| 摘要 |
The invention relates to a system which consists of mounting the wings (1) of an aircraft (2) in a hinged manner by means of hydraulic elements (13) hingedly mounted between the wing and the corresponding fuselage of the aircraft (2), in order to make it possible to vary the angle of attack of said wings (1), until achieving the necessary angle of attack which, in combination with the flaps (3) and slats (4) and complemented with the elevators in which the angle of attack is also increased in a precise manner, makes it possible to perform aircraft take-off and landing operations quickly and with very short runway requirements. |
