TW200611932A - The manufacture processing of a high-temperature carbon composite - Google Patents
The manufacture processing of a high-temperature carbon compositeInfo
- Publication number
- TW200611932A TW200611932A TW093131156A TW93131156A TW200611932A TW 200611932 A TW200611932 A TW 200611932A TW 093131156 A TW093131156 A TW 093131156A TW 93131156 A TW93131156 A TW 93131156A TW 200611932 A TW200611932 A TW 200611932A
- Authority
- TW
- Taiwan
- Prior art keywords
- carbon composite
- ablation
- refractory
- compacting treatment
- compacting
- Prior art date
Links
Abstract
This invention is a manufacture processing of a high-temperature carbon composite. Rich beta-resin is added into pitch and a solvent to form a pre-preg material, which is processed with carbon fiber to form pre-preg cloth, followed by the processes of press molding, carbonized treatment, compacting treatment by fururyl alcohol, and resin curing. By one compacting treatment process, the density of the specimen can reach 1.56g/cm3 and the bending stress can reach 41,000psi. The characteristic of this invention is to use a simple process to develop a manufacturing method of low-cost, high-temperature for carbon composite material without use of expensive equipment and graphite fiber, and the number of using the compacting treatment can be decreased and this method can fabricate a component having large size, so the product can be applied to different kinds of ablation materials, such as a refractory nozzle. Because this refractory material can be applied to many kinds of ablation nozzles, the carbon composite material must be heated up to 580~1000 DEG C and processed by the compacting treatment process, so the design of this invention can both fulfill the required effect of refractory and ablation.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
TW93131156A TWI300079B (en) | 2004-10-14 | 2004-10-14 | The manufacture processing of high-temperature carbon composite |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
TW93131156A TWI300079B (en) | 2004-10-14 | 2004-10-14 | The manufacture processing of high-temperature carbon composite |
Publications (2)
Publication Number | Publication Date |
---|---|
TW200611932A true TW200611932A (en) | 2006-04-16 |
TWI300079B TWI300079B (en) | 2008-08-21 |
Family
ID=45069870
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
TW93131156A TWI300079B (en) | 2004-10-14 | 2004-10-14 | The manufacture processing of high-temperature carbon composite |
Country Status (1)
Country | Link |
---|---|
TW (1) | TWI300079B (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
TWI615268B (en) * | 2016-12-30 | 2018-02-21 | 國家中山科學研究院 | Integrated ablative adiabatic coating |
-
2004
- 2004-10-14 TW TW93131156A patent/TWI300079B/en active
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
TWI615268B (en) * | 2016-12-30 | 2018-02-21 | 國家中山科學研究院 | Integrated ablative adiabatic coating |
US10913553B2 (en) | 2016-12-30 | 2021-02-09 | National Chung Shan Institute Of Science And Technology | Integrated ablative heat shield |
Also Published As
Publication number | Publication date |
---|---|
TWI300079B (en) | 2008-08-21 |
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