Your browser does not support JavaScript!
http://iet.metastore.ingenta.com
1887

access icon openaccess Safety design method of a civil aircraft cargo door actuation system

A safety design method of a civil aircraft cargo door actuation system has been listed in this study in order to fulfil the requirements of airworthiness throughout the product's life circle, in which a safety design process has been illustrated to show the entire process which will have an impact on the function design. A safety analysis method of fault tree analysis has been chosen to realise the purpose, which is based on the fault modes provided from failure modes and effects analysis and the system reliability prediction results. A design refinement has been made according to the analysis results in order to realise a high safety system.

References

    1. 1)
      • 7. Bristow, J.W., Irving, P.E.: ‘Safety factors in civil aircraft design requirements’, Eng. Fail. Anal., 2007, 14, pp. 459470.
    2. 2)
      • 6. Job, M.: ‘Air disaster’ (Aerospae Publications Pty. Ltd., Australia, 2001), vol. 1, pp. 127144.
    3. 3)
      • 2. Cheng, C.: ‘A thesis in safety technology and engineering’, Nanjing University of Aeronautics, 1028707 09-0021.
    4. 4)
      • 14. Zheng, L.: ‘Design and implementation of fault detection system based on dynamic fault tree’ (Harbin Engineering University, People's Republic of China, 2017).
    5. 5)
      • 8. Guofang, Z.: ‘Study on a safety quantitative analysis method of civil airplane reckoning with wire failures’, Adv. Aeronaut. Sci. Eng., 2012, (2), pp. 241246.
    6. 6)
      • 5. Qiaojun, C.: ‘A preliminary aircraft safety assessment research based on aircraft structure’, Sci. Technol. Innov. Herald, 2015, 36, pp. 4144.
    7. 7)
      • 11. SAE-ARP4761: ‘Guidelines and methods for conducting the safety assessment process on civil airborne systems and equipment’, Society of Automotive Engineers, December 1996.
    8. 8)
      • 9. Lei, L.: ‘Research on system preliminary safety assessment of civil aircrafts’, Sci. Technol. Innov. Herald, 2015, 22, pp. 2829.
    9. 9)
      • 10. SAE-ARP4754A REV A: ‘Guidelines for Development of Civil Aircraft and Systems’, SAE Aerospace, December 2010.
    10. 10)
      • 3. Kelin, Z.: ‘Airwothiness considerations of landing gear control system design of civil aircraft’, Sci. Technol. Innov. Herald, 2011, 29, pp. 4244.
    11. 11)
      • 12. Jian, Y., Zhenjin, N., Xin, W., et al: ‘Cargo door electromechanical actuation system design on load matching’, Aerosp. Manuf. Technol., 2019, 4, (2), pp. 2327.
    12. 12)
      • 1. Qiang, Q.: ‘Safety and reliability analysis for the doors of civil aircraft’ (Northwestern Polytechnical University, People's Republic of China, 2016).
    13. 13)
      • 15. Dobrivoje, C., Milomir, G., Mile, S., et alFault tree analysis of hydraulic power-steering system’, Int.J.Veh. Des., 2014, 64, (1), pp. 2645.
    14. 14)
      • 4. Yunwen, F., Xionghua, Y., Xiaofeng, X., et al: ‘Rearch of safety analysis of doors of civil aircraft’, J. Northwesten Polytechnical Univ., 2013, 31, (5), pp. 803809.
    15. 15)
      • 13. Ortmeier, F., Schellhorn, G.: ‘Formal fault tree analysis-practical experiences’, Electron. Notes Theor. Comput. Sci., 2007, 185, pp. 139151.
http://iet.metastore.ingenta.com/content/journals/10.1049/joe.2020.0051
Loading

Related content

content/journals/10.1049/joe.2020.0051
pub_keyword,iet_inspecKeyword,pub_concept
6
6
Loading
This is a required field
Please enter a valid email address