发明名称 |
Turbomachine nozzle cowl, and corresponding nozzle and turbomachine |
摘要 |
<p>The bonnet (14) has jet noise reduction units (26) arranged in extension a trailing edge (14a) of the bonnet and circumferentially spaced to each other. Each unit has a triangular contour with a base (26a) formed by a part of the edge, and has an apex (26b) spaced towards downstream of the base and connected to the base by two sides (26c). Each side is connected to the edge based on a bent contour of each side with a bend radius (R) higher than or equal to that of a bent contour of the apex. The bent contour of each side has an inflection point (28) at a tangent (30) parallel to the base.</p> |
申请公布号 |
EP1873389(A1) |
申请公布日期 |
2008.01.02 |
申请号 |
EP20070109797 |
申请日期 |
2007.06.07 |
申请人 |
SNECMA |
发明人 |
AU, DAX;BIGOT, PASCAL MOISE MICHEL;BRIEND, PIERRE;LOHEAC, PIERRE, PHILIPPE, MARIE |
分类号 |
F02K1/38;F02K1/48 |
主分类号 |
F02K1/38 |
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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