发明名称 |
Bleed structure for a bleed passage in a gas turbine engine |
摘要 |
A bleed structure for a bleed passage in a gas turbine engine includes a first wall portion defining a first side of an opening for the passage, and a second wall portion defining a second side, opposite the first side of the opening. The first and second wall portions end at different positions in an extension direction of the opening.
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申请公布号 |
US8528344(B2) |
申请公布日期 |
2013.09.10 |
申请号 |
US20100752284 |
申请日期 |
2010.04.01 |
申请人 |
MAARTENSSON HANS;NILSSON MARTIN;VOLVO AERO CORPORATION |
发明人 |
MAARTENSSON HANS;NILSSON MARTIN |
分类号 |
F02C6/08;F02C6/04 |
主分类号 |
F02C6/08 |
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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