Multistage rotational optimization using unified Jacobian–Torsor model in aero-engine assembly

S Ding, S **, Z Li, H Chen - Proceedings of the Institution of …, 2019 - journals.sagepub.com
For revolving components like compressor stages in aero-engine, it is critical to ensure that
the overall concentric performance of the assembly is extremely excellent to satisfy the …

Point-based solution using Jacobian-Torsor theory into partial parallel chains for revolving components assembly

S **, S Ding, Z Li, F Yang, X Ma - Journal of manufacturing systems, 2018 - Elsevier
Aero-engine rotors are mostly manufactured as an assembly of individual parts to keep
manufacturability and maintainability. Assembly deviations are unavoidable because of …

Assembly accuracy prediction and optimization of aero-engine rotor under the separation condition of assembly and measurement

M Li, Y Wang, Q Sun, X Mu - The International Journal of Advanced …, 2022 - Springer
The measurement and assembly of the aero-engine rotor are separated from each other,
which makes it difficult to keep the assembly datum consistent with the measurement datum; …

Improvement of location and orientation tolerances propagation control in cylindrical components assembly using stack-build assembly technique

L Wang, C Sun, J Tan, B Zhao, G Wan - Assembly Automation, 2015 - emerald.com
Purpose–This paper aims to provide an assembly method to improve cylindrical
components assembly quality. The proposed method not only could be applied to tolerance …

Research on multistage rotor assembly optimization methods for aeroengine based on the genetic algorithm

Y Chen, J Cui, X Sun, S Cui - Complexity, 2021 - Wiley Online Library
The coaxiality and unbalance are the two important indexes to evaluate the assembly quality
of an aeroengine. It often needs to be tested and disassembled repeatedly to meet the …

[HTML][HTML] A prediction model of two-sided unbalance in the multi-stage assembled rotor of an aero engine

L Song, Y Chen - Machines, 2024 - mdpi.com
In rotating machinery with a multi-stage assembled rotor, such as is found in aero engines,
any unbalance present will undergo unknown changes at each stage when rotating the …

An unbalance optimization method for a multi-stage rotor based on an assembly error propagation model

Y Chen, J Cui, X Sun - Applied Sciences, 2021 - mdpi.com
For the assembly of a multi-stage rotor, such as an aero-engine or gas turbine, the parts
need to be assembled optimally to avoid excessive unbalance. We propose a method to …

Novel optimization technique for variation propagation control in an aero-engine assembly

Z Yang, T Hussain, AA Popov… - Proceedings of the …, 2011 - journals.sagepub.com
This paper presents a novel optimization technique in straight-build assembly to control
variation propagation. The optimization technique is developed by minimizing the …

Semi-physical simulation of fan rotor assembly process optimization for unbalance based on reinforcement learning

H Zhang, M Wang, Z Li, J Zhou, K Zhang, X Ma… - Aerospace, 2022 - mdpi.com
An aero engine fan rotor is composed of a multi-stage disk and multi-stage blades.
Excessive unbalance of the aero engine fan rotor after assembly is the main cause of aero …

A vibration suppression method for the multistage rotor of an aero-engine based on assembly optimization

Y Chen, J Cui, X Sun - Machines, 2021 - mdpi.com
The assembly quality of the multistage rotor is an essential factor affecting its vibration level.
The existing optimization methods for the assembly angles of the rotors at each stage can …