One-key start-stop control system of single-shaft gas turbine
By using a one-button start-stop control system for a single-shaft gas turbine, the system collects and analyzes gas turbine parameters in real time, generates a set of state parameters, and dynamically plans the start-stop control sequence. This solves the problem of balancing equipment lifespan loss and operating efficiency during the start-stop process of the gas turbine, and optimizes the long-term reliability and economy of the equipment.
Patent Information
- Application Number
- CN202511814942.8
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2025-12-04
- Publication Date
- 2026-01-27
AI Technical Summary
Existing gas turbine start-stop control systems lack real-time equipment life assessment and optimization mechanisms, resulting in significant differences in equipment life loss during start-stop processes. Furthermore, the start-stop process is disconnected from operational efficiency optimization, making it impossible to achieve a balance between life loss and operational efficiency, thus increasing power plant operating costs.
The system adopts a one-button start-stop control system for a single-shaft gas turbine. It collects gas turbine parameters in real time through a state observer, generates a state parameter set, and combines it with a life assessment and efficiency calculation model to dynamically plan the start-stop control sequence. It also utilizes a multi-loop coordinated control system and an adaptive PID controller to generate precise control commands, thereby minimizing equipment life loss and optimizing operating efficiency.
It effectively avoids excessive stress impact on hot components during start-up and shutdown, extends equipment overhaul cycle, reduces maintenance costs, improves operating efficiency, reduces fuel waste, and enhances the power plant's competitiveness in the peak-shaving ancillary services market.