发明名称 |
Variable inlet guide vanes for varying gas turbine engine inlet air flow |
摘要 |
<p>A method for assembling an articulated fan front frame for a gas turbine engine facilitates improving engine performance. The method includes forming a strut (60) including a pair of sidewalls (80) connected at a leading edge (82) and a trailing edge (84), forming a flap (62) including a first sidewall and a second sidewall connected at a leading edge and a trailing edge, and extending in radial span between a root endwall (86) and a tip endwall (88), wherein each endwall extends between the first and second sidewalls, and wherein at least one of the root endwall and the tip endwall is contoured in a radial direction extending between the flap leading and trailing edges, and pivotally coupling the flap downstream from the strut such that a gap is defined between the flap and the strut. <IMAGE></p> |
申请公布号 |
EP1340894(B1) |
申请公布日期 |
2007.06.13 |
申请号 |
EP20030251106 |
申请日期 |
2003.02.25 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
CAPOZZI, JOSEPH;ZENON, RUBY LASANDRA;TURNER, ALAN GLEN;WALLIS, CAROL VACZY;SZUCS, PETER NICHOLAS |
分类号 |
F01D17/00;F02C7/042;F01D5/14;F01D17/16;F02K1/12;F04D27/00;F04D29/54;F04D29/56;F04D29/64 |
主分类号 |
F01D17/00 |
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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