AIRLINER SHOVEL WITH DIVERGING OUTPUT EDGE.

摘要

Wind turbine blade with aerodynamic profile (5) with a leading edge (11), a trailing edge (13) and pressure and suction sides (19, 17) between the leading edge (11) and the trailing edge (13) which has at least a part of the wind turbine blade a region of the trailing edge (TER) whose cross section is increased in the direction of the trailing edge (13). Preferably, that region of the trailing edge (TER) has a "divergent" shape with a concave curved surface at its bottom.