Liu Xiyang Senior Engineer
Address: Tsinghua University, Haidian District, Beijing
Postal Code: 100084
Email: liuxiyang@tsinghua.edu.cn
Educational Background
March 2004 - July 2009 Graduate School of Chinese Academy of Sciences Doctoral Degree
September 2001 - March 2004 Beihang University Master's Degree
September 1997 - July 2001 Beihang University Bachelor's Degree
Work Experience
December 2019 - Present Institute for Aero Engine, Tsinghua University Senior Engineer
December 2012 - December 2019 Institute of Engineering Thermophysics, Chinese Academy of Sciences Senior Engineer
July 2009 - December 2012 Institute of Engineering Thermophysics, Chinese Academy of Sciences Assistant Researcher
Research Field
Aero-engine / Gas Turbine
Research Overview
I have extensive experience in researching aero - engines and gas turbines, with a focus on three main areas: the design of high - load compressors, numerical simulation of three - dimensional viscous flow in turbomachinery, and the overall design of engines.
In the field of key technologies, I have conducted research on the design of high - load vaneless counter - rotating compressors and the design and verification of two - stage centrifugal compressors. These studies aimed to improve the performance and efficiency of relevant components.
Regarding overall engine development, I served as the technical director for the development of a 100kW gas turbine project. In this role, I led the team through the entire development process, from initial design to the final stage of experimental verification, successfully validating the feasibility of the gas turbine design.
Academic Achievements
Main Patent Achievements
1. A Device and Optimized Control Method for Preventing Cold and Hot Hanging during the Starting Process of a Gas Turbine, 2018, 4th Author, Patent Number: ZL 201610305787.1
2. A Method and Device for Real-time Fuel Control during the Starting Process of a Gas Turbine, 2016, 5th Author, Patent Number: ZL 201410751451.9
3. A Compact High-load Power Turbine Generator, 2014, 4th Author, Patent Number: ZL 201210237159.6
4. A Thermal Side Air Cooling Method for a Vortex Combustion End Cover, 2014, 2nd Author, Patent Number: ZL 201010612737.0
Main Published Papers
1. Chaowei Z , Xuezhi D , Xiyang L , et al. A method to select loss correlations for centrifugal compressor performance prediction[J]. Aerospace science and technology, 2019, 93(Oct.):105335.1-105335.15.
2. Zhang C , Dong X , Liu X , et al. One-dimensional modeling for tip clearance leakage vortex trajectory and stall-onset prediction in subsonic centrifugal impellers[J]. Proceedings of the Institution of Mechanical Engineers Part A Journal of Power and Energy, 2019, 234(3):095765091985673.
3. Zhao Qing-Jun , Liu Xi-Yang , et al. Experimental Investigation on Unsteady Pressure Fluctuation of Rotor Tip Region in High Pressure Stage of a Vaneless Counter-Rotating Turbine[J]. Science in China Series E-Technological Sciences , 2009, 52(6):1478-1483.
4. Liu Xi-Yang, Wen Quan, Zhao Xiao-Lu. A Revised Program for the Bypass Turbomachine Inverse Problem of Flow along S2 Surface[J]. Journal of Engineering Thermophysics, 2006, 27(003):417-419.
Main Scientific Research Projects
1. Overall Modeling and Digital Control System Development of a Certain Micro Gas Turbine, in Charge, Institute-level, 2017-2018
2. Research and Development and Verification of Gas Turbine Technology, Participated, Ministry-level, 2011-2016
3. Micro Gas Turbine Applicable to Distributed Energy Supply System, in Charge, Ministry-level, 2011-2015
4. Development of a 1MW-class Micro Gas Turbine and Its Energy Supply System, Participated, National-level, 2008-2014
