The invention relates to a
delta wing manpower aircraft with
flapping wings. The
delta wing manpower aircraft comprises a
delta wing (1), a hanging frame (3), a pair of
flapping wings (2) and a pair of pull rod frames (4). The hanging frame (3) further comprises a pair of front suspenders (20), a rear suspender (21), a
butt joint frame (5) and a hung frame (6). Each single-face
flapping wing (2) in the pair of flapping wings (2) further comprises a
flapping wing frame (9), a net (10), fan blades (11), guide blades (12), traction wires (13) and short struts (14). Each single pull rod frame (4) in the pair of pull rod frames (4) further comprises two pull rods (7), a middle transverse rod (17) and a transverse rod as both the lower edge and a
handle (8). The hanging frame (3) is hung on a
keel (15) of the delta wing (1). The pair of flapping wings (2) are symmetrically arranged on the left side and the right side of the
butt joint frame (5) of the hanging frame (3). The pair of pull rod frames (4) are movably connected to an outside edge portion (27) of the pair of flapping wings (2). In operation, the pull rod frames are pulled with manpower to drive the flapping wings to flap up and down like bird wings, and enough flight power is supplied to the delta wing through the flapping wings conducting the flapping action.