Abstract detail

123 / 2021-03-31 08:17:46
Dynamic Programming Method of Aeroengine Multi-stage Rotors Stacking Policy
Dynamic programming; Combinatorial optimization; Multi-object optimization; Rotors stacking policy; Reinforcement learning
Other related fields
Abstract Accepted
Jia Kang / Zhejiang University
Jun He / Zhejiang University
Zhisheng Peng / Hangzhou Steam Turbine & Power Group Co., Ltd
Haizhou Huang / Huadian Electric Power Research Institute Co., Ltd
Shixi Yang / Zhejiang University
Aeroengine high pressure compressor (HPC) multi-stage rotors assembly is stacked stage by stage by single rotor. The traditional stacking method is the trial assembly method, which usually requires multiple disassembly and assembly of rotors to ensure assembly precision, and the assembly process is cumbersome and may cause damage to parts. It is meaningful to optimize the multi-stage rotors stacking to improve the assembly quality and reduce aeroengine operational failure. The actual aeroengine HPC rotors assembly data is limited, according to the manufacture precision grade of rotors, this paper simulated the manufacture tolerance data of rotors through the Gaussian distribution and other methods, and simulated the assembly data through FEM. Aiming at the propagation and accumulation of assembly deviations in the stacking process of multi-stage rotors, based on the operational research analysis method, the bolts combination of rotors is regarded as a combinatorial optimization process, while the precision requirements of concentricity and perpendicularity of rotors are regarded as multi-object optimization, and the stacking dynamic programming model is established. With respect to the large computation to carry out the stacking dynamic programming model, the reinforcement learning algorithm is used to improve the computation speed and generate the stacking policy, and the effectiveness of stacking policy is demonstrated by FEM. This paper innovatively proposed a stacking dynamic programming method, which can generate reasonable optimal or near optimal stacking policy, and control the assembly precision of the aeroengine multi-stage rotors within the target range with single assembly. The research of this paper can be used to guide the actual stacking process of aeroengine multi-stage rotors.

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Important Dates

Abstract Submission Deadline:

 31st March 2021 15th April 2021

Extended Deadline: 1st Aug. 2022

 

Abstract Acceptance:

30th April  2021 Rollover

 

Full Paper Submission Deadline:

30th June 2021  14th July 2021

Extended Deadline: 15th Aug. 2022 

 

Notification of Acceptance:

15th August 2021 1st Sept. 2021

1st Sept. 2022

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