Continuous fiber reinforced sic part preparation method and product based on additive manufacturing
A continuous fiber and fiber-reinforced technology, which is applied in the field of continuous fiber-reinforced SiC parts preparation, can solve problems such as the difficulty in manufacturing continuous fiber composite parts, and achieve the effects of short preparation cycle, wide adaptability and easy operation
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment 1
[0052] (a) Construct the CAD model of the part, convert it into STL format, and use the fused deposition modeling additive manufacturing technology, use ABS as the polymer material, and untreated continuous carbon fiber as the reinforcing fiber material to form a three-dimensional polymer blank;
[0053] (b) thermally decomposing and carbonizing the three-dimensional polymer preform obtained in step (a) under vacuum conditions at 600° C. for 5 hours to obtain a carbon preform;
[0054] (c) Use the precursor impregnation cracking method, vacuumize the air in the preform, and then immerse the carbon preform in the toluene solution of polycarbosilane, pressurize to make the polycarbosilane fully fill the pores of the preform, and fill the preform after curing. The carbon preform with polycarbosilane is moved to the cracking furnace, and heat-treated at 900°C under vacuum conditions. The polycarbosilane is cracked at high temperature and reacts with the carbon preform to form SiC, ...
Embodiment 2
[0056] (a) Construct the CAD model of the part, convert it into STL format, and adopt the fused deposition modeling additive manufacturing technology, use PLA as the polymer material, and the continuous carbon fiber with CVD deposited SiC on the surface as the reinforcing fiber material to form a three-dimensional polymer preform;
[0057] (b) Pyrolysis and carbonization of the three-dimensional resin structure obtained in step (a) under vacuum conditions at 900°C for 8 hours to obtain a carbon preform;
[0058] (c) Use the precursor impregnation cracking method, vacuumize the air in the preform, and then immerse the carbon preform in the carbon tetrachloride solution of polycarbosilane, pressurize the polycarbosilane to fully fill the pores of the preform, and cure Finally, the carbon preform filled with polycarbosilane is moved to a cracking furnace, and heat-treated at 800°C under vacuum conditions. The polycarbosilane is cracked at high temperature and reacted with the carb...
Embodiment 3
[0060] (a) Construct the CAD model of the part, convert it into STL format, and adopt the fused deposition modeling additive manufacturing technology, use PC as the polymer material, and the continuous glass fiber with surface chemical modification as the reinforcing fiber material to form a three-dimensional polymer blank;
[0061] (b) Pyrolytically carbonizing the three-dimensional resin structure obtained in step (a) under an argon atmosphere at 800° C. for 10 h to obtain a carbon preform;
[0062] (c) Using the precursor impregnation and cracking method, vacuumize the air in the preform, and then immerse the carbon preform in the n-hexane solution of polycarbosilane, pressurize to make the polycarbosilane fully fill the pores of the preform, and cure it. The carbon preform filled with polycarbosilane is moved to a cracking furnace and heat-treated at 1100°C under vacuum conditions. The polycarbosilane is cracked at high temperature and reacts with the carbon preform to form...
PUM
| Property | Measurement | Unit |
|---|---|---|
| density | aaaaa | aaaaa |
Abstract
Description
Claims
Application Information
Login to View More 
