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Volume 41 Issue 2
Feb.  2015
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Journal of Beijing University of Aeronautics and Astronautics  > 2015  >  41(2): 241-245.
LI Xianxue, DING Li, WANG Xingwei, et al. Comfort evaluation for aircraft seat cushion based on finite element model[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(2): 241-245. doi: 10.13700/j.bh.1001-5965.2014.0122(in Chinese)
Citation: LI Xianxue, DING Li, WANG Xingwei, et al. Comfort evaluation for aircraft seat cushion based on finite element model[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(2): 241-245. doi: 10.13700/j.bh.1001-5965.2014.0122(in Chinese)
shu

Comfort evaluation for aircraft seat cushion based on finite element model

doi: 10.13700/j.bh.1001-5965.2014.0122
  • 1.

    School of Biological Science and Medical Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • 2. Institute of Aviation Medicine of Air Force, Chinese People's Liberation Army, Beijing 100036, China

  • 3. School of Mechanical and Electrical Engineering, Taizhou Polytechnic College, Taizhou 225300, China

  • 4. China National Institute of Standardization, Beijing 100088, China

  • Received Date: 14 Mar 2014
  • Publish Date: 20 Feb 2015
    Abstract
  • The comfort of pilot's seat is highly demanded and the sitting pressure is a very important index to evaluate the seat comfort. A human-seat cushion finite element model including the pelvis was built to simulate the pressure distribution in the human-seat cushion interface and interior the human body, and finally to evaluate the comfort of the plane's seat. The simulation and experiment results were compared to verify the validity of the model, after that simulation under different overload accelerations was performed. By an analysis of the pressure distribution and maximum pressure, the simulation and experiment results are highly consistent and the maximum pressure is linearly dependent with the overload acceleration. The results show that the human-seat cushion model is validated and can be used to evaluate the comfort of different seat cushions under different overload accelerations.

     

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    • References(19)
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