CN102061996A - Inlet air processing system of combustion gas turbine - Google Patents
Inlet air processing system of combustion gas turbine Download PDFInfo
- Publication number
- CN102061996A CN102061996A CN2010106043642A CN201010604364A CN102061996A CN 102061996 A CN102061996 A CN 102061996A CN 2010106043642 A CN2010106043642 A CN 2010106043642A CN 201010604364 A CN201010604364 A CN 201010604364A CN 102061996 A CN102061996 A CN 102061996A
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- exhaust
- inlet
- gas turbine
- bypass
- vent systems
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Abstract
The invention relates to an inlet air processing system of a combustion gas turbine, which comprises an inlet system, a bypass exhaust system and an exhaust system, wherein the inlet system is connected with the exhaust system through the bypass exhaust system, the inlet system comprises an inlet air defroster, a filtering chamber, an inlet air cooling device, an inlet silencer and an inlet pipeline; the bypass exhaust system comprises a combustion gas turbine rail, an exhaust ventilating pipeline, an overturning regulating valve, a compensator, an exhaust silencer and a bypass exhaust chimney, the overturning regulating valve, the compensator and the exhaust silencer are arranged on the bypass exhaust chimney; and the exhaust system comprises an exhaust box and an exhaust chimney connected with the exhaust box. The invention has the advantages of less occupation space, large processing air quantity, high air quality and low energy consumption.
Description
Technical field
The present invention relates to air treatment system, relate in particular to the gas turbine inlet air processing system.
Background technique
The air-treatment unit is used to regulate the equipment of Temperature and Relative Humidity of Indoor Air and cleanliness.Have and satisfy air heater, air-cooler, the air humidifier that hot wet process requirement is used, the air filter of the usefulness that purifies air is regulated the mixed bellows that new wind, return air uses and is reduced the silencing apparatus that air-blower noise is used.The air-treatment unit is equipped with ventilator, according to the requirement of annual air conditioning, and the configurable automatic regulating system that is connected with cold ﹠ heat source of unit.New blower fan group is primarily aimed at the state point of outdoor new wind and handles, and the air-treatment unit is primarily aimed at the state of indoor circulation wind and handles.
Summary of the invention
The purpose of this invention is to provide a kind of gas turbine inlet air processing system that air quantity is big, air quality is high, energy-conservation of handling.
The technical solution used in the present invention is:
The gas turbine inlet air processing system, it is characterized in that: it includes port system, bypass vent systems and vent systems, described entrance system is connected with vent systems by the bypass vent systems, described entrance system comprises intake air anti-icing equipment, filter chamber, intake air cooling unit, inlet silencing apparatus and inlet pipe, described filter chamber front end is equipped with the intake air anti-icing equipment, rear end, described filter chamber is equipped with the intake air cooling unit, described intake air cooling unit again with the inlet silencing apparatus, described inlet silencing apparatus is connected with inlet pipe; Described bypass vent systems comprises gas turbine fence, exhaust ventilation pipeline, upset modulating valve, compensator, exhaust silencer and bypass exhaust chimney, described gas turbine fence is connected with the bypass exhaust chimney by the exhaust ventilation pipeline, and upset modulating valve, compensator and exhaust silencer are installed on the described bypass exhaust chimney; Vent systems comprises exhaust box and the exhaust chimney that is connected with exhaust box.
Described intake air anti-icing equipment is a windshield heater.
Described intake air cooling unit is an air-cooler.
Advantage of the present invention: occupy little space, handle that air quantity is big, air quality is high and energy consumption is low.
Description of drawings
Fig. 1 is a structured flowchart of the present invention.
Wherein: 1, exhaust box, 2, exhaust chimney, 3, the bypass exhaust chimney, 4, windshield heater, 5, the filter chamber, 6, air-cooler, 7, the inlet silencing apparatus, 8, inlet pipe, 9, the gas turbine fence, 10, exhaust ventilation pipeline, 11, the upset modulating valve, 12, compensator, 13, exhaust silencer.
Embodiment
As shown in Figure 1, gas turbine inlet air processing system of the present invention, it includes port system, bypass vent systems and vent systems, entrance system is connected with vent systems by the bypass vent systems, entrance system comprises windshield heater 4, filter chamber 5, air-cooler 6, inlet silencing apparatus 7 and inlet pipe 8, and filter chamber's 5 front ends are equipped with windshield heater 4, and 5 rear ends, filter chamber are equipped with air-cooler 6, air-cooler 6 again with the inlet silencing apparatus 7, the inlet silencing apparatus 7 be connected with inlet pipe 8; The bypass vent systems comprises gas turbine fence 9, exhaust ventilation pipeline 10, upset modulating valve 11, compensator 12, exhaust silencer 13 and bypass exhaust chimney 3, gas turbine fence 9 is connected with bypass exhaust chimney 3 by exhaust ventilation pipeline 10, and upset modulating valve 11, compensator 12 and exhaust silencer 13 are installed on the bypass exhaust chimney 3; Vent systems comprises exhaust box 1 and the exhaust chimney 2 that is connected with exhaust box 1.
Claims (3)
1. gas turbine inlet air processing system, it is characterized in that: it includes port system, bypass vent systems and vent systems, described entrance system is connected with vent systems by the bypass vent systems, described entrance system comprises the intake air anti-icing equipment, the filter chamber, the intake air cooling unit, inlet silencing apparatus and inlet pipe, described filter chamber front end is equipped with the intake air anti-icing equipment, rear end, described filter chamber is equipped with the intake air cooling unit, described intake air cooling unit again with the inlet silencing apparatus, described inlet silencing apparatus is connected with inlet pipe; Described bypass vent systems comprises gas turbine fence, exhaust ventilation pipeline, upset modulating valve, compensator, exhaust silencer and bypass exhaust chimney, described gas turbine fence is connected with the bypass exhaust chimney by the exhaust ventilation pipeline, and upset modulating valve, compensator and exhaust silencer are installed on the described bypass exhaust chimney; Vent systems comprises exhaust box and the exhaust chimney that is connected with exhaust box.
2. gas turbine inlet air processing system according to claim 1 is characterized in that: described intake air anti-icing equipment is a windshield heater.
3. gas turbine inlet air processing system according to claim 1 is characterized in that: described intake air cooling unit is an air-cooler.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010106043642A CN102061996A (en) | 2010-12-24 | 2010-12-24 | Inlet air processing system of combustion gas turbine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010106043642A CN102061996A (en) | 2010-12-24 | 2010-12-24 | Inlet air processing system of combustion gas turbine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN102061996A true CN102061996A (en) | 2011-05-18 |
Family
ID=43997451
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2010106043642A Pending CN102061996A (en) | 2010-12-24 | 2010-12-24 | Inlet air processing system of combustion gas turbine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102061996A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106321245A (en) * | 2015-06-30 | 2017-01-11 | 通用电气公司 | Air supply and conditioning system for a gas turbine |
| CN107664068A (en) * | 2016-07-28 | 2018-02-06 | 通用电气公司 | Compact gas turbine air entrance system |
-
2010
- 2010-12-24 CN CN2010106043642A patent/CN102061996A/en active Pending
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106321245A (en) * | 2015-06-30 | 2017-01-11 | 通用电气公司 | Air supply and conditioning system for a gas turbine |
| CN107664068A (en) * | 2016-07-28 | 2018-02-06 | 通用电气公司 | Compact gas turbine air entrance system |
| CN107664068B (en) * | 2016-07-28 | 2021-07-02 | 通用电气公司 | Compact gas turbine air inlet system |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20110518 |