A method to minimize stage-by-stage initial unbalance in the aero engine assembly of multistage rotors-Reference-Cited by-同舟云学术

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A method to minimize stage-by-stage initial unbalance in the aero engine assembly of multistage rotors

Published:2019-02 Issue: Volume:85 Page:270-276
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Liu Yongmeng,Zhang Maowei,Sun Chuanzhi,Hu Ming,Chen Danyang,Liu Zewei,Tan Jiubin

Funder

National Natural Science Foundation of China

Natural Science Foundation of Heilongjiang Province

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference34 articles.

1. Review of design optimization methods for turbomachinery aerodynamics;Li;Prog. Aerosp. Sci.,2017

2. Experimental testing for the influences of rotation and tip clearance on the labyrinth seal in a compressor stator well;Kong;Aerosp. Sci. Technol.,2017

3. Effects of unbalance on the nonlinear dynamics of rotors with transverse cracks;Wang;Nonlinear Dyn.,2018

4. Inspection of assembly error with effect on throat and incidence for turbine blades;Chen;J. Manuf. Syst.,2017

5. Control of vibration and resonance in aero engines and rotating machinery – an overview;Ewins;Int. J. Press. Vessels Piping,2010

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2. A Prediction Model of Two-Sided Unbalance in the Multi-Stage Assembled Rotor of an Aero Engine;Machines;2024-07-24

3. Multi-objective optimization of aeroengine rotor assembly based on tensor coordinate transformation and NSGA-II;CIRP Journal of Manufacturing Science and Technology;2024-07

4. Assembly accuracy analysis and phase optimization of aero-engine multistage rotors considering surface morphology and non-uniform contact deformation;Precision Engineering;2024-06

5. Unbalance prediction method of aero-engine saddle rotor based on deep belief networks and GA-BP intelligent learning;Journal of Intelligent Manufacturing;2024-04-29

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