发明名称 Structural component for aircraft
摘要 The component (1) has several reinforcement profiles (2), which are at least partly welded onto at least one main plate (4). Reinforcements (5) are arranged on the reinforcement profiles. Preferably, the reinforcement profiles are formed as longitudinal stringers and transverse ribs. The reinforcements may be formed as doublers (6), which are each glued or riveted on one side of profile bars (3A) of the profiles. Independent claims are included for a reinforcement profile for the structure component and for a method to manufacture the structure component.
申请公布号 AU5405501(A) 申请公布日期 2002.01.03
申请号 AU20010054055 申请日期 2001.06.26
申请人 EADS AIRBUS GMBH 发明人 HANS-JURGEN SCHMIDT
分类号 B64C1/08;B23K31/02;B64C1/12 主分类号 B64C1/08
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