| 摘要 |
A turbine engine, particularly for aircrafts, of the type comprising a rotor and at least two stages of stator blade rows positioned upstream and downstream of the rotor, wherein the rotor blades (8) are of the variable pitch type and have a drop shape, are of the twisted type (1) or of the constant deflection type (2) and the stator blades (25), positioned downstre am of the rotor, are of the twisted type. |
