THE RESEARCH AND DEVELOPMENT OF COMPOSITE LANDING GEAR FOR AN UNMANNED AERIAL VEHICLE (UAV)

Fiber Reinforced Plastics/Composites ›› 2017, Vol. 0 ›› Issue (6): 89-93.

• APPLICATION RESEARCH • Previous Articles Next Articles

THE RESEARCH AND DEVELOPMENT OF COMPOSITE LANDING GEAR FOR AN UNMANNED AERIAL VEHICLE (UAV)

ZHANG Guo-qi¹, HU Qi², WU Hai-sheng¹, GUAN Xin¹

1.Beijing Spacecrafts, Beijing 100094, China;
2.UAV Research Institute, China Aerospace Ninth Academy of Science and Technology Corporation, Beijing 100094, China

Received:2017-01-13 Online:2017-06-28 Published:2017-06-28

Abstract

Abstract: According to the main technical specifications for landing gear of an UAV, the composite foam sandwich is adopted based on the engineering formula and numerical simulation. In addition, the specific geometric parameter and stacking sequence are definitely determined. Furthermore, the specimen is fabricated by manual molding technology. The experimental results demonstrate that both the mechanical property and the weight of this specimen satisfy the requirement.

Key words: landing gear, composite, sandwich structure

CLC Number:

TB332

ZHANG Guo-qi, HU Qi, WU Hai-sheng, GUAN Xin. THE RESEARCH AND DEVELOPMENT OF COMPOSITE LANDING GEAR FOR AN UNMANNED AERIAL VEHICLE (UAV)[J]. Fiber Reinforced Plastics/Composites, 2017, 0(6): 89-93.

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THE RESEARCH AND DEVELOPMENT OF COMPOSITE LANDING GEAR FOR AN UNMANNED AERIAL VEHICLE (UAV)

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