Effect of solar radiation on thermal comfort in civil aircraft cabin

被引:0
|
作者
Pang L. [1 ,2 ]
Li H. [1 ]
Wang T. [3 ]
Fan J. [4 ]
Zou L. [1 ]
机构
[1] School of Aeronautic Science and Engineering, Beihang University, Beijing
[2] School of Aero-engine, Shenyang Aerospace University, Shenyang
[3] School of Economic and Management, Shenyang Aerospace University, Shenyang
[4] Army Air Force Research Institute, Beijing
关键词
CFD dynamic simulation; Quantitative analysis; Real-time measurement; Solar radiation; Thermal comfort;
D O I
10.13700/j.bh.1001-5965.2019.0056
中图分类号
学科分类号
摘要
The requirement of thermal comfort for passengers is constantly increasing, which puts forward more urgent requirements for the overall thermal comfort of civil aircraft cabin. Based on the actual measurement of flights flying from north to south, it is found that the temperature distribution on both sides of the cockpit is extremely uneven due to the influence of solar radiation, especially around the windows, the average temperature difference reaches 20℃, and the thermal comfort on both sides of the cockpit is quite different. Combined with the CFD dynamic simulation, based on the actual situation, the thermal comfort of the cockpit on both sides of the cockpit is quite different. Real-time measurements of temperature and thermal comfort PMV in the cabin of civil aircraft are reproduced by setting up a simulation model of equal proportion cabin. The simulation boundary condition is temperature and pressure data measured in practice. The theoretical basis for quantitative analysis of thermal comfort in the cabin of north-south flights is provided. © 2019, Editorial Board of JBUAA. All right reserved.
引用
收藏
页码:1924 / 1930
页数:6
相关论文
共 17 条
  • [1] Rancesca R.D.A., Boris I.P., Giuseppe R., Notes on the calculation of the PMV index by means of Apps, Energy Procedia, 101, pp. 249-256, (2016)
  • [2] Hasan M.H., Alsaleem F., Rafaie M., Sensitivity study for the PMV thermal comfort model and the use of wearable devices biometric data for metabolic rate estimation, Building and Environment, 110, pp. 173-183, (2016)
  • [3] Shen C., Yu N., Study of thermal comfort in free-running buildings based on adaptive predicted mean vote, International Conference on E-Product E-Service and E-Entertainment, pp. 1-4, (2010)
  • [4] Marcel S., Andreas W., A framework for an adaptive thermal heat balance model (ATHB), Building and Environment, 94, pp. 252-262, (2015)
  • [5] Beck P., Rollet S., Latocha M., Et al., TEPC reference measurements at aircraft altitudes during a solar storm, Advances in Space Research: The Official Journal of the Committee on Space Research(COSPAR), 36, 9, pp. 1627-1633, (2005)
  • [6] PPG quick-application windshield coating kit available for general aviation, Aviation Maintenance, 60, 10, pp. 66-68, (2010)
  • [7] Lv M.Y., Yao Z.B., Zhang L.C., Et al., Effects of solar array on the thermal performance of stratospheric airship, Applied Thermal Engineering, 124, pp. 22-33, (2017)
  • [8] Battistoni G., The FLUKA code, galactic cosmic ray and solar energetic particle events: From fundamental physics to space radiation and commercial aircraft doses, IEEE Nuclear Science Symposium Conference Record, pp. 1609-1615, (2008)
  • [9] Hei S.G., Jiang S.G., Yang J., Et al., Development and applicability analysis of Fanger PMV thermal comfort model, Cryogenic Building Technology, 39, 10, pp. 125-128, (2017)
  • [10] Yang J.Z., Zhang Z.B., Chen X.Y., Et al., Experimental study on temperature disturbance in aircraft cockpit, Science and Technology and Engineering, 17, 31, pp. 364-368, (2017)