Methods of washing gas turbine engines and gas turbine engines
Washing of the gas turbine engine, during operation of the gas turbine engine, comprises a washing phase that consists in spraying a detergent liquid substance towards the inlet of the compressor of the engine; the mass flow of the detergent liquid substance to be sprayed is set so that the liquid-to-gas ratio at the inlet of the compressor is more than 1% and less than 5% with reference to the rated mass flow of the compressor; the washing phase comprises a first sub-phase during which the flow of the detergent liquid substance is increased gradually and a second sub-phase during which the flow of the detergent liquid substance is maintained constant.
1. A method of washing a gas turbine engine during operation of the gas turbine engine, the method comprising:
a washing phase that comprises spraying a detergent liquid substance towards an inlet of a compressor of the gas turbine engine;
wherein a mass flow of the detergent liquid substance to be sprayed is set so that a liquid-to-gas ratio at the inlet of the compressor is more than 1% and less than 5% with reference to a rated mass flow of the compressor, and wherein the washing phase comprises:
a first sub-phase during which the mass flow of the detergent liquid substance is increased gradually, and
a second sub-phase during which the mass flow of the detergent liquid substance is maintained constant.
2. The method of claim 1 , wherein the washing phase further comprises a third sub-phase during which the mass flow of the detergent liquid substance is decreased gradually.
3. The method of claim 1 , wherein the mass flow of the detergent liquid substance during the second sub-phase is constant at a desired value.
4. The method of claim 3 , wherein the mass flow value of the detergent liquid substance is set on a basis of ambient conditions.
5. The method of claim 1 , wherein the second sub-phase lasts for a predetermined period of time that is more than 0.5 minutes and less than 5 minutes.
6. The method of claim 2 , wherein at least one of the first sub-phase or the third sub-phase lasts for a predetermined period of time that is more than 5 seconds and less than 30 seconds.
7. The method of claim 1 , wherein the washing phase lasts for a predetermined period of time that depends on gas turbine efficiency.
8. The method of claim 7 , further comprising the steps of:
providing a design compressor pressure ratio;
measuring an actual compressor pressure ratio; and
calculating the predetermined period of time as function of a ratio between the actual compressor pressure ratio and the design compressor pressure ratio.
9. The method of claim 1 , wherein the washing phase is repeated a predetermined number of times in a day for a predetermined time length.
10. The method of claim 9 , wherein the predetermined number of times the washing phase is repeated is more than 1 and less than 10.
11. The method of claim 1 , wherein a pressure of the detergent liquid substance to be sprayed is more than 0.2 MPa and less than 2.0 MPa.
12. The method of claim 1 , wherein the detergent liquid substance is sprayed at a certain distance from an external wall of an inlet path of the compressor and at a certain distance from a internal wall of the inlet path of the compressor and in a certain direction.
13. The method of claim 1 , wherein the detergent liquid substance is sprayed in front of the compressor.
14. The gas turbine engine comprising:
the compressor,
a turbine downstream of the compressor,
a plurality of nozzles configured to spray a detergent liquid substance towards the inlet of the compressor; and
a control unit configured to carry out the method according to claim 1 .
15. The method of claim 2 , wherein the mass flow of the detergent liquid substance during the second sub-phase is constant at a desired value.
16. The method of claim 3 , wherein the mass flow value of the detergent liquid substance is set on a basis of ambient temperature.
17. The method of claim 1 , wherein the detergent liquid substance is sprayed from a mouth of the compressor.