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Citation: WANG Suming, FENG Shiyu, LI Zongqi, et al. Numerical simulation and comparison of oxygen consumption inerting and hollow membrane inerting in fuel tank[J]. Journal of Beijing University of Aeronautics and Astronautics, 2020, 46(5): 1032-1038. doi: 10.13700/j.bh.1001-5965.2019.0332(in Chinese)

Numerical simulation and comparison of oxygen consumption inerting and hollow membrane inerting in fuel tank

doi: 10.13700/j.bh.1001-5965.2019.0332
Funds:

Open Fund of Graduate Innovation Base (Laboratory) of Nanjing University of Aeronautics and Astronautics kfjj20180101

The Priority Academic Program Development of Jiangsu Higher Education Institutions 

National Natural Science Foundation of China U1933121

More Information
  • Corresponding author: FENG Shiyu, E-mail:shiyuf@nuaa.edu.cn
  • Received Date: 25 Jun 2019
  • Accepted Date: 30 Aug 2019
  • Publish Date: 20 May 2020
  • To solve the problem of oxygen mole fraction changing with time in the upper space of oil tank of oxygen consuming inerting system. A mathematical model was established for the reaction process of the Green On-Board Inert Gas Generation System (GOBIGGS), and the inerting process of the GOBIGGS and the On-Board Inert Gas Generation System (OBIGGS) was simulated by CFD method. The simulation results were compared with the experimental data, which verifies the accuracy of the simulation results. The research results show that, when the flow rate of the exhaust gas from the fuel tank in the GOBIGGS is identical with that of the Nitrogen Enriched Air (NEA) in the OBIGGS, GOBIGGS not only has shorter inerting time than OBIGGS, but also reduces the oxygen mole fraction of the fuel tank to a lower level. The inerting effect of the GOBIGGS is similar to that of the OBIGGS of NEA0 (100%N2) under the same flow rate. GOBIGGS makes the upper oxygen mole fraction greater than the lower oxygen mole fraction in the gas phase space of the fuel tank, while OBIGGS is the opposite.

     

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