Invention Grant
US08801885B2 Method for making a structural part of a composite material having a calibrated thickness and structural part thus obtained
有权
制造具有由此获得的校准厚度和结构部分的复合材料的结构部分的方法
- Patent Title: Method for making a structural part of a composite material having a calibrated thickness and structural part thus obtained
- Patent Title (中): 制造具有由此获得的校准厚度和结构部分的复合材料的结构部分的方法
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Application No.: US12595313Application Date: 2008-04-09
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Publication No.: US08801885B2Publication Date: 2014-08-12
- Inventor: Mathieu Normand , Jean-Claude Lacombe
- Applicant: Mathieu Normand , Jean-Claude Lacombe
- Applicant Address: FR Toulouse
- Assignee: Airbus Operations SAS
- Current Assignee: Airbus Operations SAS
- Current Assignee Address: FR Toulouse
- Agency: Dickinson Wright PLLC
- Priority: FR0754446 20070413
- International Application: PCT/FR2008/050624 WO 20080409
- International Announcement: WO2008/139115 WO 20081120
- Main IPC: B29C65/00
- IPC: B29C65/00 ; B29C70/54

Abstract:
The disclosed embodiments offer a solution for controlling the thickness of a finished structural composite part when precise tolerances must be complied with for the quality of the assembly and in order to ease the assembly operations of this part. In order to implement the method according to the disclosed embodiments, an additional layer of plies made out of a non-structural composite material, called calibrating plies, is applied onto the structural plies of the structural part, at least in an area where the thickness must be maintained within close tolerances and, after the composite material has been cured, the calibrating plies are machined in order to obtain the thickness required for the finished part. The thickness of the calibrating plies applied is determined according to the possible thicknesses of structural plies, taking into account the manufacturing spreads so that the machining operation for the calibrating plies does not affect the structural plies.
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