Continuous fiber-reinforced silicon carbide member, manufacturing method thereof, and nuclear reactor structural member
A manufacturing method and technology of silicon carbide, which are applied in the directions of reactor fuel elements, moderator/core structure, reactor, etc., can solve problems such as brittle fracture, and achieve the effect of improving environmental resistance and improving mechanical properties
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no. 1 Embodiment approach >
[0028] [constitute]
[0029] figure 1 It is a perspective view schematically showing the long-fiber-reinforced silicon carbide member of the first embodiment.
[0030] Such as figure 1 As shown in , the long-fiber-reinforced silicon carbide member 1 of this embodiment is, for example, a cylindrical tubular body in which long fibers are continuously arranged in the long-fiber-reinforced silicon carbide member 1 .
[0031] figure 2 It is a sectional view showing the long-fiber-reinforced silicon carbide member of the first embodiment. figure 2 In , the long-fiber-reinforced silicon carbide member 1 is shown for a cross-section perpendicular to the axial direction.
[0032] Such as figure 2 As shown in , the long fiber reinforced silicon carbide member 1 has a first composite material layer 11 and a second composite material layer 21, and the first composite material layer 11 and the second composite material layer 21 are laminated in the radial direction.
[0033] The f...
no. 2 Embodiment approach >
[0050] [constitute]
[0051] Figure 6 It is a cross-sectional view showing a long-fiber-reinforced silicon carbide member of the second embodiment. Figure 6 and figure 2 Similarly, regarding the long-fiber-reinforced silicon carbide member 1 , a cross-section perpendicular to the axial direction is shown.
[0052] Such as Figure 6 As shown in , the long-fiber-reinforced silicon carbide member 1 of the present embodiment includes the first composite material layer 11 and the second composite material layer 21 similarly to the case of the first embodiment.
[0053] The long fibers of silicon carbide forming the first composite material layer 11 have a tensile strength of 2 to 4 GPa and a tensile modulus of 150 to 400 GPa. The carbon long fibers forming the second composite material layer 21 have a tensile strength of 1 to 7 GPa and a tensile modulus of 30 to 950 GPa. In the first composite material layer 11 and the second composite material layer 21, depending on the co...
no. 3 Embodiment approach >
[0069] [constitute]
[0070] Figure 9 It is a cross-sectional view showing a long-fiber-reinforced silicon carbide member according to a third embodiment. Figure 9 With figure 2 Similarly, with regard to the long fiber reinforced silicon carbide member 1 , a cross section perpendicular to the axial direction is shown.
[0071] Such as Figure 9 As shown in , in this embodiment, unlike the case of the first embodiment, the long-fiber-reinforced silicon carbide member 1 further has a coating material layer 41 . Except for this point and points related thereto, this embodiment is the same as the case of the first embodiment, and description of overlapping parts will be appropriately omitted.
[0072] The coating material layer 41 is provided so as to cover the outer peripheral surface of the second composite material layer 21 .
[0073] In the present embodiment, the coating material layer 41 is formed of a single substance of a material selected from carbon, titanium car...
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Abstract
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