CENTRAL PANEL OF WING FOR AIRCRAFT AND METHOD OF ITS CONTROL Russian patent published in 2019 - IPC B60F5/02 B64C3/56 

FIELD: aviation.

SUBSTANCE: invention relates to aircraft engineering, particularly, to wings. Central wing panel has front frame section and rear frame section connected by one or more traverses. Central wing panel can also have a first vertical axis and a second vertical axis located adjacent to the front ends of the front frame section, wherein the first and second wings are configured to rotate about the first and second vertical axes. Central wing panel can additionally have a first horizontal axis located parallel along lower fragment of front frame section, wherein the wing central panel is configured to turn about the first horizontal axis, providing the possibility of adjusting the wing angle of the vehicle wing. Central panel of wing may also have second horizontal axis extending along lower fragment of rear frame section, wherein rear frame section is configured to turn about second horizontal axis for connection and disconnection of rear frame section from wings.

EFFECT: enabling control of wing angle and ailerons.

16 cl, 8 dwg