| 摘要 |
An axial turbomachine housing is designed to channel a primary annular flow in the low-pressure compressor of the turbomachine. The housing has a first shell and a second shell designed to be contiguous and coaxial. The first shell has a flange and a centring surface substantially cylindrical. The second shell has a flange and radial centring means designed to mate with the centring surface. The flange of the first shell includes cut-outs distributed along its circumference, and the centring means extend axially from the flange of the second shell through the cut-outs to the centring surface where the two flanges are in contact. |
