发明名称 |
Vortex reducing device for a gas turbine engine |
摘要 |
<p>A gas turbine engine (12) has a vortex reducing device (20) therein that includes a retainer (30) and paddles (32). The retainer is arcuate in shape and has a plurality of circumferentially spaced slots (46) that extend through it. The paddles are circumferentially spaced about the retainer and extend outward therefrom. Each paddle is disposed between adjacent slots.</p> |
申请公布号 |
EP2410136(A2) |
申请公布日期 |
2012.01.25 |
申请号 |
EP20110165089 |
申请日期 |
2011.05.06 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
YILMAZ, CAGDAS |
分类号 |
F01D25/12;F01D5/08;F04D27/02;F04D29/58 |
主分类号 |
F01D25/12 |
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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