Abstract
As the aviation maintenance equipments and technology developing, commercial aircrafts apply central maintenance system (CMS) to improve traditional aircraft maintenance mode. In this paper, the functions, structures, and fault diagnosis methods are discussed. The CMS helps to improve the safety of aircraft and the maintenance efficiency. The fault diagnosis method based on logic equations is developed to meet the needs of CMS. The example is correct and effective.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
References
Wei W, Zhang B (2007) Evolution of aircraft maintenance systems (in Chinese). Int Aviat 3:42–45
Zhang B, Zeng T (2000) Intelligent BIT technologies (in Chinese). Meas Control Technol 11:1–4
Zhao R (2007) Preliminary research on CMS Based on modular integrated processing platform (in Chinese). Avionics Technol 38(1):20–25
Hess R, Due A, Kogut D (2001) The IMD HUMS as a tool for rotorcraft health management and diagnostics. In: IEEE aerospace conference proceedings, 2001
Ferrell BL (2000) Air vehicle prognostics and health management. In: IEEE aerospace conference proceedings, 2000
Author information
Authors and Affiliations
Corresponding author
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2014 Springer-Verlag Berlin Heidelberg
About this paper
Cite this paper
Guo, Jq., Song, D., Chen, Dy. (2014). The Research of the Fault Diagnosis Method Based on Logic Equations on Central Maintenance System. In: Wang, J. (eds) Proceedings of the First Symposium on Aviation Maintenance and Management-Volume I. Lecture Notes in Electrical Engineering, vol 296. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-54236-7_48
Download citation
DOI: https://doi.org/10.1007/978-3-642-54236-7_48
Published:
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-54235-0
Online ISBN: 978-3-642-54236-7
eBook Packages: EngineeringEngineering (R0)