| 摘要 |
A turbomachine such as an aircraft turbojet comprising an electrical generator/starter ( 26 ) that can be mounted and dismounted by axial translation in an upstream enclosure ( 18 ) of the turbomachine between the low-pressure compressor and the high-pressure compressor, and couple to electrical cables ( 34 ) which extend inside the structural arms ( 12 ) of the intermediate casing ( 10 ) of the turbomachine. |
