Bin Wang  Associate Researcher

E-mail：wang_bin@tsinghua.edu.cn

Address ：Room 5213, Building A5, Tsinghua University Changping Research Base, Nankou Town, Changping District, Beijing.

EDUCATION

Graduated from Beihang University in 2014，Obtained a doctor degree in Engineering.

WORK EXPERIENCE

2021- Present, Institute for Aero Engine, Tsinghua University

2016-2021, Strategic Planning and Argumentation Center, Aero Engine Academy of China

2014-2016, Strategy Center, AVIC Academy of Aeronautic Propulsion Technology

2007-2011, Research Department for Whole Performance, China Gas Turbine Establishment

Major Research Direction

Engaged in the research of adaptive/variable cycle engines, turbofan engines, turboshaft engines and gas turbine control systems，Participated in the development projects of multiple aeroengine control systems，the main research directions are as follows.

 The overall design of aeroengine control system

 Engine and control system modeling,

 Multi-variable robust control

 Health management and fault diagnosis

 Intelligent control

 Control software

Papers

1. Wang Bin, Wang Xi, Shi Yulin,Wang Huawei. A real-time piecewise linear dynamic model of aeroengine [J]. Journal of Aerospace Powe, 2014, 29(3):696-701.

2. Wang Bin, Wang Xi, Kong Xiangxi, Yang Be. Direct thrust control of turbofan engines based on unknown input observer [J]. Journal of Aerospace Power, 2016, 31(3):693-700.

3. Wang Bin, Xiao Yi, Liu Feng. Prospect for Future Aero Engine Control Technology Development from Adaptive Cycle Engine [J]. Aerospace Power, 2019, (3):48-51.

4.Wang Bin, Shi Yulin, and Wang Xi. Aeroengine State Variable Modeling based on the PSO Algorithm[C]. 2013 Chinese Automation Congress（CAC2013). 7-8 November 2013, Changsha, China.

5.Wang Bin, Wang Xi and Liu Yue. A High By-pass Ratio Turbofan Model Based on CMF Method[C]. Applied Mechanics and Materials Vol. 302 (2013) pp 578-582.

6.Wang Huawei, Wang Xi, Dang Wei, Yao Huating and Wang Bin. Generic Design Methodology for Electro-Hydraulic Servo Actuator in Aero-engine Main Fuel Control System [C]. ASME Turbo Expo 2014 Dusseldorf, Germany.

7.Penghui Sun, Xi Wang, Shubo Yang , Bei Yang , Huairong Chen and Bin Wang. Bumpless Transfer of Uncertain Switched System and Its Application to Turbofan Engines. Energies 2021, 14(16), 5204.