| 摘要 |
<p>The present invention relates to a support device intended for the vanes of axial-flow engines, mainly turbojet engines. The device is characterised in that at least two support crowns (12, 14) can be adjusted so as to be adjacent or opposite relative to each other, wherein said crowns are intended for mounting between the guide vanes or the rotor vanes in the adjacent stages of compressors or engine units.</p> |
