Modularized wing angle aircraft

The invention relates to a modularized wing angle aircraft which comprises an aircraft body and an extension mounting frame module detachably arranged on the aircraft body, a plurality of composite wing modules are detachably arranged on the two sides of the extension mounting frame module, and each composite wing module comprises a wing body and a duct formed in the middle of the wing body. Connecting mechanisms are arranged on the left side and the right side of the wing main body, and one extension mounting frame module and the other composite wing module are selectively connected through the connecting mechanisms; the duct is communicated with the upper wing surface and the lower wing surface of the wing main body; a hybrid power module capable of providing lift force is arranged in the duct; the extension mounting frame module comprises a front rod, a rear rod and a side mounting plate; the front rod and the rear rod are arranged on the machine body side by side front and back, and the two sides of the f