发明名称 Wing box for aircraft wing, has framework connected to at least one exterior shell such that load acting on exterior shell is transferred by framework
摘要 <p>The wing box includes at least one exterior shell (1), a framework (7), and an interior shell (2) spaced apart from the exterior shell. The framework is connected to the at least one exterior shell such that a load acting on the exterior shell is transferred by the framework. An independent claim is also included for a method for transferring forces in a wing box of an aircraft wing.</p>
申请公布号 DE102005038851(A1) 申请公布日期 2007.03.01
申请号 DE20051038851 申请日期 2005.08.17
申请人 AIRBUS DEUTSCHLAND GMBH 发明人 MAENZ, CHRISTIAN
分类号 B64C3/18;B64C1/06;B64C1/26;B64C3/22 主分类号 B64C3/18
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