发明名称 |
NACELLE DRAG REDUCTION DEVICE FOR A TURBOFAN GAS TURBINE ENGINE |
摘要 |
<p>The nacelle drag reduction device (22) comprises a substantially circular and axis symmetrical external airfoil (24) concentric with a aft section of the nacelle (20) and located outside a propulsive jet zone (30) defined behind the engine (10) when operating, the airfoil (24) being positioned at a location providing a maximum streamline angle with reference to the main axis (26) of the engine (10) and a highest streamline curvature.</p> |
申请公布号 |
WO2008058368(A1) |
申请公布日期 |
2008.05.22 |
申请号 |
WO2007CA01812 |
申请日期 |
2007.10.10 |
申请人 |
PRATT & WHITNEY CANADA CORP.;ALECU, DANIEL T. |
发明人 |
ALECU, DANIEL T. |
分类号 |
B64C23/00;B64D29/00;F01D25/28;F15D1/08;F15D1/10 |
主分类号 |
B64C23/00 |
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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