The invention provides a design method for a vertical
tail docking structure. The design method is characterized in that an amount of single lug joints are respectively arranged at the root of a vertical
tail at two sides of a course, a same amount of double lug joints are correspondingly arranged at a docking structure of the vertical
tail, the diameters of holes in the single lug joints are equal to those of holes in the corresponding double lug joints, the axes of the holes are coaxial, bushes are pressed into docking through holes of the single lug joints and the double lug joints, and the single lug joints and the double lug joints are fixedly connected in a
bolt connection mode. According to the invention, docking between the box section of a vertical tail
composite material and
fuselage lugs is realized in multi-point docking manner, so connection
processing amount is reduced, connection
workload is reduced, docking weight is lowered down, assembling
workload is decreased, rapid docking between the vertical tail and a
fuselage is realized, and connection of a few points enables the purpose of docking to be achieved and requirements on usage of an
airplane to be met; thus, a
development period is shortened, production cost is reduced, and
maintainability and replaceability of a product are improved.