| 摘要 |
The invention relates to a turbine engine compressor (10'), comprising at least one annular row of variable-pitch stator blades (12), wherein said blades are substantially radial and comprise pivots (22, 24) at the radial ends thereof, the radially external pivots of the blades being inserted in first openings of a stator housing (20) and the radially internal pivots being inserted in second openings of a floating ring (60) that surrounds a rotor (18) of the compressor, characterized in that an annular stator part (62) is inserted between the floating ring and the compressor rotor, and in that first sealing means are mounted between the stator part and the compressor rotor, and second sealing means are mounted between the floating ring and the stator component. |
