WING-FUSELAGE STRUCTURAL COMPONENT FOR THE CONNECTION OF TWO AIRFOILS AND A FUSELAGE SECTION ON AN AIRCRAFT,申请号EP20080867053-传众专利搜索

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发明名称	WING-FUSELAGE STRUCTURAL COMPONENT FOR THE CONNECTION OF TWO AIRFOILS AND A FUSELAGE SECTION ON AN AIRCRAFT
摘要
申请公布号	EP2229317(B1)	申请公布日期	2012.07.04
申请号	EP20080867053	申请日期	2008.12.30
申请人	AIRBUS OPERATIONS GMBH	发明人	GROSS, CLAUS-PETER
分类号	B64C1/12;B64C1/26	主分类号	B64C1/12
代理机构		代理人
主权项
地址

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