Gas turbine control method and system based on distributed control system
By using a gas turbine control method based on a distributed control system, feature engineering is performed using distributed sensor arrays and edge computing nodes, combined with an improved model predictive control algorithm. This solves the problems of data processing lag and multivariable coupling control difficulties in traditional gas turbine control systems, and enables efficient operation and improved stability of gas turbines under complex operating conditions.
Patent Information
- Application Number
- CN202510827554.7
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Filing Date
- 2025-06-19
- Publication Date
- 2026-03-31
- Estimated Expiration
- 2045-06-19
AI Technical Summary
Traditional gas turbine control systems rely on a centralized control architecture, which leads to data processing delays and difficulties in controlling multiple variables. This makes it difficult to achieve coordinated optimization of gas turbine combustion efficiency, emission indicators, and equipment lifespan under complex operating conditions, increasing the risk of energy waste and environmental pollution.
A distributed control system-based approach is adopted, which uses a distributed sensor array to synchronously collect gas turbine operating parameters, performs feature engineering processing through edge computing nodes, and uses an improved model predictive control algorithm to decouple control quantities. Combined with closed-loop feedback and parameter self-learning mechanism, real-time evaluation and signal feedback are performed.
It improves the dynamic response capability of gas turbines under multi-dimensional operating conditions, increases combustion efficiency, reduces environmental pollution risks, and enhances operational stability and adaptability under complex operating conditions.