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Yiguang Li

Reader

Cranfield University

United Kingdom

Research Interests

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Professors in United Kingdom Professors in Aerospace Engineering Aerospace Engineering professors in United Kingdom

About

Dr. Yiguang Li is a Reader at Cranfield University in the United Kingdom. His research focuses on gas turbine engines, intelligent diagnostics, and performance simulation, as evidenced by his recent publications. Key areas of interest include performance control for sequential combustors, health signal noise filtering using neural networks, and the evaluation of hydrogen-powered aero engines.

Articles (12)

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2026

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2025

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2024

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2023

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2023

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2022

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2022

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2022

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2021

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2021

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2020

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2020

Collaborators (2)

Vishal Sethi

Professor in Low Emissions Technologies and Combustion

Cranfield University

UNITED KINGDOM

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Ioannis Roumeliotis

Prof at Faculty of Engineering and Applied Science

Cranfield University

UNITED KINGDOM

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Yiguang Li

Research Interests

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Articles (12)

Gas turbine equivalent operating hour estimation considering creep-LCF interactions

Off-design performance control and simulation for gas turbine engines with sequential combustors

Thrust Rebalance to Extend Engine Time On-Wing With Consideration of Engine Degradation and Creep Life Consumption

Convolutional Neural Network Denoising Auto-Encoders for Intelligent Aircraft Engine Gas Path Health Signal Noise Filtering

A hierarchical structure built on physical and data-based information for intelligent aero-engine gas path diagnostics

Review of More Electric Engines for Civil Aircraft

Aeroengine transient performance simulation integrated with generic heat soakage and tip clearance model

A dynamic performance diagnostic method applied to hydrogen powered aero engines operating under transient conditions

Development and application of a preliminary design methodology for modern low emissions aero combustors

Techno-economic evaluation and optimization of CCGT power Plant: A multi-criteria decision support system

Assessment of degradation equivalent operating time for aircraft gas turbine engines

Sliding mode control with system constraints for aircraft engines

Collaborators (2)

Vishal Sethi

Ioannis Roumeliotis

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