• RELIABILITY • Previous Articles
HOSSEIN T, ANDER B, RICHARD B, et al Successes and challenges in non-destructive testing of aircraft composite structures. Chinese Journal of Aeronautics, 2020, 33 (3): 771- 791.
|2||ZHAO S, ZHANG P. Study on maintenance interval control of heat exchanger in aircraft systems based on MSG-3 philosophy. Proc. of the 31st China Control and Decision Conference, 2019. DOI: 10.1109/CCDC.2019.8833075.|
|3||LIU S J, ZHONG R C, YAN Z Q. Analysis and research on MSG-3 of modern civil aircraft composite material structure. China High-Tech Enterprises, 2016, 9: 7−9. (in Chinese)|
|4||Airworthiness standards: transport category airplane. Washington DC: U.S. Department of Transportation Federal Aviation Administration, 2015.|
|5||ZHENG X L. Composite structure design and certification of the civil aircraft. Shanghai: Shanghai Jiao Tong University Press, 2011. (in Chinese).|
CAI J, LI X, CHEN X Joint optimization of maintenance inspection and spare provisioning for aircraft deteriorating parts. Journal of Systems Engineering and Electronics, 2017, 28 (6): 1133- 1140.
|7||CAI Y S Research on the differences of damage rating between metal & composite civil aircraft structure. Aeronautical Science & Technology, 2016, 27 (8): 21- 26.|
|8||SUN X S. Civil aircraft structural strength stiffness design and verification guide. Beijing: Aviation Industry Press, 2012. (in Chinese)|
ALDERLIESTEN R C, HOMAN J J Fatigue and damage tolerance issues of Glare in aircraft structures. International Journal of Fatigue, 2006, 28 (10): 1116- 1123.
|10||CHENG X Q, WU X R Methods for improving damage tolerance of composite laminates after low velocity impact and their influence factors. Polymer Materials Science & Engineering, 2002, 18 (3): 20- 25.|
|11||HUANG F Study on the compression after impact behavior of two composite materials. Science Technology and Engineering, 2015, 15 (7): 158- 160.|
CHEN X, REN H, BIL C Inspection intervals optimization for aircraft composite structures considering dent damage. Journal of Aircraft, 2014, 51 (1): 303- 309.
LIN K Y, STYUART A V Probabilistic approach to damage tolerance design of aircraft composite structures. Journal of Aircraft, 2007, 44 (4): 1309- 1317.
|14||CHEN X. Scheduled maintenance optimization of aircraft structures considering uncertainty and structural health monitoring. Melbourne, Australia: Royal Melbourne Institute of Technology University, 2014.|
|15||USHAKOV A, STEWART A, MISHULIN I, et al Probabilistic design of damage tolerant composite aircraft structures. Washington DC: Office of Aviation Research, 2002.|
|16||USHAKOV A, STEWART A, MISHULIN I, et al. Probabilistic design of damage tolerant composite aircraft structures, DOT/FAA/AR-01/55. Washington DC: Office of Aviation Research, 2002.|
|17||MIL-HDBK-17-3F. Composite materials handbook, volume 3: polymer matrix composites materials usage, design, and analysis, Department of Defense. 2002.|
|18||KAN H P. Enhanced reliability prediction methodology for impact damaged composite structures, DOT/FAA/AR-97/79. Washington DC: Office of Aviation Research, 1998.|
|19||JIA X S, CHENG Z H The development trend of reliability centered maintenance (RCM). Journal of Ordnance Engineering College, 2016, 14 (4): 29- 32.|
|20||ZHANG L. Numerical analysis and experimental study on propagation behavior of laminated composite plates with embedded delamination. Harbin: Harbin Institute of Technology, 2012. (in Chinese)|
|21||U.S. Department of Transportation Federal Aviation Administration. Composite aircraft structure, AC 120-107B. 2009.|
|22||XIAO S S. Probabilistic assessment methodology of impact damage tolerance for composite aircraft structures. Nanjing: Nanjing University of Aeronautics and Astronautics, 2013. (in Chinese)|
|23||XIAO S S, CHEN P H, SHEN W, et al Experimental study and analysis on probability of detection for impact damage of composite structures. Acta Materiae Compositae Sinica, 2013, 30 (4): 231- 237.|
|24||SHAO C J. Research on the method to determine the inspection interval and evaluate the repair tolerance of composite structure. Nanjing: Nanjing University of Aeronautics and Astronautics, 2018. (in Chinese)|
|25||HUANG C K, LIN K Y. A method for reliability assessment of aircraft structures subject to accidental damage. Proc. of the 46th AIAA/ASME/ASCE/AHS/ASC Structure, Structural Dynamics & Materials Conference, 2016. DOI: 10.2514/6.2005-1830.|
|26||REN H L, Simulation of failure process and residual strength of composite laminates with low velocity impact damage under compressive load. Xi ’an: Northwestern Polytechnical University, 2001. (in Chinese)|
|27||European Aviation Safety Agency. Certification specifications and acceptable means of compliance for large aeroplanes, CS 25. 2012.|
|28||REN H, CHEN X, CHEN Y. Inspection interval optimization for aircraft composite structures considering dent damage. Reliability Based Aircraft Maintenance Optimization and Applications, 2017, 51(1): 133–152.|
CHEN X, REN H, BIL C, et al Repair tolerance analysis for composite structures using probabilistic methodologies. Journal of Aircraft, 2014, 51 (6): 1997- 2004.
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