发明名称 A fan blade for a gas turbine engine
摘要 <p>An injection-moulded thermoplastic mini-platform (42) is adhesively bonded, in use, to the aerofoil surfaces of a fan blade (312) in a gas turbine engine. The mini-platform (42) is divided into a number of leaves (46), to increase its flexibility, and ribs (48) beneath the leaves (46) provide additional stiffness in the radial direction. In the event that a fan blade is released in operation, the mini-platform (42) is designed to detach from the blade (312) and/or to break apart, so that damage to other components of the engine is minimised.</p>
申请公布号 EP1881159(A1) 申请公布日期 2008.01.23
申请号 EP20070252531 申请日期 2007.06.22
申请人 ROLLS-ROYCE PLC 发明人 EVANS, DALE EDWARD
分类号 F01D11/00;F01D21/04 主分类号 F01D11/00
代理机构 代理人
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