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
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