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Gas turbine energy saving type incoming gas anti-icing apparatus

A gas turbine and anti-icing device technology, which is applied in the direction of gas turbine devices, jet propulsion devices, mechanical equipment, etc., can solve the problems of undisclosed structure and implementation difficulties of hybrid heating devices

Active Publication Date: 2014-02-12
PIPECHINA SOUTH CHINA CO
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] CN101661451A discloses an energy-saving air intake anti-icing device for gas turbines, but its hybrid heating device, an important device, does not disclose the specific structure, and there are still difficulties in its specific implementation

Method used

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  • Gas turbine energy saving type incoming gas anti-icing apparatus
  • Gas turbine energy saving type incoming gas anti-icing apparatus
  • Gas turbine energy saving type incoming gas anti-icing apparatus

Examples

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Embodiment

[0076] Embodiment. This example takes the RR gas compressor set of the West-to-East Gas Pipeline as a test machine, and its composition is as follows figure 1 shown. A high-temperature flue gas outlet pipe 6 is installed on the upper part of the flue, and the high-temperature flue gas outlet pipe 6 is connected to the induced draft fan 8 through the manual adjustment valve 7, and the exhaust port of the induced draft fan 8 is connected to the mixing heating device 9, and the upper part of the mixing heating device 9 is already installed The air inlet filter 2 is connected to the air duct after the air inlet filter 2 to the air inlet of the gas turbine compressor 1.

[0077] The structure of the mixing heating device 9 is as Figure 3-Figure 5 As shown, it is 10 rows of mixed heating pipes 11 arranged in parallel, the two ends of the mixed heating pipes 11 are connected to the connecting box 10, and the connecting boxes 10 at the two ends of the pipes are connected at one end,...

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Abstract

The present invention discloses a gas turbine energy saving type incoming gas anti-icing apparatus, provides improvement on the existing gas turbine air compressor inlet air anti-icing apparatus, and relates to the technical field of non-variable-capacity engines, heat exchange and pipeline systems. The gas turbine energy saving type incoming gas anti-icing apparatus is characterized in that the mixing heating device structure is that multi-row mixing heating alignment pipes (11) are aligned in a parallel manner, both ends of the mixing heating alignment pipes (11) are connected with connection boxes (10), one ends of the connection boxes (10) on both ends of the alignment pipes are communicated to form an n shape, the middle portion of the communication edge of the n-shaped connection box (10) is connected with a wind outlet pipe of an induced fan, the n-shaped connection box and the horizontal plane form downward inclination with an angle of 1-3 DEG along the air flow direction, and the lowest end bottom is provided with a tiny connection box low point drainage hole (12). According to the present invention, gas turbine unit power loss caused by the anti-icing system can be reduced, adverse effects of the anti-icing system on gas turbine unit operation stability can be reduced, and effects of anti-icing, frost prevention and energy saving are provided.

Description

technical field [0001] The invention is an energy-saving air intake anti-icing device for a gas turbine, which is an improvement to the existing air anti-icing device for the compressor inlet of the gas turbine. It relates to the technical fields of non-variable engine, heat exchange and pipeline system. Background technique [0002] As of the end of 2011, there were 113 combustion drive compressor units put into operation in CNPC's natural gas pipeline, mainly including RR units (27 units), GE units (63 units) and Solar units (21 units). Most of these units work in the central and western regions where the environment is relatively harsh. Especially under low temperature and high humidity working conditions, the moisture in the intake air may freeze, which will cause serious losses to the unit. There are many problems in the existing anti-icing measures of these units. For example, RR and GE units are equipped with compressor inlet air anti-icing systems that bleed air fro...

Claims

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Application Information

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IPC IPC(8): F02C7/047
Inventor 张衍岗姬忠礼李刚张磊蔡德宇刘建臣刘培军谷思宇
Owner PIPECHINA SOUTH CHINA CO
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