发明名称 |
Stator for a jet engine, a jet engine comprising such a stator, and an aircraft comprising the jet engine |
摘要 |
A stator for installation in a rear section of a jet engine includes a plurality of guide vanes which extend in the radial direction of the stator and between them define ducts for leading a gas. A first side of the stator in its axial direction defines an inlet for the gas and a second side, opposite the first side, defines an outlet for the gas. The guide vanes have such a shape that together they at least substantially cover the gas inlet viewed in the axial direction of the stator from the outlet side thereof. |
申请公布号 |
US8403629(B2) |
申请公布日期 |
2013.03.26 |
申请号 |
US20050718727 |
申请日期 |
2005.10.20 |
申请人 |
LUNDBLADH ANDERS;VOLVO AERO CORPORATION |
发明人 |
LUNDBLADH ANDERS |
分类号 |
F01D5/14;F01D25/16;F02K;F02K1/46 |
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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