| 发明名称 | Rotating inlet cowl for a turbine engine, comprising an eccentric forward end | ||
| 摘要 | A rotating inlet cowl for a turbine engine, having a rotation axis and for which the forward end is arranged to be eccentric relative to this rotation axis. Furthermore, a forward cone of the cowl is truncated by a truncation surface defining the forward end of the inlet cowl. | ||
| 申请公布号 | US8984855(B2) | 申请公布日期 | 2015.03.24 |
| 申请号 | US201013262386 | 申请日期 | 2010.03.31 |
| 申请人 | SNECMA | 发明人 | Delapierre Mickael;Gignoux Herve;Loro Gael;Wintenberger Sylvie |
| 分类号 | F02G3/00;F02K1/78;F02K99/00;F02K3/06;B64D15/16;B64D15/00;F03B15/22;F03D11/04;F04D29/60;F04D29/52;F02C7/047;F02C6/20 | 主分类号 | F02G3/00 |
| 代理机构 | Oblon, McClelland, Maier & Neustadt, L.L.P. | 代理人 | Oblon, McClelland, Maier & Neustadt, L.L.P. |
| 主权项 | 1. A rotating inlet cowl of a gas turbine engine, the cowl having a rotation axis and comprising: a forward cone defining a forward end of the inlet cowl, wherein the forward end is configured to be eccentric relative to the rotation axis of the inlet cowl, wherein the forward cone is truncated by a truncation surface defining the forward end of the inlet cowl, and wherein the forward cone is oblique with an axis inclined from the axis of rotation of the inlet cowl. | ||
| 地址 | Paris FR | ||