The invention relates to a method for applying a cover (1) to an aircraft wing (2), the method comprising placing a skin (3) provided with one or more access holes (4) on the aircraft wing (2); placing a gasket (5) for the or each manhole (4) of the skin (3); placing a plug (6) in the or each manhole (4); and curing the aircraft wing (2) having the cover (1), the cover (1) comprising a skin (3), one or more gaskets (5) and one or more plugs (6). The invention also relates to an aircraft wing (2) comprising a cover (1) applied by said method, comprising a skin (3), one or more washers (5) and one or more plugs (6). This reduces application time, frequent cost and has positive environmental footprint effects.
本发明涉及一种用于将覆盖件(1)施加到飞行器机翼(2)的方法,该方法包括将设置有一个或更多个检修孔(4)的蒙皮(3)安置在飞行器机翼(2)上;将垫圈(5)安置成用于蒙皮(3)的该检修孔(4)或每个检修孔(4);将塞(6)安置在该检修孔(4)或每个检修孔(4)中;并且固化具有覆盖件(1)的飞行器机翼(2),覆盖件(1)包括蒙皮(3)、一个或多个垫圈(5)和一个或多个塞(6)。本发明还涉及一种飞行器机翼(2),该飞行器机翼包括通过所述方法施加的覆盖件(1),该覆盖件包括蒙皮(3)、一个或更多个垫圈(5)和一个或更多个塞(6)。这减少了施加时间、经常性成本并且具有积极的环境足迹影响。
Method for applying cover to aircraft wing and aircraft wing
用于将覆盖件施加到飞行器机翼的方法和飞行器机翼
2024-06-04
Patent
Electronic Resource
Chinese
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