发明名称 COMPOSITE FAN CASE WITH INTEGRAL CONTAINMENT ZONE
摘要 A turbofan engine which has a composite fan case surrounding a fan with a plurality of fan blades is disclosed. The composite fan case includes a containment zone having an inner fabric layer composed of resin-impregnated fibres substantially uni-axially oriented in a common angular direction corresponding to a blade release angle of the fan blades. The fan case also includes a composite outer shell and an energy absorbing core disposed radially between the inner fabric layer and the composite outer shell. The energy absorbing core includes non resin impregnated multidirectional fibres.
申请公布号 US2010077721(A1) 申请公布日期 2010.04.01
申请号 US20080239177 申请日期 2008.09.26
申请人 MARSHALL ANDREW R 发明人 MARSHALL ANDREW R.
分类号 F01D21/00;B23P15/00;F01D25/24 主分类号 F01D21/00
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