Invention Grant
- Patent Title: Clamping device and method for assembly of stringer couplings
- Patent Title (中): 夹紧装置及其连接方法
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Application No.: US13267917Application Date: 2011-10-07
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Publication No.: US08646161B2Publication Date: 2014-02-11
- Inventor: Rolf Bense , Axel Sauermann , Eugen Gorr
- Applicant: Rolf Bense , Axel Sauermann , Eugen Gorr
- Applicant Address: DE Hamburg
- Assignee: Airbus Operations GmbH
- Current Assignee: Airbus Operations GmbH
- Current Assignee Address: DE Hamburg
- Agency: Leydig, Voit & Mayer, Ltd.
- Priority: DE102010047561 20101007
- Main IPC: B23Q1/00
- IPC: B23Q1/00

Abstract:
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.
Public/Granted literature
- US20120084962A1 CLAMPING DEVICE AND METHOD FOR ASSEMBLY OF STRINGER COUPLINGS Public/Granted day:2012-04-12
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