Method and device for evaluating outlet temperature of combustion chamber of gas turbine in real time and gas turbine
By monitoring conventional parameters at the gas turbine inlet and outlet boundaries and combining them with thermodynamic laws and flow characteristics, an evaluation model was constructed to achieve real-time online evaluation of the combustion chamber outlet temperature. This solved the problem of difficult monitoring of gas turbine combustion chamber temperature and ensured the safe, stable operation and efficient control of the gas turbine.
Patent Information
- Application Number
- CN202511688291.2
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2025-11-18
- Publication Date
- 2026-03-03
AI Technical Summary
Existing technologies make it difficult to achieve real-time online monitoring of the combustion chamber outlet temperature of gas turbines, resulting in the difficulty of accurately obtaining core temperature data during the whole-machine testing and actual operation phases of gas turbines, which affects the life assessment of hot-end components and the control of combustion efficiency.
By deploying sensor systems at the inlet and outlet boundaries of the gas turbine, atmospheric environment, fuel supply, and unit operating parameters are monitored in real time. Combining the first law of thermodynamics and the critical flow state at the throat of the turbine's first-stage guide vane, an evaluation model is constructed to achieve online evaluation of the combustion chamber outlet temperature.
It eliminates the need for detailed characteristic curves of components such as the compressor or turbine, simplifying the assessment process of the combustion chamber outlet temperature and providing key data support for real-time monitoring and efficient control, thus ensuring the safe and stable operation of the gas turbine.