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2023 | OriginalPaper | Buchkapitel

A Kinematics Analysis of Actuation System Based on DCM Method

verfasst von : Yige Liu, Xiaohua Liu

Erschienen in: Proceedings of the International Conference on Aerospace System Science and Engineering 2021

Verlag: Springer Nature Singapore

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Abstract

The actuator system of gas turbine compressor is composed of several spatial linkages. This study aims to investigate the relationship between the deflection angle of Variable Stator Vane (VSV) and the stroke of hydraulic system using the Direction Cosine Matrix (DCM) method. The actuator system is divided into two parts, and the kinematic models are established respectively. In this work, a motion simulation is carried out to verify the theoretical model. The results show that the theoretical calculation results are completely consistent with the simulation results. This kinematic model can be applied to further optimization of actuation characteristics.

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Literatur
1.
Zurück zum Zitat Wirkowski P (2007) Influence of changes of axial compressor variable stator vanes setting on gas turbine engine work. In: V international scientifically-technical conference POLISH CIMAC Explo-Diesel & Gas Turbine’07, vol 2007, pp 511–518 Wirkowski P (2007) Influence of changes of axial compressor variable stator vanes setting on gas turbine engine work. In: V international scientifically-technical conference POLISH CIMAC Explo-Diesel & Gas Turbine’07, vol 2007, pp 511–518
2.
Zurück zum Zitat Liang S, Yin X, Wang H (2016) Parametric design of stator blade jointly adjusting mechanism based on ADAMS. Aeroengine 42(1):65–69. (in Chinese) Liang S, Yin X, Wang H (2016) Parametric design of stator blade jointly adjusting mechanism based on ADAMS. Aeroengine 42(1):65–69. (in Chinese)
3.
Zurück zum Zitat Yu J, Sun J, Ji F et al (2019) Motion analysis and optimization of jointly ad-justing mechanism of aero-engine stator vane. J Aerosp Power 34(6):1193–1200 Yu J, Sun J, Ji F et al (2019) Motion analysis and optimization of jointly ad-justing mechanism of aero-engine stator vane. J Aerosp Power 34(6):1193–1200
4.
Zurück zum Zitat Hu M, Zheng L (2014) Simulation analysis of single-stage variable stator vane system based on CATIA and ADAMS. Aeronauti Manuf Technol 22(8):98–101. (in Chinese) Hu M, Zheng L (2014) Simulation analysis of single-stage variable stator vane system based on CATIA and ADAMS. Aeronauti Manuf Technol 22(8):98–101. (in Chinese)
Metadaten
Titel
A Kinematics Analysis of Actuation System Based on DCM Method
verfasst von
Yige Liu
Xiaohua Liu
Copyright-Jahr
2023
Verlag
Springer Nature Singapore
DOI
https://doi.org/10.1007/978-981-16-8154-7_40

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