The large deformation problem of the Design and Performance Analysis of Axial Flux Permanent Magnet Machines with Double-Stator Dislocation Using a Combined Wye-Delta Connection wing with high aspect ratio cannot be avoided due to the large bending moment and poor torsional stiffness.The wing design follows the following procedure; firstly, the design indexes of high aspect ratio wing are preliminarily formulated referring to some parameters of the Predator UAV.Then, the aerodynamic analysis of the wing is performed, and the stress cloud diagram is obtained.Next, the finite element model of the wing is designed, and the static analysis is conducted in the ANSYS ACP module, and the unreasonable component size is changed.An appropriate thickness which is 12 mm Canine Dirofilariasis: A Case Report and Review of the Literature is selected as the final thickness of the wing.
Then, the analysis of laying methods of skin structure is conducted.Finally, the composite structure is proved to reduce the maximum deformation and maximum stress effectively compared with the metal wing.