An aircraft landing gear door (140) includes an attachment mechanism adapted to pivotally mount the door to an aircraft; a first side (141) arranged to face inward with respect to the aircraft landing gear compartment when the door is closed and to face one side of a main leg of the landing gear when the door is open and the landing gear is deployed; and an opposite second side portion (142). A shape formed by the first side portion and the second side portion provides an airfoil profile of the door. An aircraft landing gear arrangement (100), an aircraft (1000), a method of operating an aircraft and a method of reducing noise are also provided.
一种飞行器起落架舱门(140)包括:附接机构,该附接机构适用于将门枢转地安装至飞行器;第一侧部(141),该第一侧部布置成在门关闭时相对于飞行器起落架舱面向内侧,并且第一侧部在门打开且起落架展开时面向起落架的主支腿的一个侧部;以及相反的第二侧部(142)。由第一侧部和第二侧部形成的形状提供了门的翼型外形。本发明还提供了一种飞行器起落架布置结构(100)、一种飞行器(1000)、一种操作飞行器的方法以及一种减小噪音的方法。
Aircraft landing gear hatch door
飞行器起落架舱门
2023-05-26
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
CONNECTING ROD MECHANISM FOR CONTROLLING AIRCRAFT LANDING GEAR HATCH DOOR
Europäisches Patentamt | 2018
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