| 摘要 |
The invention relates to an element of a stator guide of an axial compressor of a turbomachine, in the form of a monobloc assembly, the outer shape thereof being a cylinder sector forming, in a radially outer manner, an outer shroud sector (46a) common to a plurality of axial stage sectors of radial stator guide blades (481,482,483) which are secured to said outer shroud sector in a radially outer manner, and, in a radially inner manner, stage by stage, to an inner platform sector (521,522,523), each inner platform sector stage being connected, in a radially inner manner, to a sector of first sealing means (561,562,563), each one suitable for engaging, tightly in relation to said gas, with second sealing means connected to a rotor shaft of the axial compressor. |
