Invention Grant
- Patent Title: Composite structure
- Patent Title (中): 复合结构
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Application No.: US13641210Application Date: 2011-04-07
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Publication No.: US09102102B2Publication Date: 2015-08-11
- Inventor: Jonathan Meyer , Michael Matthews
- Applicant: Jonathan Meyer , Michael Matthews
- Applicant Address: GB Bristol
- Assignee: Airbus Operations Limited
- Current Assignee: Airbus Operations Limited
- Current Assignee Address: GB Bristol
- Agency: Nixon & Vanderhye P.C.
- Priority: GB1006257.8 20100415
- International Application: PCT/GB2011/050687 WO 20110407
- International Announcement: WO2011/128667 WO 20111020
- Main IPC: B32B5/12
- IPC: B32B5/12 ; B29C70/20 ; B64C3/26 ; B29L31/08 ; B29L31/30

Abstract:
A structure comprising a plurality of plies of fiber-reinforced composite material, each ply having a ply orientation defined by a principal stiffness direction of the ply. The structure has a first region and a second region, each region comprising N1 primary plies, N4 cross plies with a ply orientation substantially perpendicular to the primary plies, N2 positive-angled bias plies with a ply orientation at a positive acute angle to the primary plies, and N3 negative-angled bias plies with a ply orientation substantially perpendicular to the positive-angled bias plies. The ply orientation of the primary plies in each region is more closely aligned with a primary axis of the structure than the cross plies or the bias plies. N1=N4 in the first region but not in the second N region, and N2=N3 in the second region but not in the first region. In each of the two regions, one ply set is balanced and the other ply set is un-balanced. This provides a compromise between the advantages of using un-balanced ply sets, for instance to provide bending torsion coupling, and the disadvantage that un-balanced ply sets can introduce thermally induced distortion during manufacture.
Public/Granted literature
- US20130034684A1 COMPOSITE STRUCTURE Public/Granted day:2013-02-07
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