A Fiber Arrangement Method for Improving the Mechanical Properties of Ceramic Matrix Composites for Engine Hot End Components
A composite material and fiber arrangement technology, which is applied in the field of fiber arrangement methods to improve the mechanical properties of ceramic matrix composite materials for engine hot end components, can solve the problems of cracking, deformation, low transverse mechanical properties, etc., and achieves increased transverse mechanical properties. performance, the effect of improving mechanical properties
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Embodiment 1
[0034] figure 1 A schematic diagram of a two-dimensional cross-section of a fiber structural unit provided by the present invention; as figure 1 As shown, the fiber structure unit includes: a total of 4 layers from top to bottom, with a total of 10 fibers; among them, a total of 5 fibers in the upper 2 layers, arranged in an equilateral triangle; a total of 6 fibers in the middle 2 layers, arranged in a square; the lower 2 layers A total of 5 fibers are arranged in an inverted triangle.
[0035] where the triangles are arranged as figure 2 As shown, 3 fibers surround to form a triangle.
[0036] Quartet arranged as image 3 As shown, 4 fibers surround to form a rectangle.
[0037] Wherein, the side length of the triangle formed by the 3 fibers arranged in a triangle is larger than the diameter of the fiber.
[0038] The side length of the rectangle formed by four fibers arranged in a square is larger than the fiber diameter.
Embodiment 2
[0040] Figure 4 A schematic diagram of a two-dimensional cross-section of another fiber structural unit provided by the present invention;
[0041] The fiber structure unit includes: a total of 4 layers from top to bottom, a total of 10 fibers; wherein, a total of 5 fibers in the upper 2 layers are arranged in an equilateral triangle; a total of 6 fibers in the middle 2 layers are arranged in a square; A total of 5 fibers in the layer are arranged in an inverted equilateral triangle. Of course, in addition to equilateral triangles, the arrangement of isosceles triangles is also possible; the normal stress in the X direction of the arrangement of equilateral triangles is lower than that of the arrangement of isosceles triangles. (The normal stress in the X direction will be explained in detail later)
[0042] Wherein, the side length of the triangle formed by the three fibers arranged in a triangle is equal to the diameter of the fiber.
[0043] The side length of the recta...
Embodiment 3
[0048] like Figure 5 Shown is an embodiment of the ceramic matrix composite material for the engine hot end component formed by repeating the transverse arrangement of the fiber structural units in the first embodiment.
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