发明名称 METHOD OF JOINING COMPOSITE COMPONENTS
摘要 Composite components (50) are joined by firstly locating portions of two separate composite components in adjacent or overlapping relation, to provide a join area. The components (50) are substantially fully cured, with the portions located within the join area being uncured or partially cured. At least one pressure chamber (3, 4) is located over the join area, the pressure chamber including a displacement abutment face (5, 6). Fluid is circulated at an elevated temperature and pressure through the pressure chamber to compress the join area with the displaceable abutment face of the pressure chamber and elevate its temperature in a controlled manner over time to effect curing of the join area.
申请公布号 EP1268120(B1) 申请公布日期 2015.04.22
申请号 EP20010909338 申请日期 2001.03.02
申请人 QUICKSTEP TECHNOLOGIES PTY, LTD. 发明人 GRAHAM, NEIL
分类号 B23P6/00;B29C65/48;B29C43/36;B29C65/00;B29C73/10;B29C73/12;B29C73/32;B32B37/12;B32B37/14;B32B37/16;B64F5/00 主分类号 B23P6/00
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