发明名称 |
METHOD OF MANUFACTURING HIGH PRESSURE CONTAINERS |
摘要 |
The pressure container used as high-pressure combustion tube of a rocket engine, is manufactured by polar and helical winding method. The method is composed of forming a primary laminated body (10) by mounting a small diameter boss (7) at an end of a mandrel (6), mounting a metallic jig (9) having a larger diameter than the boss (7) and a large diameter boss (8), winding the fiber by the polar winding method; laminating a secondary laminated body (13) on the body (10) by mounting jig (11) having a smaller diameter than the boss (8) at the outside of the boss (7), mounting a jig having the same diameter as the boss (8) on the boss (8), winding the fiber by the helical winding method. |
申请公布号 |
KR940003246(B1) |
申请公布日期 |
1994.04.16 |
申请号 |
KR19920004370 |
申请日期 |
1992.03.17 |
申请人 |
THE RESEARCH INSTITUTE OF NATIONAL DEFENCE SCIENCE |
发明人 |
PARK, BYONG - RYOL;JONG, SANG - KI;JONG, BAL;JONG, KUN - CHUN;KIM, JONG - SHIK |
分类号 |
B29C70/16;B29C53/60;B29C70/06;B29D22/00;B29K105/08;B29L22/00;F17C1/16;(IPC1-7):B21D51/00 |
主分类号 |
B29C70/16 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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