TY - GEN
T1 - Aero-engine life limit parts replacement policy optimization
T2 - 2020 Asia-Pacific International Symposium on Advanced Reliability and Maintenance Modeling, APARM 2020
AU - Lin, Lin
AU - Liu, Jie
AU - Liu, Jinshan
AU - Zhong, Shisheng
AU - Guo, Feng
N1 - Publisher Copyright:
© 2020 IEEE.
PY - 2020/8
Y1 - 2020/8
N2 - An optimization method for aero-engine life limit parts (LLPs) replacement policy is proposed based on reinforcement learning method, aiming at optimizing the aero-engine LLP-s replacement policy. In the proposed LLPs replacement policy optimization method, the real-life LLPs replacement rules are adopted as the constraints and the minimum long-term LLPs replacement discount cost is regarded as the optimization objective. In reinforcement learning framework, the Q-learning algorithm is adopted to optimize the LLPs replacement policy. Compared with the traditional methods, the proposed optimization method is simple in structure, and it can achieve better optimization results. To validate the proposed aero-engine LLPs replacement policy optimization method, the LLPs list of a civil turbofan aero-engine is adopted as the sample data. And the existing particle swam optimization algorithm is adopted as the comparative experimental method. The comparison experiment results show that the proposed LLPs replacement policy optimization method achieves obvious advantages. The proposed optimization method is able to provide decision-making supports for aero-engine LLPs replacement.
AB - An optimization method for aero-engine life limit parts (LLPs) replacement policy is proposed based on reinforcement learning method, aiming at optimizing the aero-engine LLP-s replacement policy. In the proposed LLPs replacement policy optimization method, the real-life LLPs replacement rules are adopted as the constraints and the minimum long-term LLPs replacement discount cost is regarded as the optimization objective. In reinforcement learning framework, the Q-learning algorithm is adopted to optimize the LLPs replacement policy. Compared with the traditional methods, the proposed optimization method is simple in structure, and it can achieve better optimization results. To validate the proposed aero-engine LLPs replacement policy optimization method, the LLPs list of a civil turbofan aero-engine is adopted as the sample data. And the existing particle swam optimization algorithm is adopted as the comparative experimental method. The comparison experiment results show that the proposed LLPs replacement policy optimization method achieves obvious advantages. The proposed optimization method is able to provide decision-making supports for aero-engine LLPs replacement.
KW - Q-learning algorithm
KW - aero-engine
KW - life limit part
KW - reinforcement learning
KW - replacement policy
UR - https://www.scopus.com/pages/publications/85093980195
U2 - 10.1109/APARM49247.2020.9209367
DO - 10.1109/APARM49247.2020.9209367
M3 - 会议稿件
AN - SCOPUS:85093980195
T3 - 2020 Asia-Pacific International Symposium on Advanced Reliability and Maintenance Modeling, APARM 2020
BT - 2020 Asia-Pacific International Symposium on Advanced Reliability and Maintenance Modeling, APARM 2020
PB - Institute of Electrical and Electronics Engineers Inc.
Y2 - 20 August 2020 through 23 August 2020
ER -