Affiliation:
1. National Space Research & Development Agency (NASRDA)
Abstract
The 21st century aviation and aerospace technologies have evolved and become more complex and technical. Turbofan jet engines as well as their cousins, the rocket engines (liquid/solid) have gone through several design upgrades and enhancements during the course of their design and exploitation. These technological upgrades have made engines very complex and expensive machines which need constant monitoring during their working phase. As the demand and use of such engines is growing steadily, both in the civilian and military sectors, it becomes necessary to monitor and predict the behavior of parametric data generated by these complex engines during their working phases. In this paper flight parameters such as Exhaust Gas Temperature (EGT), Engine Fan Speeds (N1 and N2), Fuel Flow (FF), Oil Temperature (OT), Oil Pressure (OP), Vibration and others where used to determine engine fault. All turbo fan engines go through several distinctly different working phases: Take-off phase, Cruise phase and Landing phase. Recording generated parametric data during these different phases leads to a massive amount of in-flight data and maintenance reports, which makes the task of designing and developing a fault diagnostic system highly challenging. It becomes imperative to use modern techniques in data analysis that can handle large volumes of generated data and provide clear visual results for determining the technical status of the engine under investigation/monitoring. These modern techniques should be able to give clear and objective assessment of the object under investigation. Cluster analysis methods based on Neural Networks such as c-means, k-means, self-organizing maps and DBSCAN algorithm have been used to build clusters. Differences in cluster groupings/patterns between healthy engine and engine with degraded performance are compared and used as the bases for defining faults. Fault diagnosis plays a crucial role in aircraft engine management. Timely and accurate detection of faults is the foundation on which maintenance turnaround times, operational costs and flight safety are based. The data used in this paper for analysis was obtained from flight data recorder during one flight cycle. The final decision on a fault is taken by an engineer.
Publisher
Moscow State Institute of Civil Aviation
Reference11 articles.
1. Buraimah, I.J. (2015). Primenimosti neyrosetevykh algoritm k otsenke tekhnicheskogo sostoyaniya aviatsionnykh dvigateley [Application of the neural network algorithm for determining technical condition of aircraft engine]. Nauchnyye chteniya po aviatsii, posvyashchennyye pamyati N.Ye. Zhukovskogo: sbornik dokladov XII Vserossiyskoy nauchno-tekhnicheskoy konferentsii [12th Russian Scientific and Technical Conference, (technical reading on aviation), Dedicated to the memory of Ghukovski, N.E.], pp. 104–106. (in Russian).
2. DePold, H.R. and Gass, F.D. (1999). The application of expert systems and neural networks to gas turbine prognostics and diagnostics. ASME. Journal of Engineering for Gas Turbines and Power, vol. 121, issue 4, pp. 607–612. DOI: https://doi.org/10.1115/1.2818515
3. Polycarpou, M.M. (1994). An on-line approximation approach to fault monitoring, diagnosis, and accommodation. SAE Technical Paper 941217. DOI: https://doi.org/10.4271/941217
4. Merrigton, G.L. (1994). Fault diagnosis in gas turbines using a model-based technique. ASME Journal of Engineering for Gas Turbines and Power, vol. 116, issue 2, pp. 374–380. DOI: https://doi.org/10.1115/1.2906830
5. Gorinevsky, D., Nwadiogbu, E. and Mylaraswany, D. (2002). Model based diagnostics for small-scale turbomachines. Proceedings of the 41st IEEE Conference on Decision and Control, Las Vegas, NV, USA, vol. 4, pp. 4784–4789. DOI: 10.1109/CDC.2002.1185136
Cited by
1 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. POSSIBLE APPLICATIONS OF ARTIFICIAL INTELLIGENCE ALGORITHMS IN F-16 AIRCRAFT;Scientific Journal of Silesian University of Technology. Series Transport;2024-06-30