High-temperature and high-pressure preparation method of continuous carbon fiber reinforced aluminum base composite material powder
A composite material and reinforced aluminum-based technology, applied in the field of aerospace manufacturing, can solve the problem that continuous carbon fiber reinforced aluminum-based composite materials do not have a relatively complete process, and achieve the effects of high density, uniform organization and excellent performance.
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[0029] A high-temperature and high-pressure preparation method of continuous carbon fiber reinforced aluminum matrix composite material powder proposed by the present invention will be described in detail below with reference to the accompanying drawings and specific examples.
[0030] like figure 1 — Figure 5 As shown, the high temperature and high pressure preparation method of continuous carbon fiber reinforced aluminum matrix composite material powder proposed by the present invention includes the following steps carried out in order:
[0031] 1) According to the size of the carbon fiber, such as figure 1 The envelope 5 shown is composed of a U-shaped base plate 1, a side wall plate 2 and an upper cover plate 4 with a vacuum tube 3. In order to prevent the carbon fiber material from deforming with the deformation of the sheath during hot isostatic pressing, the wall thickness of the upper cover plate 4 and the side wall plate 2 is 5mm, and the wall thickness of the U-sh...
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