The invention provides a fairing device for a high-lift mechanism of an aircraft, a high-lift system for the aircraft, an aircraft wing and the aircraft. The high lift mechanism has flaps and mounting and guiding mechanisms. The fairing device has a flap-side fairing unit and a wing-side fairing unit. The flap-side cowl unit has a flap-side cowl for covering the rear portion of the mounting and guiding mechanism and a flap-side cowl mount for mounting the flap-side cowl to the flap. The wing-side cowl unit has a wing-side cowl for covering the front portion of the mounting and guiding mechanism and a wing-side cowl mount for mounting the wing-side cowl to the wing. The wing-side cowl mount is configured for movably connecting the wing-side cowl to the wing. A fairing coupling couples the flap-side fairing and the wing-side fairing so as to transmit motion of the flap-side fairing to the wing-side fairing. The lateral or rotational movement of the wing-side fairing is thus controlled by the flap-side fairing.

    提供用于飞行器的高升力机构的整流罩装置、用于飞行器的高升力系统、飞行器机翼及飞行器。高升力机构有襟翼及安装和导引机构。整流罩装置有襟翼侧整流罩单元和机翼侧整流罩单元。襟翼侧整流罩单元有用于覆盖安装和导引机构的后部部分的襟翼侧整流罩及用于将襟翼侧整流罩安装至襟翼的襟翼侧整流罩安装件。机翼侧整流罩单元有用于覆盖安装和导引机构的前部部分的机翼侧整流罩及用于将机翼侧整流罩安装至机翼的机翼侧整流罩安装件。机翼侧整流罩安装件构造成用于将机翼侧整流罩可移动地连接至机翼。整流罩结合件联接襟翼侧整流罩和机翼侧整流罩以便将襟翼侧整流罩的运动传递至机翼侧整流罩。因此机翼侧整流罩的侧向或旋转运动由襟翼侧整流罩控制。


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    Title :

    Fairing device for high-lift mechanism of aircraft, high-lift system for aircraft, aircraft wing and aircraft


    Additional title:

    用于飞行器的高升力机构的整流罩装置、用于飞行器的高升力系统、飞行器机翼和飞行器


    Contributors:

    Publication date :

    2024-10-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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