发明名称 |
DEFLECTOR FOR A GAS TURBINE STRUT AND VANE ASSEMBLY |
摘要 |
A gas turbine engine is provided having an annular duct having an inner duct wall and an outer duct wall. At least one strut extends between the inner duct wall and the outer duct wall. The strut has an aerodynamic shape. At least one vane located circumferentially adjacent the strut and axially behind a leading edge of the strut, and an aerodynamic deflector located circumferentially between each strut and each vane. The aerodynamic deflector may positioned axially upstream of a flow separation point which would otherwise be caused by the strut. |
申请公布号 |
CA2699938(A1) |
申请公布日期 |
2010.10.24 |
申请号 |
CA20102699938 |
申请日期 |
2010.04.14 |
申请人 |
PRATT & WHITNEY CANADA CORP. |
发明人 |
DUROCHER, ERIC;SLEIMAN, MOHAMAD;TSIFOURDARIS, PANAGIOTA |
分类号 |
F01D5/14;F01D9/02;F01D25/28;F02C7/00 |
主分类号 |
F01D5/14 |
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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