发明名称 |
CLAMPING DEVICE AND METHOD FOR ASSEMBLY OF STRINGER COUPLINGS |
摘要 |
A clamping device is provided for an assembly of a stringer coupling in a region of a lateral butt joint between a first and a second fuselage section of an aircraft for coaxially connecting a respective first and second stringer of the first and the second fuselage sections, the stringer coupling intersecting a frame element profile in the region of the lateral butt joint. A supporting yoke is configured to bridge the frame element profile in an arc-shaped manner and includes a first end foot supported by the stringer coupling on the first side of the frame element profile and a second end foot supported by the stringer coupling on the second side of the frame element profile. The supporting yoke includes a middle tensioning hook configured to interact with the frame element profile. The first and the second end feet are tensionable against the stringer coupling.
|
申请公布号 |
US2012084962(A1) |
申请公布日期 |
2012.04.12 |
申请号 |
US201113267917 |
申请日期 |
2011.10.07 |
申请人 |
BENSE ROLF;SAUERMANN AXEL;GORR EUGEN;AIRBUS OPERATIONS GMBH |
发明人 |
BENSE ROLF;SAUERMANN AXEL;GORR EUGEN |
分类号 |
B25B5/16;B23P11/00;B23P17/00 |
主分类号 |
B25B5/16 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|