披露了一种飞行器的飞行控制面、制造飞行控制面的方法和飞行器,所述飞行控制面包括:‑主体(1),所述主体包括:上覆盖件和下覆盖件(3,4),上蒙皮和下蒙皮(5,6,7,8)和芯部构件(9,10),所述蒙皮长度上的延长部(12),所述延长部超过所述芯部构件的长度,从而限定了台阶区域(16),‑后缘(2),所述后缘包括包绕所述延长部的U形型材(11),‑所述U形型材在弦向方向上向所述主体延伸直至所述台阶区域,并且包括逐渐减小的截面,所述后缘包括位于所述延长部中的第一组和第二组铆钉(13,14),所述第一组铆钉联结所述上覆盖件和所述下覆盖件,并且所述第二组铆钉联结所述U形型材与所述上覆盖件和所述下覆盖件。
Flight control surface comprising:- a main body (1) comprising an upper and lower cover (3, 4), upper and lower skins (5, 6, 7, 8) and a core member (9, 10), a prolongation (12) of their length over the length of the core member (9, 10) defining a stepped area (16),- a trailing edge (2) comprising a U-shaped profile (11) enclosing the prolongation (12),- the U-shaped profile (11) extending towards the main body in the chordwise direction up to the stepped area (16) and comprising a section that progressively decreases,the trailing edge (2) comprising a first and a second set of rivets (13, 14) located in the prolongation (12), the first set of rivets (14) joining the upper (3) and lower (4) covers and the second set of rivets (13) joining the U-shaped profile (11), the upper (3) and lower (4) covers.
飞行器的飞行控制面、制造飞行控制面的方法和飞行器
2024-07-19
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |