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Analysis of the impact response of the ship-borne drone blocking the fuselage in the ship

Xiong, Wenqiang ; Zhang, Run ; Zhang, Xiaoqing ; Zhu, Xiaolong ; Gao, Zongzhan ; Liu, Xiaoming ; He, Min ; Yao, Xiaohu

Hang kong xue bao, 2019-01, Vol.40 (12), p.97

Beijing: Chinese Society of Aeronautics and Astronautics

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  • Título:
    Analysis of the impact response of the ship-borne drone blocking the fuselage in the ship
  • Autor: Xiong, Wenqiang ; Zhang, Run ; Zhang, Xiaoqing ; Zhu, Xiaolong ; Gao, Zongzhan ; Liu, Xiaoming ; He, Min ; Yao, Xiaohu
  • Assuntos: Airframes ; Computer simulation ; Coupling ; Dynamic response ; Fuselages ; Ground motion ; Hooks ; Impact analysis ; Impact resistance ; Impact response ; Simulation ; Unmanned aerial vehicles
  • É parte de: Hang kong xue bao, 2019-01, Vol.40 (12), p.97
  • Descrição: Aiming at the strength problem of a carrier-based drone during the process of blocking the ship, the fuselage structure is the main research object, and for the first time, components including the middle fuselage structure and front and rear fuselage, wing fakes, and blocking hooks were designed. The ground blocking simulation test scheme and the corresponding device were set up. The ground response and rigid-flexible coupling simulation were used to analyze the dynamic response characteristics of the fuselage structure under the impact of blocking resistance during blocking. The test and simulation results show that the maximum heading overload of the middle fuselage attenuates along the two main transmission force paths from the rear fuselage to the front fuselage, and the overload peak at the lower transmission path point is significantly larger than the peak at the upper transmission path point; the maximum overload point was found It is located at the blocking joint, and the strain danger point is locat
  • Editor: Beijing: Chinese Society of Aeronautics and Astronautics
  • Idioma: Chinês
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