The invention relates to a slat arrangement (2) for a wing of an aircraft (58), said arrangement (2) having a movable leading edge slat (4) and a connecting section (6), the leading edge slat (4) comprising a slat leading edge (5) and a slat trailing edge (10), the connecting section (6) comprising a receiving opening (16) for receiving the slat trailing edge (10), the connecting section (6) comprising an overhang (12) having a free end (13), the slat trailing edge (10) is designed to translate under the overhang (12), and wherein the tail region (18) of the slat (4) is configured to elastically deform by means of the overhang (12) when the slat trailing edge (10) is moved into the receiving opening (16).
提出了一种用于飞行器(58)的机翼的缝翼装置(2),所述装置(2)具有可动的前缘缝翼(4)和连接部段(6),其中,前缘缝翼(4)包括缝翼前缘(5)和缝翼后缘(10),其中,连接部段(6)包括用于接纳缝翼后缘(10)的接纳开口(16),其中,连接部段(6)包括具有自由端部(13)的悬伸部(12),其中,缝翼后缘(10)设计成在悬伸部(12)下方平移,并且其中,缝翼(4)的尾部区域(18)构造成当缝翼后缘(10)移动到接纳开口(16)中时借助悬伸部(12)而弹性变形。
Slat device for aircraft wing
用于飞行器机翼的缝翼装置
08.07.2022
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |