发明名称 VERBINDUNGSANORDNUNG ZUM VERBINDEN ZWEIER VERSTEIFUNGSELEMENTE UNTERSCHIEDLICHEN QUERSCHNITTPROFILS FÜR EIN LUFT- ODER RAUMFAHRZEUG, UND EIN SCHALENBAUTEIL
摘要 <p>A connecting arrangement for connecting two reinforcing elements of an aircraft or spacecraft, wherein the reinforcing elements have different cross-sectional profiles with at least one foot portion and at least one comb portion, at least one foot portion connecting element which on one side can be adapted to the geometric shape of the foot portion of the first reinforcing element and on the opposite side can be adapted to the geometric shape of the foot portion of the second reinforcing element and can be connected rigidly thereto; and at least one comb portion connecting element which on one side can be adapted to the geometric shape of the comb portion of the first reinforcing element and on the opposite side can be adapted to the geometric shape of the comb portion of the second reinforcing element and can be connected rigidly thereto.</p>
申请公布号 DE502008003231(D1) 申请公布日期 2011.05.26
申请号 DE20085003231T 申请日期 2008.12.10
申请人 AIRBUS OPERATIONS GMBH 发明人 TACKE, STEFAN;LENGSFELD, HAUKE;REYE, VOLKER
分类号 B64C1/12;B64C1/06 主分类号 B64C1/12
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