| 摘要 |
AEROENGINE WASHING SYSTEM AND METHOD5The present invention is a collector (56) for collecting washing fluid issuing (40, 41) from a gas turbine engine (10) during and/or after a washing operation. The collector (56) comprises a collection tray (58, 53) and an10 inlet collector (70) attached at a first end (72) to the collection tray (58, 53). The second end (74) of the inlet collector (70) is connected to an inlet (12) of the engine (10), thereby collecting washing fluid (40, 41) issuing from any one or both the inlet (21) and below the engine15 (10). (Figure 1) |
