Gas turbine compressor blade cleaning system and method

The invention discloses a gas turbine compressor blade cleaning system and method. The gas turbine compressor blade cleaning system comprises a first set of nozzles at least arranged on the inner wall of a gas compressor shell and a second set of nozzles arranged on the inner wall of a gas compresso...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	FU XUFENG, CHEN SHUAI, LI HENGHAI, CAO ZHIMING, ZHANG GUILIN, ZHOU PENG, YAN YUFENG, YAN CHUANWU, YU PENGFENG, LONG YANCHANG
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT PUMPS POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC FLUIDS WEAPONS
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Beschreibung
Zusammenfassung:	The invention discloses a gas turbine compressor blade cleaning system and method. The gas turbine compressor blade cleaning system comprises a first set of nozzles at least arranged on the inner wall of a gas compressor shell and a second set of nozzles arranged on the inner wall of a gas compressor shell. The first drainage pipeline is arranged on the inner wall of the bottom of the compressor shell; a steam generating device; the output end is connected with the first group of nozzles, and the input end is connected with the fluid conveying pipeline of the steam generating device; a first control valve is arranged on the fluid conveying pipeline; a second control valve is arranged on the first drainage pipeline; the control device is connected with the steam generating device, the first control valve and the second control valve and used for controlling the steam generating device to generate high-temperature and high-pressure steam with the temperature not lower than the set temperature and the set air pr