The invention relates to a functionally improved fairing arrangement for a high lift mechanism of an aircraft. The high lift mechanism comprises a flap to be arranged at the trailing edge of the aircraft wing and a mounting and guiding mechanism for the flap. The fairing device comprises a flap side fairing unit and a wing side fairing unit. The flap-side cowl unit includes 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 includes 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 such that the wing-side cowl is rotatable about an axis oriented at least partially in a vertical direction.
本发明涉及一种用于飞行器的高升力机构的在功能上改进的整流罩装置。高升力机构包括待布置在飞行器机翼的后缘处的襟翼以及用于襟翼的安装和导引机构。整流罩装置包括襟翼侧整流罩单元和机翼侧整流罩单元。襟翼侧整流罩单元包括用于覆盖安装和导引机构的后部部分的襟翼侧整流罩以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。机翼侧整流罩单元包括用于覆盖安装和导引机构的前部部分的机翼侧整流罩以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,使得机翼侧整流罩能够围绕至少部分地沿竖向方向定向的轴线旋转。
Fairing device for high lift mechanism of aircraft
用于飞行器的高升力机构的整流罩装置
2024-06-21
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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