vehicle shell with a drag-reducing surface, and the method of 3D printing is selected to construct the drag-reducing structure of the shell surface, such as image 3 As shown, the feather-shaped drag-reducing structure constituting the feather-shaped drag-reducing structure array is composed of a rachis structure 2 and a barb structure 3, the rachis structure 2 is a raised structure, the barb structure 3 is a ravine structure, and the barb structure 3 The included angle with the fluid flow direction is 30 degrees. The cross-sectional shape of the protrusion is circular, the rachis structure 2 is linear, the barb structure 3 is curved, and the width ratio of the rachis structure 2 and the barb structure 3 is 2:1. The feather-shaped drag reducing structure is evenly distributed on the upper surface of the aircraft shell, and the structure size of the feather shaft on the upper surface is larger than the struc...
Embodiment 3
[0051] This embodiment is used to manufacture a new type of underwater vehicle shell with a drag-reducing surface. The laser direct writing method is selected to construct the drag-reducing structure on the surface of the shell. The feather-shaped drag-reducing structure forming the array of feather-shaped drag-reducing structures consists of The rachis structure 2 and the barb structure 3 are composed of the rachis structure 2 and the barb structure 3, both of which are ravine structures, and the angle between the barb structure 3 and the direction of fluid flow is 20 degrees. The cross-sectional shape of the rachis is circular, the rachis structure 2 is linear, the barb structure 3 is linear, and the width ratio of the rachis structure 2 and the barb structure 3 is 3:1. The feather-shaped drag-reducing structure is evenly distributed on the upper surface of the aircraft shell, and the structure size of the feather shaft on the upper surface is smaller than the structure size ...
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