发明名称 |
Engine Compressor Wash System |
摘要 |
A gas turbine engine includes: a compressor; a combustor downstream of the compressor along a gaspath; a turbine downstream of the combustor along the gaspath; a plurality of wash nozzles having outlets along the gaspath; and at least one inlet fitting coupled to the wash nozzles to bound a wash flowpath from an inlet port of the at least one inlet fitting to said outlets of said nozzles. The plurality of stages include: a stage upstream of blades of one compressor section; and another stage between said blades of one compressor section and blades of another compressor section. |
申请公布号 |
US2014144151(A1) |
申请公布日期 |
2014.05.29 |
申请号 |
US201213689305 |
申请日期 |
2012.11.29 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
BIFULCO ANTHONY R. |
分类号 |
F02C3/04;B23P6/00;F02C9/00 |
主分类号 |
F02C3/04 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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