The invention provides a suspension structure of a control surface of a large aircraft. The suspension structure of the control surface of the large aircraft is comprised of a hinged line load bearingstructure (1) and an
aerodynamic load bearing structure (2). Hinged line load is independently borne by the hinged line
load bearing structure (1), wherein the hinged line
load bearing structure (1)is comprised of box-shaped beams (11), bolt shafts (13), and an axial joint (12). The box-shaped beams (11) are arranged in a stabilizing plane (4), the bolt shafts (13) are arranged in the box-shapedbeams (11), and the axial joint (12) is arranged in the control surface (3).
Aerodynamic load is independently borne by the
aerodynamic load bearing structure (2), wherein the
aerodynamic load bearing structure (2) is comprised of a suspension support arm (21) and a suspension joint (22). The suspension support arm (21) is arranged in the stabilizing plane (4), and the suspension joint (22) is arranged in the control surface (3). The hinged line
load bearing structure (1) is arranged on the root portion of the control surface and the lower portion of the stabilizing plane, so that a large opening in the front of the control surface is avoided, and the aerodynamic efficiency of the control surface is enhanced; the box-shaped beams (11) are directly connected with butt joints on a
tail wing, the force transmission is simple and direct, and the weight is light; and through the combination of a
bushing and a bearing and a clearance which is arranged reasonably, different
degrees of freedom are released, and the work of each structure is non-interference and reliable.