Patent ID: 6186854
Filing Date: 2001-02-13
Classification: A63H

Abstract:
An assembly structure for a tail wing of a model airplane, comprising:an airplane body having a tail section with a horizontal connecting face for connecting with a horizontal tail wing and a vertical tail fin, said vertical tail fin having a bottom face formed with a pair of rectangular sockets formed therein;first and second fixing rods each having a rectangular section respectively inserted in said pair of rectangular sockets, said rectangular section of each said fixing rod being disposed at an upper section thereof, a lower section of each of said fixing rods being formed with a cylindrical section and a bottom end of each of said fixing rods being formed with an axial hole;a pair of screws each fitted with a washer, each said screw being engaged in an axial hole of a respective fixing rod, said horizontal tail wing having a center portion formed with first and second through holes corresponding to said first and second fixing rods of said vertical tail fin;a first pair of sleeves respectively mounted in said first and second through holes, said horizontal connecting face of said tail section being formed with a pair of connecting through holes respectively corresponding to said first and second fixing rods installed in said vertical tail fin; and,a second pair of sleeves respectively mounted in said connecting through holes.