作者: Christian Wolf , Hanno Niemann , Patrik Schmiedel , Matthias Hopf
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摘要: A loads interface ( 1 ) of an aircraft structure with edge member 6 and a background both preferably made from fiber reinforced plastics. transferring flange 2 is adapted mounted to said transmit bending moments into the structure. Said provided two angled upper lower planes 8, 9 ). member's transfer 10, 11 The are paired essentially parallel respectively oriented each other angle approximately 90° . invention relates as well applications such