作者: Carl-Johan Hjerpe , Peter Asplund
DOI:
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摘要: Device for cleaning a gas turbine engine (2), and in particular an of turbofan type. The present invention further relates to method such engine. device comprises plurality nozzles (31, 33, 35) arranged atomize liquid the air stream inlet (20) (2) up-stream fan (25) (2). According first nozzle (31) is at position that emanating from impinges surfaces blades (40) substantially on pressure side (53); second (35) suction (54); third (33) passes between enters (23) core (203). Thereby, different types fouling found compressor can be removed efficient manner.