• CN: 11-2187/TH
  • ISSN: 0577-6686

Journal of Mechanical Engineering ›› 2023, Vol. 59 ›› Issue (1): 59-70.doi: 10.3901/JME.2023.01.059

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Reliability Optimization Design for Large Aerospace Planetary Mechanism Based on Hierarchical Finite Element

LI Ming1, LUO Yuan1, XIE Liyang2   

  1. 1. School of Mechatronics Engineering, Shenyang Aerospace University, Shenyang 110136;
    2. School of Mechanical Engineering and Automation, Northeastern University, Shenyang 110819
  • Received:2022-07-17 Revised:2022-10-26 Online:2023-01-05 Published:2023-03-30

Abstract: As the foundation and core of various heavy aircraft transmission systems, the reliability level of large-scale aviation planetary mechanism restricts the economic affordability and service safety for the aircraft to a great extent. A model of heavy helicopter planetary mechanism as the object of study, and aims to improve the fatigue reliability level of the system. The fatigue load history of the gear teeth under the coupling of global elastic behavior of the system is calculated using a hierarchical finite element method, and the probabilistic fatigue strength of gear teeth is fitted based on the gear low circumference fatigue test with the minimum order statistics transformation method to provide cost-effective load and strength input variables for the system reliability prediction model. Based on this, a mapping path from the key structural elements of large-scale aviation planetary mechanism to the system reliability indexes is established, and then a new method of reliability-driven multi-objective optimization design for planetary mechanism structural dimensions is proposed. Finally, the influence law of ring gear rim thickness and planet carrier baseplate thickness on the fatigue reliability of the planetary gear train is analyzed, and the results of the best stiffness matching between the rim and baseplate dimensions for the specified type of large aviation planetary mechanism can be obtained. The stiffness potential of the core structural elements is maximized as a way to balance the contradiction between reliability and lightweight requirements of large aviation planetary equipment.

Key words: planetary transmission, hierarchical analysis, finite element method, reliability modeling, fatigue test

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