| 发明名称 |
DEVICE FOR PROTECTING THE FRONT SPAR STRUCTURE OF A CENTRAL CASING OF AN AIRCRAFT WING AND AT LEAST ONE PIECE OF EQUIPMENT LOCATED IN SAID WING |
| 摘要 |
A device for protecting a front spar structure of a central casing of an aircraft wing and at least one item of equipment situated in the wing, comprising:;a shielding surface extending in front of the front spar of the central casing, from a surface of an intersection between the wing and the fuselage delimited by the root of the wing, transversely to the surface of intersection, to a first rib of the central casing partially surrounding at least one item of equipment; and;means—for fixing the shielding surface to the central casing producing an isostatic link. |
| 申请公布号 |
US2016176501(A1) |
申请公布日期 |
2016.06.23 |
| 申请号 |
US201314417406 |
申请日期 |
2013.06.20 |
| 申请人 |
Airbus Operations (SAS) |
发明人 |
Dazet Francis |
| 分类号 |
B64C3/28;B64D45/00 |
主分类号 |
B64C3/28 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A device for protecting a front spar structure of a central casing of an aircraft wing and at least one item of equipment situated in the wing, comprising:
a shielding surface extending in front of the front spar of the central casing, from a surface of an intersection between the wing and the fuselage delimited by the root of the wing, transversely to the surface of intersection, to a first rib of the central casing partially surrounding at least one item of equipment; and means for fixing the shielding surface to the central casing to produce an isostatic link. |
| 地址 |
Toulouse FR |
