Forming system and material of carbon fiber reinforced aluminum matrix composites
A composite material and reinforced aluminum-based technology, applied in chemical instruments and methods, layered products, metal layered products, etc., can solve the problems of complex preparation process, low efficiency, and high cost
Active Publication Date: 2021-04-02
漳州宙士新材料科技有限公司
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Problems solved by technology
However, the preparation process of continuous carbon fiber reinforced aluminum matrix composites in the prior art is generally complicated, with long cycle time, high cost and low efficiency. the key of
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[0018] The technical solutions in the embodiments of the present invention are clearly and completely described below in conjunction with the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of them. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.
[0019] In the following description, a lot of specific details are set forth in order to fully understand the present invention, but the present invention can also be implemented in other ways different from those described here, and those skilled in the art can do it without departing from the meaning of the present invention. By analogy, the present invention is therefore not limited to the specific examples disclosed below.
[0020] like figure 1 A...
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The invention discloses a forming system of a carbon fiber reinforced aluminum-based composite material and the material. According to the system, carbon fiber yarn on a carbon fiber yarn wheel is uniformly soaked into aluminum alloy melt, so that an aluminum alloy liquid film is formed between the carbon fiber yarn; under the cooling effect, the aluminum alloy liquid film is solidified in the carbon fiber yarn direction and combined with the carbon fiber yarn so that a carbon fiber aluminum film composite layer can be formed; then after being pre-heated through a first heater, the carbon fiber aluminum film composite layer and aluminum foil are rolled together through a first extruding roller and a second extruding roller, and a carbon fiber reinforced aluminum-based composite layer is formed; annealing is performed through a second heater so that the carbon fiber reinforced aluminum-based composite layer can be wound onto a composite material winding roller under continuous extrudingof an extruding levelling roller, and the carbon fiber reinforced aluminum-based composite material is formed; and high temperature extruding improves the combining strength of the interface of the carbon fiber reinforced aluminum-based composite layer and the carbon fiber reinforced aluminum-based composite material. Thus, the system has the advantages of being simple in process, low in cost, good in carbon fiber and aluminum base combining effect and the like.
Description
technical field [0001] The invention relates to the technical field of carbon fiber-reinforced aluminum-based composite materials, in particular to a forming system and material for carbon-fiber-reinforced aluminum-based composite materials. Background technique [0002] Carbon fiber reinforced aluminum matrix composites with continuous interface structure have the characteristics of high specific strength, specific modulus, high thermal conductivity, low thermal expansion coefficient, and good dimensional stability at high temperature. Compared with ceramic materials, it has the characteristics of impact resistance, good toughness, thermal conductivity and electrical conductivity. Therefore, carbon fiber reinforced aluminum matrix composites are widely used in aerospace and aviation and other fields, as well as in the automotive industry, electronics, sporting goods, and construction fields. application. Commonly used preparation and molding methods include solid-state met...
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IPC IPC(8): B32B15/04C22C47/12C22C47/06C22C49/06C22C49/14C22C101/10
CPCC22C47/064C22C47/12C22C49/06C22C49/14
Inventor 王书杰孟静
Owner 漳州宙士新材料科技有限公司