| 摘要 |
A row of stator blades 62 in a compressor 52 of a combustion turbine engine, the combustion turbine engine including a diffuser 83 located downstream of the compressor 52, and the row of stator blades 62 disposed in close proximity to the diffuser 83; the row of stator blades 62 comprising stator blades 62 that include at least one of an inboard forward notch 95 and an outboard forward notch 121.
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