The invention belongs to the field of
aviation structure strength analysis, and particularly relates to a dense rib type anti-
shock wave control
surface structure which comprises a control surface
skin, a connector support, a control surface front beam and a rib plate. The multiple sets of rib plates are distributed at equal intervals in a dense rib mode, the front beam is fixedly connected to the control surface
skin, the connector support is fixedly connected with the control surface front beam, and the rib plates are fixedly connected with the control surface
skin and the control surface front beam. The dense rib type
layout enables the control surface wall plates to form a continuous
supporting system, and the overall rigidity is remarkably improved.
Shock wave loads are cooperatively borne through the skin and the rib structures, and local sinking and buckling deformation of the skin are effectively restrained. Through dense rib type
layout innovation, the triple technical effects of rigidity improvement, strain control and displacement constraint of the control
surface structure under the
shock wave load are achieved, light weight, high safety and
engineering applicability are achieved at the same time, and the technical blank of
special design for
shock wave resistance of the aircraft control surface is filled up.