| 发明名称 | Translating cable device sealing | ||
| 摘要 | An aircraft wing assembly, comprising a wing having a fixed leading edge, a slat mounted for movement between a retracted position and an extended position with respect to the fixed leading edge, and a translating cable device for electrically connecting the slat to the wing and having a strut coupled at one end to the slat, the fixed leading edge having an aperture to accommodate the strut, and a seal assembly for sealing between the strut and the aperture. | ||
| 申请公布号 | US9027890(B2) | 申请公布日期 | 2015.05.12 |
| 申请号 | US201213714701 | 申请日期 | 2012.12.14 |
| 申请人 | Airbus Operations Limited | 发明人 | Wilson James;Hadley Paul;Teodoru Alexandru |
| 分类号 | B64C13/30;B64C9/22;B64D15/12 | 主分类号 | B64C13/30 |
| 代理机构 | Lowe Hauptman & Ham, LLP | 代理人 | Lowe Hauptman & Ham, LLP |
| 主权项 | 1. An aircraft wing assembly, comprising a wing having a fixed leading edge, a slat mounted for movement between a retracted position and an extended position with respect to the fixed leading edge, and a translating cable device for electrically connecting the slat to the wing and having a strut coupled at one end to the slat, the fixed leading edge having an aperture to accommodate the strut, and a seal assembly for sealing between the strut and the aperture, wherein the seal assembly includes a first seal fixed within the aperture, and a second seal fixed to the strut of the translating cable device, and wherein the first and second seals contact when the slat is moved to one or more predetermined positions. | ||
| 地址 | Bristol GB | ||