Abstract：In order to design and manufacture a lightweight, simple technology and affordable electric general
aircraft, a new method of composite structure design and verification is adopted. After analyzing the load transfer of the
aircraft, the model of the aircraft structure is built by CATIA and the strength of the aircraft structure is calculated by PATRAN/
NASTRAN. Based on the calculation, the composite layer design is optimized, and the drawings in two dimensions
are issued quickly. With a series of mechanical tests for the composite aircraft components and the aircraft, a test verification
method for fast testing the structure of light sport aircraft is formed. According to the characteristics of parts with different
types, different manufacturing processes are adopted, so that the production costs and cycle are controlled effectively.
The effectiveness of the results and the test data are proven on RX1E (Rui Xiang) aircraft with the satisfaction of the design
requirements.
顾 超，黄 俊，杨凤田. 电动通用飞机复合材料结构设计及验证技术[J]. 航空制造技术, 2017, 60(13): 93-99.
GU Chao, HUANG Jun, YANG Fengtian. Structure Design and Test Technology of Electric General Aircraft With Composite Materials. Aeronautical Manufacturing Technology, 2017, 60(13): 93-99.
2017, 
