Experiment and analysis of mechanical properties of carbon fiber composite laminates under impact compression

Author:

Yang Kang1,Yang Li2,Gong Peng3,Zhang Liguo4,Yue Yumei4,Li Qunfang1

Affiliation:

1. Design Department, Liaoning General Aviation Academy , Shenyang 110136 , China

2. Manufacturing Inspection Office, Shenyang Aircraft Airworthiness Certification Center of Civil Aviation of China , Shenyang , 110043 , China

3. College of Automation, Shenyang Aerospace University , Shenyang 110136 , China

4. College of Aerospace Engineering, Shenyang Aerospace University , Shenyang 110136 , China

Abstract

Abstract Composite materials are more and more widely used in aircraft structural design, and impact damage is the most serious defect/damage form of aviation composite structures in service. Therefore, it is of great significance to study the impact resistance of composites with different materials and structural forms for aircraft structural design. In this article, the damage of reinforced fiber/resin composite laminates with unidirectional carbon fiber prepreg (UIN23100), carbon fiber woven fabric (W-3021FF), and carbon fiber-aramid fiber blended fabric (W-38211) under the same impact energy were studied. The impact damage area was scanned and analyzed by ultrasonic C-scan, and the impact resistance of the three laminates were obtained. Finally, the compression bearing capacity of carbon fiber laminates after impact was tested, and the compression failure mode of each material has been analyzed. The results show that the impact resistance of carbon fiber unidirectional prepreg was stronger than that of carbon fiber woven fabric; the compression bearing capacity of carbon fiber laminate after impact was higher than that of carbon fiber unidirectional prepreg; the post impact bearing capacity of W-38211 was higher than that of W-3021FF.

Publisher

Walter de Gruyter GmbH

Subject

Polymers and Plastics,Physical and Theoretical Chemistry,General Chemical Engineering

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