The invention relates to a door fairing for an aircraft landing gear leg, in particular a door fairing (300) for a retractable landing gear leg of an aircraft, the door fairing having an outer member (330) which covers a portion of a landing gear compartment of the aircraft when the landing gear leg is retracted. An inner member (310) of the door cowl (300) is coupled to an outer member (330) via a plurality of configurable couplings (350, 360, 370, 380, 390) that allow for adjustment of the position of the outer member (330) relative to the inner member (310). The inner member (310) has a mounting point (315, 320) for mounting the door fairing (300) to the landing gear leg. The configurable couplings (350, 360, 370, 380, 390) are adjusted using measured or derived size parameters of the landing gear bay prior to fitting the hatch fairing (300) at the aircraft such that the hatch fairing (300) is pre-configured to match the landing gear bay of the aircraft.
本发明涉及一种用于飞行器起落架支腿的舱门整流罩、特别是用于飞行器的可伸缩起落架支腿的舱门整流罩(300),舱门整流罩具有外部构件(330),该外部构件在起落架支腿缩回时将飞行器的起落架舱的一部分覆盖。舱门整流罩(300)的内部构件(310)经由多个可配置的联接件(350、360、370、380、390)联接至外部构件(330),多个可配置的联接件允许调节外部构件(330)相对于内部构件(310)的位置。内部构件(310)具有用于将舱门整流罩(300)安装至起落架支腿的安装点(315、320)。在将舱门整流罩(300)配装在飞行器处之前,使用测量或导出的起落架舱的尺寸参数来调节可配置的联接件(350、360、370、380、390),使得舱门整流罩(300)被预先配置为匹配该飞行器的起落架舱。
Cabin fairing for aircraft landing gear leg
用于飞行器起落架支腿的舱门整流罩
2023-12-12
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |