| 发明名称 |
DEVICE FOR RETAINING A TANK IN AN AIRCRAFT |
| 摘要 |
The present invention relates to a device for mounting and supporting a generally cylindrical or tapered tank, having a main axis X, that includes a pair of first means for retaining the tank along a vertical axis Z on each of a first and second end of the tank, a second means for retaining the tank along a horizontal axis Y, perpendicular to the main axis, on the first end of the tank, and a third means for retaining in a ball-and-socket joint, the means being located around the vertical axis and connected to the second end of the tank. |
| 申请公布号 |
US2015360792(A1) |
申请公布日期 |
2015.12.17 |
| 申请号 |
US201414765399 |
申请日期 |
2014.02.04 |
| 申请人 |
ASTRIUM SAS ;AIRBUS DEFENCE AND SPACE SAS |
发明人 |
FAURE Benjamin;BERTRAND Jérôme;CORABOEUF Yohann;CHEVROLLIER Samuel;ABADIE-LA-HAILLE Robert;MEZIERES Pascal;SANTERRE Angélique |
| 分类号 |
B64D37/04;B64G1/40;B64D37/30;B64D37/06 |
主分类号 |
B64D37/04 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A supporting and holding device for a tank of a cylindrical or conical overall shape and of a main axis X in a vehicle such as an aircraft, comprising a pair of first tank-retaining means for retaining the tank along an axis Z perpendicular to the main axis X at each of a first and of a second end of the tank, a second tank-retaining means along an axis Y perpendicular to the main axis X and to the axis Z, at the first end of the tank and a third tank-retaining means designed to retain the tank along the axis X and the axis Y and connected to the second end of the tank. |
| 地址 |
Suresnes FR |
