Method and device for setting parameters of closed-loop PID (proportion integration differentiation) controller of gas turbine

A gas turbine and controller technology, applied to electric controllers, controllers with specific characteristics, etc., can solve problems such as poor control effects, achieve the effects of reducing fuel consumption, good control effects, and prolonging service life

Inactive Publication Date: 2015-05-20
BEIJING HUAQING GAS TURBINE & INTEGRATED GASIFICATION COMBINED CYCLE ENG TECH
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Problems solved by technology

[0004] Aiming at the defect that each controller of the existing gas turbine is controlled according to the parameters obtained by mainly relying on the engineer's experience setting, the control effect is not good, the present invention provides a parameter setting method and device for the closed-loop PID controller of the gas turbine

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  • Method and device for setting parameters of closed-loop PID (proportion integration differentiation) controller of gas turbine
  • Method and device for setting parameters of closed-loop PID (proportion integration differentiation) controller of gas turbine
  • Method and device for setting parameters of closed-loop PID (proportion integration differentiation) controller of gas turbine

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Embodiment Construction

[0030] The technical solution of the present invention will be further described in detail in conjunction with the accompanying drawings and embodiments.

[0031] figure 1 Shows a schematic flow chart of the parameter tuning method of the gas turbine closed-loop PID controller in this embodiment, as figure 1 As shown, the parameter tuning method of a gas turbine closed-loop PID controller provided in this embodiment includes:

[0032] S1, initialize the initial value of the proportional action coefficient and the search step size in the PID controller, and initialize the initial value and the search step size of the integral action coefficient in the PID controller; wherein the search step size refers to the proportional action coefficient and the integral The action factor is incremented for each search.

[0033] For example, the steps of initializing the initial value of the proportional action coefficient and the search step size in the PID controller, and initializing th...

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Abstract

The invention relates to a method and a device for setting parameters of a closed-loop PID (proportion integration differentiation) controller of a gas turbine. The method comprises the following steps of initializing the initial values of a proportion action coefficient and an integration action coefficient of the PID controller, and researching the step length; determining the researching ranges of the proportion action coefficient and the integration action coefficient; performing the step response testing of a gas turbine model on all combinations of searching values of the proportion action coefficient and the integration action coefficient within the searching range, and selecting all searching values meeting the maximum overshoot and time adjusting requirements; determining one group of setting parameters. The method has the advantages that the defects of low parameter setting effect and poor control effect because of reliance on experiences of engineers in the prior art are overcome; a plurality of controller parameters meeting the dynamic property indexes of the controller can be automatically obtained, the setting parameters are determined, the control effect better than the effect of the manual setting method is obtained, the service life of the gas turbine unit is effectively prolonged, and the fuel consumption of the gas turbine unit is decreased.

Description

technical field [0001] The invention relates to the technical field of gas turbine control, in particular to a parameter setting method and device for a gas turbine closed-loop PID controller (Proportion Integration Differentiation, proportional-integral-differential controller). Background technique [0002] The working process of a heavy-duty gas turbine for power generation is that the air is compressed in the compressor, mixed with the fuel injected in the combustion chamber for combustion, and the high-temperature combustion gas expands in the turbine to do work, driving the generator to be connected to the grid for power generation. The heavy-duty gas turbine is a multivariable nonlinear coupling system. The common control system adopts segmental control, which is similar to an expert control system, including: start-up control in the start-up process, speed control in the load process, and close to Use temperature control at base load, etc. The control objectives and...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05B11/42
Inventor 刘蕾
Owner BEIJING HUAQING GAS TURBINE & INTEGRATED GASIFICATION COMBINED CYCLE ENG TECH
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