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Pressure adjustment method of combined cycle waste heat boiler for gas turbine deterioration

A waste heat boiler and combined cycle technology, applied in the field of gas turbines, can solve problems such as affecting the operation performance of the waste heat boiler

Active Publication Date: 2019-01-29
SOUTH CHINA UNIV OF TECH
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

These parameter changes will affect the operating performance of the waste heat boiler, so that the original design operating parameters (such as steam pressure at all levels) may not be the optimal value. Therefore, it is necessary to optimize the operating pressure of the waste heat boiler so that the combined cycle can High-efficiency operation of the unit

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  • Pressure adjustment method of combined cycle waste heat boiler for gas turbine deterioration
  • Pressure adjustment method of combined cycle waste heat boiler for gas turbine deterioration
  • Pressure adjustment method of combined cycle waste heat boiler for gas turbine deterioration

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Embodiment Construction

[0099] The present invention will be further described below in conjunction with specific examples.

[0100] Such as figure 1 and figure 2 As shown, the method for adjusting the pressure of the combined cycle waste heat boiler for the deterioration of the gas turbine according to the present invention includes the following steps:

[0101] 1) Establish a gas turbine model with IGV for a specific unit using the general curve of the gas turbine combined with the regression analysis method;

[0102] 2) Based on the empirical formula of convective heat transfer and the principle of energy conservation, a waste heat boiler model is established;

[0103] 3) Referring to the actual control principle of the gas turbine, the operation of the unit is controlled based on the corresponding relationship between the exhaust temperature of the gas turbine turbine and the opening of the IGV;

[0104] 4) When the gas turbine components deteriorate, in order to achieve the specified power, ...

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Abstract

The invention discloses a pressure adjustment method for a combined cycle heat recovery boiler with a deteriorated gas turbine. The method comprises steps as follows: 1), a gas turbine model provided with an IGV (inlet guide vane) for adjustment and used for a specific unit is established according to a universal characteristic curve of a gas turbine in combination with a regression analysis method; 2), a heat recovery boiler model is established on the basis of a convection heat transfer empirical formula and an energy conservation principle; 3), the unit is controlled to operate according to the corresponding relation between the turbine exhaust gas temperature of the gas turbine and the opening of the IGV and in reference of the practical control principle of the gas turbine unit; 4), when a part of the gas turbine is deteriorated, the opening of the IGV is required to be readjusted to reach designated power, the exhaust parameter of the gas turbine is changed, then the operation performance of the heat recovery boiler is changed, at the time, operation pressure of the heat recovery boiler is optimized, the heat recovery boiler and the gas turbine can adapt to new work conditions and have higher power, new sliding pressure is acquired when the IGV has a new opening or combined cycle power is reached. The operation pressure of the heat recovery boiler can be optimized, and the operation efficiency is improved.

Description

technical field [0001] The invention relates to the field of gas turbines, in particular to a method for adjusting the pressure of a combined cycle waste heat boiler aiming at the deterioration of the gas turbine. Background technique [0002] In 2003, my country introduced a batch of F-class heavy-duty gas turbine combined cycle units by using the market-for-technology bundling bidding method. With the increase of power plant operation time, the deterioration of gas turbine components is inevitable. During the use of gas turbine components, due to the slight deformation, wear, corrosion and aging of the components themselves, the original performance will gradually decline, which is called the deterioration of gas turbine components. The most intuitive manifestation is the decline in component efficiency under the same external conditions. The turbine blades of the gas turbine in the combined cycle unit work in a harsh environment of high temperature and high pressure. Unle...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06F17/50G06F17/18G06N3/12
CPCG06F17/18G06F30/367G06F2111/06G06F2119/06G06N3/126
Inventor 杨承黄志峰马晓茜王旭升
Owner SOUTH CHINA UNIV OF TECH