| 发明名称 |
DEPLOYABLE INFLATABLE WING |
| 摘要 |
The invention relates to a space wing, produced by means of a diaphragm forming a polygonal surface provided with an inflatable structure which includes ribs extending over the diaphragm along diagonals of the diaphragm and passing through a central point of the diaphragm. The inflatable structure includes at least one film strip, the perimeter of which adheres onto the diaphragm such as to form an inflatable space with the diaphragm. |
| 申请公布号 |
US2016304220(A1) |
申请公布日期 |
2016.10.20 |
| 申请号 |
US201415103121 |
申请日期 |
2014.12.18 |
| 申请人 |
AIRBUS DEFENCE AND SPACE SAS |
发明人 |
CECCHINI Guillaume;GUENAT Hervé;MAHY Claude-Emile |
| 分类号 |
B64G1/22;B64G1/44;B64G1/66;B64G1/40 |
主分类号 |
B64G1/22 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A space wing produced by means of a membrane forming a polygonal surface provided with an inflatable structure which comprises ribs extending over the membrane along diagonals of the membrane and passing through a central point of the membrane, wherein the inflatable structure comprises at least one film strip the contour thereof being adhesively bonded to the membrane so as to form an inflatable volume with the membrane and to produce extension ribs of the membrane. |
| 地址 |
Les Mureaux FR |
