Device for the continuous adjustment, in flight, of the inclination of the wing structure in an ultralight aircraft of the pendular type.

摘要

In order to adjust the angular position of the structure (107,207,307) of the wing profile with respect to the carriage (105,305) (and hence the lift value), provision is made for a transmission which can be operated in flight via a servomechanism (318) and is designed to modify the angle of attack of the wing profile with respect to the carriage, about a transverse hinging axis (110,210,310). <IMAGE>