发明名称 Process for lining composite rocket motor cases.
摘要 <p>The making of an elastomer lined composite rocket motor case or portion of such case is disclosed. The case or portion thereof is made by extruding a thin ribbon comprising a filled, crosslinkable elastomer containing unsaturated plasticizing oil and peroxide curative and causing it to continuously so encircle a center rotational axis of a mandrel as to adjacently position and tack together integral segments of the ribbon substantially circumferentially relative to this center rotational axis thereby forming a layer of the elastomer about the mandrel; applying a shell comprising filaments and thermosettable resin to the cured or uncured layer of elastomer; curing the thermosettable resin (preferably in stages with a later stage including cure of the elastomer) to provide the rocket motor case or portion thereof. The use of the filled, crosslinkable elastomer containing unsaturated plasticizing oil has processing advantages. The cured elastomer also has performance advantages.</p>
申请公布号 EP0116453(A2) 申请公布日期 1984.08.22
申请号 EP19840300721 申请日期 1984.02.06
申请人 HERCULES INCORPORATED 发明人 TAYLOR, TIMOTHY TERRANCE
分类号 B29C69/00;B29B15/00;B29C45/00;B29C51/00;B29C53/58;B29C53/60;B29C55/00;B29C61/00;B29C63/00;B29C65/70;B29C70/38;B29D22/00;B29K21/00;B29K105/08;B29L22/00;B32B1/02;B32B25/08;F02K9/34;(IPC1-7):29D3/02;02K9/34 主分类号 B29C69/00
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