公开(公告)号：US20240343382A1

公开(公告)日：2024-10-17

申请号：US18630256

申请日：2024-04-09

申请人： Airbus Operations GmbH

发明人： Dort DAANDELS ,  Florian LORENZ ,  Sönke WUNDERLICH

IPC分类号： B64C9/04 ,  B64C9/02 ,  B64C9/16

CPC分类号： B64C9/04 ,  B64C9/02 ,  B64C9/16

摘要： An aerodynamic system for an aircraft. The aerodynamic system includes a first aerodynamic component configured to be movably coupled to a primary structure of the aircraft, a second aerodynamic component which is movably coupled to the first aerodynamic component and a first panel element coupled to the first aerodynamic component. The first panel element at least partially covers a gap between the first aerodynamic component and the second aerodynamic component. The aerodynamic system further includes a sealing element arranged between the first aerodynamic component and the second aerodynamic component. The sealing element is configured to at least partially block an airflow between the first aerodynamic component and the second aerodynamic component.