| 发明名称 |
A BLEED STRUCTURE FOR A BLEED PASSAGE IN A GAS TURBINE ENGINE |
| 摘要 |
<p>The invention relates to a bleed structure (17) for a bleed passage in a gas turbine engine. The structure comprises a first wall portion (18) defining a first side of an opening for the passage, and a second wall portion (19) defining a second side, opposite the first side of the opening. The first and second wall portions (18;19) end at different positions in an extension direction of the opening.</p> |
| 申请公布号 |
WO2006091138(A1) |
申请公布日期 |
2006.08.31 |
| 申请号 |
WO2005SE00452 |
申请日期 |
2005.03.24 |
| 申请人 |
VOLVO AERO CORPORATION;MAARTENSSON, HANS;NILSSON, MARTIN |
发明人 |
MAARTENSSON, HANS;NILSSON, MARTIN |
| 分类号 |
F02K3/075;F02K3/02 |
主分类号 |
F02K3/075 |
| 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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