Skip to main content

Simplified Programming Design Based on Automatic Test System of Aeroengine

  • Conference paper
  • First Online:
  • 1277 Accesses

Part of the book series: Communications in Computer and Information Science ((CCIS,volume 1258))

Abstract

Aeroengine is a highly complex and repairable multi-component system, and operates over a long time under the harsh conditions of high temperature, high pressure, high speed and high load, and any faults threatening the safety of the aircraft. Based on this, through the in-depth analysis of several common automatic fault detection methods used in aeroengines, an automatic test system based on association rules mining technology is proposed to realize automatic test of aeroengine fault. The system used association rule mining algorithm to deal with the database with a large amount of data. By improving the algorithm, the algorithm can reduce the size of the database and the number of programming. The test results show that the hardware design of the automatic test system is reasonable, the signal acquisition is accurate and the error can meet the requirements; the design of the fault detection process is applicable, the search algorithm is fast and accurate, the speed of detection is about twice as high as possible, and the service life of the engine is saved.

This is a preview of subscription content, log in via an institution.

Buying options

Chapter
USD   29.95
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
eBook
USD   39.99
Price excludes VAT (USA)
  • Available as EPUB and PDF
  • Read on any device
  • Instant download
  • Own it forever
Softcover Book
USD   54.99
Price excludes VAT (USA)
  • Compact, lightweight edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info

Tax calculation will be finalised at checkout

Purchases are for personal use only

Learn about institutional subscriptions

References

  1. Li, Y.P., Li, W.: The design of the test control system of small piston aircraft engine. Adv. Mater. Res. 1061–1062, 912–915 (2015)

    Google Scholar 

  2. Qiongwei, L., Li, A., Li, X., et al.: Research on built-in metrology system for aircraft integrated automatic test equipment. In: International Conference on Electronic Measurement & Instruments, pp. 340–343. IEEE (2011)

    Google Scholar 

  3. Liu, L., Wang, S., Liu, D., et al.: Entropy-based sensor selection for condition monitoring and prognostics of aircraft engine. Microelectron. Reliab. 55(9–10), 2092–2096 (2015)

    Article  Google Scholar 

  4. Anstead, J.W.: Automatic testing of electronic equipment for aircraft. Radio Electron. Eng. 34(5), 269–275 (2010)

    Article  Google Scholar 

  5. Korsun, O.N., Poplavsky, B.K., Prihodko, S.J.: Intelligent support for aircraft flight test data processing in problem of engine thrust estimation. Procedia Comput. Sci. 103, 82–87 (2017)

    Article  Google Scholar 

  6. Zang, X.J., Deng, J.N.: Aircraft pneumatic accessories automatic test system based on configuration software. Meas. Control Technol. 32(7), 110–113 (2013)

    Google Scholar 

  7. Zheng, J., Xie, W.F., Viens, M., et al.: Design of an advanced automatic inspection system for aircraft parts based on fluorescent penetrant inspection analysis. Insight Non-Destr. Test. Condition Monit. 57(1), 18–34 (2015)

    Article  Google Scholar 

  8. Dimogianopoulos, D., Hios, J., Fassois, S.: Aircraft engine health management via stochastic modelling of flight data interrelations. Aeros. Sci. Technol. 16(1), 70–81 (2012)

    Article  Google Scholar 

  9. Côme, E., Cottrell, M., Verleysen, M., Lacaille, J.: Aircraft engine health monitoring using self-organizing maps. In: Perner, P. (ed.) ICDM 2010. LNCS (LNAI), vol. 6171, pp. 405–417. Springer, Heidelberg (2010). https://doi.org/10.1007/978-3-642-14400-4_31

    Chapter  Google Scholar 

  10. Lv, Y., Gang, Z.: UG-based research and development of 3D pipe layout system of the aircraft engine. Procedia Eng. 17, 660–667 (2011)

    Article  Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to Shuang Xia .

Editor information

Editors and Affiliations

Rights and permissions

Reprints and permissions

Copyright information

© 2020 Springer Nature Singapore Pte Ltd.

About this paper

Check for updates. Verify currency and authenticity via CrossMark

Cite this paper

Xia, S. (2020). Simplified Programming Design Based on Automatic Test System of Aeroengine. In: Qin, P., Wang, H., Sun, G., Lu, Z. (eds) Data Science. ICPCSEE 2020. Communications in Computer and Information Science, vol 1258. Springer, Singapore. https://doi.org/10.1007/978-981-15-7984-4_32

Download citation

  • DOI: https://doi.org/10.1007/978-981-15-7984-4_32

  • Published:

  • Publisher Name: Springer, Singapore

  • Print ISBN: 978-981-15-7983-7

  • Online ISBN: 978-981-15-7984-4

  • eBook Packages: Computer ScienceComputer Science (R0)

Publish with us

Policies and ethics