公开(公告)号：WO2013000577A2

公开(公告)日：2013-01-03

申请号：PCT/EP2012/002725

申请日：2012-06-28

Applicant: AIRBUS OPERATIONS GMBH ,  SCHLIPF, Bernhard ,  TRIEBL, Carsten

Inventor： SCHLIPF, Bernhard ,  TRIEBL, Carsten

CPC classification number: B64C9/02 ,  B64C3/50 ,  B64C9/22 ,  B64C9/24 ,  Y02T50/14 ,  Y02T50/32

Abstract: The invention pertains to an airfoil (10) with a main wing (12), with at least one high-lift body (14) that is arranged on the leading edge of the main wing (10) such that it can be moved between an initial adjusting position and a maximally changed adjusting position referred to the initial adjusting position, with at least one guide mechanism (16), by means of which the high-lift body (14) is movably coupled to the main wing (12), and with a driving device (50) for realizing adjusting movements of the high-lift body (14), wherein the guide mechanism (16, 26) features: - an adjusting lever arrangement with at least one adjusting lever (21, 41 ), wherein at least one adjusting lever of the adjusting lever arrangement is coupled to the high- lift body (14), - at least one first main wing lever (18, 38) that is coupled to the main wing (12) by means of a first main wing pivot joint (20, 30) and to the at least one adjusting lever (21, 41 ) by means of a first adjusting lever pivot joint (22, 42) such that an effective lever arm is formed between the first adjusting lever pivot joint and the high-lift body (14), - at least one second main wing lever (19, 39) that is coupled to the main wing (12) by means of a second main wing pivot joint (26, 46) and to the at least one adjusting lever (21, 41 ) by means of a second adjusting lever pivot joint (24, 44) such that an effective lever arm is formed between the second adjusting lever pivot joint and the first adjusting lever pivot joint (22, 42), as well as to a method for realizing adjusting movements of a high-lift body (14) relative to a main wing (12).

Abstract translation: 本发明涉及具有主翼（12）的翼型件（10），其具有布置在主翼（10）的前缘上的至少一个高升降体（14），使得其可在 具有至少一个导向机构（16）的初始调整位置和最初改变的调节位置（参照初始调节位置），高升降机构（14）可移动地联接到主翼（12），以及 具有用于实现所述高升降体（14）的调节运动的驱动装置（50），其中所述引导机构（16,26）的特征在于： - 具有至少一个调节杆（21,41）的调节杆装置，其中 所述调节杆装置的至少一个调节杆联接到所述高升降机构（14）， - 至少一个第一主翼杆（18,38），其通过第一 主翼枢转接头（20,30），并通过第一调节杆枢转接头连接到至少一个调节杆（21,41） （22,42），使得在所述第一调节杆枢转接头和所述高升程体（14）之间形成有效的杠杆臂， - 至少一个第二主翼杆（19,39），其连接到所述主翼 （12）通过第二主翼枢转接头（26,46）并通过第二调节杆枢转接头（24,44）连接到所述至少一个调节杆（21,41），使得有效的杠杆臂 形成在第二调节杆枢转接头和第一调节杆枢转接头（22,42）之间，以及用于实现相对于主翼（12）调节高升降体（14）的运动的方法。

公开(公告)号：WO2013000577A3

公开(公告)日：2013-01-03

申请号：PCT/EP2012/002725

申请日：2012-06-28

Applicant: AIRBUS OPERATIONS GMBH ,  SCHLIPF, Bernhard ,  TRIEBL, Carsten

Inventor： SCHLIPF, Bernhard ,  TRIEBL, Carsten

IPC: B64C3/50 ,  B64C9/24 ,  B64C9/22

Abstract: The invention pertains to an airfoil (10) with a main wing (12), with at least one high-lift body (14) that is arranged on the leading edge of the main wing (10) such that it can be moved between an initial adjusting position and a maximally changed adjusting position referred to the initial adjusting position, with at least one guide mechanism (16), by means of which the high-lift body (14) is movably coupled to the main wing (12), and with a driving device (50) for realizing adjusting movements of the high-lift body (14), wherein the guide mechanism (16, 26) features: - an adjusting lever arrangement with at least one adjusting lever (21, 41 ), wherein at least one adjusting lever of the adjusting lever arrangement is coupled to the high- lift body (14), - at least one first main wing lever (18, 38) that is coupled to the main wing (12) by means of a first main wing pivot joint (20, 30) and to the at least one adjusting lever (21, 41 ) by means of a first adjusting lever pivot joint (22, 42) such that an effective lever arm is formed between the first adjusting lever pivot joint and the high-lift body (14), - at least one second main wing lever (19, 39) that is coupled to the main wing (12) by means of a second main wing pivot joint (26, 46) and to the at least one adjusting lever (21, 41 ) by means of a second adjusting lever pivot joint (24, 44) such that an effective lever arm is formed between the second adjusting lever pivot joint and the first adjusting lever pivot joint (22, 42), as well as to a method for realizing adjusting movements of a high-lift body (14) relative to a main wing (12).