WING CLAMP AND WING LIFTING DEVICE

Abstract

The invention of a wing clamp and wing lifting device. The wing clamp (100) includes: the main frame (120); wing clamping mechanisms made at both ends of the main frame (120) and used to clamp the wing (l); the wing clamping mechanisms are mounted in a rotating manner with respect to the main frame (120) to adjust the tilt control angle of the wing; the tilt control drive component (141), which drives the wing clamping mechanisms to rotate relative to the main frame (120); guide rails (142) made on one of the wing clamping mechanisms and the main frame (120); and rail grooves (143) made on the remaining component of the wing clamping mechanisms and the main frame (120) and capable of moving relative to the guide rails (142). Thanks to the wing clamping and lifting mechanism, tilt control can be performed on the wing during the wing lifting process, allowing for convenient wing installation.