A landing gear bay door system for a landing gear bay is provided, the landing gear bay door system comprising: a bay door pivotable about a pivot pin configured to be disposed in a longitudinal direction on a fuselage; and a mechanism configured to rotate the door about the pivot pin between a closed position in which the outer surface of the door panel is configured to provide aerodynamic continuity with the outer aircraft skin of the fuselage and an open position in which the door is rotated into the landing gear compartment and the opening is exposed. The door has a door panel rigidly connected to the arm such that the door panel and the arm generally form a V-shape as seen in the longitudinal direction.
提供了一种用于起落架舱的起落架舱门系统,该起落架舱门系统包括:舱门,该舱门可绕枢轴销枢转,该枢轴销被配置为在机身上沿纵向方向设置;以及机构,该机构被配置成使舱门在关闭位置与打开位置之间绕枢轴销转动,在关闭位置中,门板的外表面被配置为提供与机身的外飞行器蒙皮的空气动力连续性,而在打开位置中,该舱门被转动到起落架舱中并且开口被暴露。该舱门具有与臂刚性地连接的门板,使得门板和臂总体上形成如沿纵向方向看到的V形状。
Landing gear bay door system for landing gear bay
用于起落架舱的起落架舱门系统
2022-07-15
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
LANDING GEAR DOOR SYSTEM AND LANDING GEAR DOOR SYSTEM OPERATION METHOD
European Patent Office | 2021
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