Shell for reducing overpressure in the vicinity of the upstream seal of a turbojet bearing housing

1. A turbojet bearing housing including a fixed envelope traversed by a rotor, the envelope including a cylindrical end having an outer threading surrounding a seal ensuring a leak tightness of the cylindrical end with the rotor, the envelope being equipped with a shell having an inner threading screwed around the outer threading of the cylindrical end of the envelope, the shell including radial channels emerging opposite the seal while being arranged so that an air stream traversing the seal towards the housing mainly comes from these radial channels in which the seal is maintained axially locked in the cylindrical end of the envelope by the shell; and

the turbojet bearing housing further including a locking collar surrounding the shell, the locking collar including on the one hand tabs engaging in corresponding notches of the envelope and on the other hand tabs pulling down into corresponding notches of the shell to rotationally lock the shell with respect to the envelope.

2. The turbojet bearing housing according to claim 1 , in which the rotor comprises in the vicinity of the seal a drop throwing device situated opposite an inner face of the shell to centrifuge oil present on the rotor in the event of leakage of the seal.

3. The turbojet bearing housing according to claim 2 , in which the shell comprises a drainage sheet to collect the oil centrifuged by the drop throwing device.

4. A turbomachine including the turbojet bearing housing according to claim 1 .

5. A turbojet including the turbomachine according to claim 4 .