Cao Wenyu  Senior Engineer (Research Series)

Email: caowenyu@tsinghua.edu.cn

Address: Tsinghua University, Haidian District, Beijing, China

Education background

2018.09 - 2024.06: PhD of Engineering Thermophysics, University of Chinese Academy of Sciences

2009.09 - 2012.03: Master of Power Engineering and Engineering Thermophysics, Beihang University

2003.09 - 2007.06: Bachelor of Aircraft Power Engineering, Beihang University

Career Experience

2024.01 - Present: Senior Engineer (Research Series), Tsinghua University, Institute of Aerospace Engine

2019.12 - 2023.12: Engineer (Research Series), Tsinghua University, Institute of Aerospace Engine

2012.03 - 2019.11: Engineer, Institute of Engineering Thermophysics, Chinese Academy of Sciences, Lightweight Power Laboratory

2007.08 - 2009.06: Assistant Engineer, Gas Turbine Research Institute of China, Combustion Technology Department

Areas of Research Interests

Cao Wenyu is the project leader of the Digital Engine Program at Tsinghua University. He has been engaged in the overall structural design and structural strength research of aerospace engines. As the lead structure engineer, he participated in multiple projects including turbofan/turbojet engines, small gas turbines, and key national projects. His main research directions include the integration and traceability of multi-source heterogeneous data sets based on design-simulation-manufacturing, structural design-simulation integration based on MBSE, and technology state management based on physical models.

Academic Achievements

Yang Jiali, Cao Wenyu, Yao Shun, Liu Kai, Xie Pengfu, Hu Zhongzhi. 'Model Real-Time Driven Immersive Virtual Operation System for Aerospace Engines.' Aerospace Engine. 2023, 49(3): 9-16.

Cao Wenyu, Yang Junjie, Zhang Hualiang. 'Unified Constitutive Modeling of Haynes 230 Including Cyclic Hardening/Softening and Dynamic Strain Aging under Isothermal Low-Cycle Fatigue and Fatigue-Creep Loads,' International Journal of Plasticity, 2021, 138(2021): 102922.

Cao Wenyu, Hualiang Zhang. 'Unified Constitutive Modeling of Haynes 230 for Thermomechanical Fatigue-Creep and Creep Behavior,' ASME 2022 International Mechanical Engineering Congress and Exposition.

Patents

1. Pipe structure passing through three layers of casing (China: ZL202111265452.9)

Applicant: Cao Wenyu et al., Date: 2022.6.14

2. Multichannel aerospace engine casing structure with fan blade tips (China: ZL202111205513.2)

Applicant: Cao Wenyu et al., Date: 2022.6.17

3. Bearing chamber structure for aerospace engines with embedded motors (China: ZL202210412455.9)

Applicant: Cao Wenyu et al., Date: 2023.3.10

4. Vector-regulated nozzle and adaptive variable-cycle engine (China: ZL202210412339.7)

Applicant: Cao Wenyu et al., Date: 2023.9.19

5. Model Real-Time Driven Immersive Virtual Operation System for Aerospace Engines (China: ZL202310207398.5)

Applicant: Yang Jiali, Cao Wenyu et al., Date: 2023.9.20

6. Data-driven real-time 3D rendering system for aerospace engines (China: ZL202310217917.6)

Applicant: Yang Jiali, Yao Shun, Cao Wenyu et al., Date: 2023.9.16