发明名称 |
METHODS OF WASHING GAS TURBINE ENGINES AND GAS TURBINE ENGINES |
摘要 |
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. |
申请公布号 |
US2016356176(A1) |
申请公布日期 |
2016.12.08 |
申请号 |
US201415102079 |
申请日期 |
2014.12.04 |
申请人 |
NUOVO PIGNONE SRL |
发明人 |
PECCHIOL Mario;NAVARRO CANALES Celia;Olivieri Tommaso;MANON CANTU Jorge Omar |
分类号 |
F01D25/00;B08B3/02;B08B9/093;F01D5/02;F04D29/32 |
主分类号 |
F01D25/00 |
代理机构 |
|
代理人 |
|
主权项 |
1. A method of washing a gas turbine engine during operation of the gas turbine engine, comprising:
a washing phase that includes spraying a detergent liquid substance towards the inlet of the compressor of the engine;
wherein 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, and wherein the washing phase comprises:a first sub-phase during which the flow of the detergent liquid substance is increased gradually, anda second sub-phase during which the flow of the detergent liquid substance is maintained constant. |
地址 |
Florence IT |