초록

An axial compressor includes a nozzle for injecting a cleaning fluid. The cleaning fluid is injected through the nozzles in a flow duct during operation, so that rear blading rows are also cleaned.

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1. An axial compressor, comprising a compressor inlet and a compressor outlet; a flow duct, arranged between the compressor inlet and the compressor outlet, enclosed by a compressor casing and in which guide blades and rotor blades are arranged; and at least one nozzle for injecting a cleaning

1. An axial compressor, comprising a compressor inlet and a compressor outlet; a flow duct, arranged between the compressor inlet and the compressor outlet, enclosed by a compressor casing and in which guide blades and rotor blades are arranged; and at least one nozzle for injecting a cleaning fluid, arranged in the flow duct such that cleaning of at least some of the guide blades and rotor blades occurs upon the injection of the cleaning fluid, wherein the nozzle is located in a guide blade. 2. The axial compressor as claimed in claim 1, wherein the nozzle is located between a guide blade and a rotor blade. 3. A gas turbine comprising the axial compressor as claimed in claim 1. 4. The axial compressor as claimed in claim 1, wherein the nozzle is placed at a distance from the compressor casing by a lance leading through the compressor casing. 5. The axial compressor as claimed in claim 4, wherein the lance is radially traversable. 6. An axial compressor, comprising a compressor inlet and a compressor outlet; a flow duct, arranged between the compressor inlet and the compressor outlet, enclosed by a compressor casing and in which guide blades and rotor blades are arranged; and at least one nozzle for injecting a cleaning fluid, arranged in the flow duct such that cleaning of at least some of the guide blades and rotor blades occurs upon the injection of the cleaning fluid, wherein the nozzle is located between a guide blade and a rotor blade, and wherein the nozzle is placed at a distance from the compressor casing by a lance leading through the compressor casing. 7. A gas turbine comprising the axial compressor as claimed in claim 6. 8. A gas turbine including an axial compressor, the axial compressor comprising: a compressor inlet and a compressor outlet; a flow duct, arranged between the compressor inlet and the compressor outlet, enclosed by a compressor casing and in which guide blades and rotor blades are arranged; and at least one nozzle for injecting a cleaning fluid, arranged in the flow duct such that cleaning of at least some of the guide blades and rotor blades occurs upon the injection of the cleaning fluid, wherein the nozzle is located between a guide blade and a rotor blade. 9. A method of cleaning an axial compressor, including a compressor inlet and a compressor outlet and a flow duct arranged between the compressor inlet and the compressor outlet, the flow duct being enclosed by a compressor casing and including guide blades and rotor blades arranged therein, the method comprising: injecting a cleaning fluid into the flow duct at an injection position behind the compressor inlet, in the flow direction, after a first row of guide blades and before the compressor outlet during the compressor operation; and cleaning at least some of the guide blades and rotor blades by the injected cleaning fluid, wherein a nozzle is used for injecting the cleaning fluid, and, wherein the nozzle is located in a guide blade. 10. The method of claim 9, wherein the method is for cleaning an axial compressor in a gas turbine.