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Simulation and Analysis of Crashworthiness of Fuel Tank for Helicopters

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【Author】 LUO Chenga, LIU Huaa, YANG Jia-ling a,*, LIU Kai-xinb aInstitute of Solid Mechanics, Beijing University of Aeronautics and Astronautics, Beijing 100083, China bDepartment of Mechanics and Engineering, Peking University, Beijing 100871, China

【摘要】 Crashworthiness requirement of fuel tanks is one of the important requirements in helicopter designs. The relations among the protection frame, textile layer and rubber layer of the fuel tank are introduced. Two appropriate FE models are established, one is for an uncovered helicopter fuel tank without protection frame, and the other is for fuel tank with protection frame. The dynamic responses of the two types of fuel tanks impinging on the ground with velocities of 17.3 m/s are numerically simulated for the purpose of analyzing energy-absorbing capabilities of the textile layer and protection frame. The feasibility of the current crashworthiness design of the fuel tank is examined though comparing the dynamic response behaviors of the two fuel tanks.

【Abstract】 Crashworthiness requirement of fuel tanks is one of the important requirements in helicopter designs. The relations among the protection frame, textile layer and rubber layer of the fuel tank are introduced. Two appropriate FE models are established, one is for an uncovered helicopter fuel tank without protection frame, and the other is for fuel tank with protection frame. The dynamic responses of the two types of fuel tanks impinging on the ground with velocities of 17.3 m/s are numerically simulated for the purpose of analyzing energy-absorbing capabilities of the textile layer and protection frame. The feasibility of the current crashworthiness design of the fuel tank is examined though comparing the dynamic response behaviors of the two fuel tanks.

【关键词】 fuel tank; crashworthiness; helicopter; FEM;
【Key words】 fuel tank; crashworthiness; helicopter; FEM;
【基金】 Foundation items: NSFC Key Project (10532020); Engineering Research Institute, Peking University (ERIPKU) (204038)
  • 【文献出处】 Chinese Journal of Aeronautics ,中国航空学报(英文版) , 编辑部邮箱 ,2007年03期
  • 【分类号】V228
  • 【被引频次】9
  • 【下载频次】98
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