COMPOSITE STRUCTURE DESIGN OF GEOMETRIC TWIST WING FOR UAV

Abstract

Abstract:

The exterior of geometric twist wing is contorted,so the manufacture of this wing is difficult.It is introduced the composite structure design of geometric twist wing for UAV in this paper.The technological design is skillful that it is jointly solidify composite structure comprised sandwich construction and spar caps,and then it is predigested the assembly harmony of parts of wing.This design has been applied in a UAV successfully,and the effect is all right.

Key words: wing, geometric twist, composite, jointly solidify, technological design

CLC Number:

V279

Zhang, Y. M., Zhao, P. F., Liu, B.. COMPOSITE STRUCTURE DESIGN OF GEOMETRIC TWIST WING FOR UAV[J]. Fiber Reinforced Plastics/Composites, 2010, 210(1): 60-62.

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COMPOSITE STRUCTURE DESIGN OF GEOMETRIC TWIST WING FOR UAV

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