发明名称 Composite structure
摘要 An example of a composite structure is a containment case 2 for a gas turbine engine 1 which comprises an annular housing 3 and an annular flange 4 which is integral with and is positioned at an end of the housing 3. The housing 3 comprises composite material which includes tape 9 laid in the circumferential direction of the housing. The flange 4 comprises composite material which includes tape 8 laid at an oblique angle to the circumferential direction of the flange 4 and/or tape 7 laid at a perpendicular angle to the circumferential direction. The flange 4 does not include tape 9 laid in the circumferential direction of the flange, because such tape would impede the forming of the flange material to form the flange.
申请公布号 GB2484476(B) 申请公布日期 2012.12.12
申请号 GB20100017121 申请日期 2010.10.11
申请人 GKN AEROSPACE SERVICES LIMITED 发明人 BEN RALFS;JOHN MORAM
分类号 B29C70/32;B29C70/38;F01D25/24 主分类号 B29C70/32
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