| 发明名称 | Vent for an aircraft wing fuel tank | ||
| 摘要 | An aircraft fuel tank vent opening having a liquid separation nozzle, the liquid separation nozzle and the opening dimensioned such that migration across the liquid separation nozzle to the underside of a wing, of fuel escaping from the vent opening, is inhibited during normal operating conditions. | ||
| 申请公布号 | US9346554(B2) | 申请公布日期 | 2016.05.24 |
| 申请号 | US201314387087 | 申请日期 | 2013.03.19 |
| 申请人 | Airbus Operations Limited | 发明人 | James Dylan |
| 分类号 | B64D37/02;B64D37/00;B64C3/34 | 主分类号 | B64D37/02 |
| 代理机构 | Nixon & Vanderhye P.C. | 代理人 | Nixon & Vanderhye P.C. |
| 主权项 | 1. An aircraft wing having a fuel tank vent, the vent terminating at an opening in a wing surface, the fuel tank vent having a liquid separation nozzle, the liquid separation nozzle extending from an inside surface of the fuel tank vent at a position inward of the opening, and terminating substantially in line with the opening, a gap being defined between the nozzle and the opening such that migration of fuel escaping from the vent from the liquid separation nozzle to the wing surface, is inhibited. | ||
| 地址 | Bristol GB | ||