发明名称 |
A flow directing element and a method of manufacturing a flow directing element |
摘要 |
<p>A thrust reverser cascade flow directing element (28) for a gas turbine engine (10) comprises a plurality of plates (30) and a plurality of flow directing vanes (40). At least one vane (40) extends between each pair of plates (30), the plurality of plates (30) are formed from sheet material and a single integral piece of ductile sheet material (32) forms the plurality of flow directing vanes (40). The single integral piece of ductile sheet material (32) has a plurality of longitudinally spaced apart apertures (36) and a plurality of longitudinally spaced apart sheet material portions (38) between the apertures (36) and the ductile sheet material (32) is bent at a plurality of longitudinally spaced positions such that each sheet material portion (38) defines one of the plurality of flow directing vanes (40). <IMAGE></p> |
申请公布号 |
EP1118763(B1) |
申请公布日期 |
2004.09.22 |
申请号 |
EP20010300287 |
申请日期 |
2001.01.15 |
申请人 |
ROLLS-ROYCE PLC |
发明人 |
HOLME, MICHAEL JOHN;BISHOP, JEFFREY CHARLES |
分类号 |
F02K1/54;F02K1/70;(IPC1-7):F02K1/54;F02K1/72;B21D31/00;B23P15/00 |
主分类号 |
F02K1/54 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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