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RESEARCH PAPER
Life prediction and risk assessment on the aircraft cable based on thermal damage features
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1
Nanjing University of Aeronautics and Astronautics, China
 
2
Civil Aviation Management Institute of China, China
 
 
Submission date: 2024-03-12
 
 
Final revision date: 2024-06-11
 
 
Acceptance date: 2024-07-26
 
 
Online publication date: 2024-07-26
 
 
Publication date: 2024-07-26
 
 
Corresponding author
Hongjuan Ge   

Nanjing University of Aeronautics and Astronautics, China
 
 
Eksploatacja i Niezawodność – Maintenance and Reliability 2024;26(4):191696
 
HIGHLIGHTS
  • Two types of thermal damage features are defined based on the mechanism of cable thermal damage.
  • Combined with FIDES and thermal damage influence factor, a more accurate cable life prediction method is proposed.
  • The cable dynamic risk model is constructed with radial melting rate.
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ABSTRACT
Aiming at the operational risk caused by melting of aircraft cable insulation layer, an aircraft cable safety analysis method based on thermal damage characteristics is proposed to accurately predict the life and dynamically assess the risk. Based on the mechanism of cable thermal damage, two types of damage characteristics including the thermal damage influence factor and the radial melting rate are defined, which characterizes the influence and degree of cable thermal damage. Use thermal damage influence factor to indicate that cable thermal damage accelerates cable failure, and a method of cable life prediction is proposed. Moreover, a dynamic risk assessment model for aircraft cable is constructed from two perspectives of thermal damage degree and failure probability. The results show that the cable life prediction method proposed owes higher accuracy and better applicability in different operating areas. The proposed risk assessment model is effective and the results are consistent with the experimental.
ACKNOWLEDGEMENTS
The authors would like to thank the referees for their valuable comments and useful suggestions that help them to greatly improve the paper, and the support from the China Scholarship Council, National Natural Science Foundation of China and the Civil Aviation Joint Research Fund of the Civil Aviation Administration of China under the project number U2233205 & U2133203 and the Postgraduate Research & Practice Innovation Program of Jiangsu Province under the project number KYCX23_0390.
eISSN:2956-3860
ISSN:1507-2711
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