Method for ventilating brake discs of an aircraft wheel

1. A method for ventilating discs ( 11 ) of a brake ( 10 ) fitted to an aircraft wheel ( 1 ) having a rim ( 2 ) mounted so as to rotate on an axle ( 4 ) of a landing gear of the aircraft, the brake discs being threaded onto a torsion tube ( 12 ) of the brake which extends around the axle, the method comprising:

integrating a compressor into a space extending inside the torsion tube in order to draw in air beneath the torsion tube and to return the air thus drawn in by the compressor over the torsion tube towards the brake discs, the compressor comprising rotary blades mounted on a ring that is secured to the rim to rotate with said rim.

2. The method according to claim 1 , in which the compressor is of the axial type and comprises at least one stage comprising rotating blades ( 21 ; 31 ) followed by fixed stator vanes ( 22 ; 32 ).

3. The method according to claim 1 , in which the compressor is of the centrifugal type.

4. The method according to claim 3 , in which the compressor is designed such that it draws in air only in its lower portion.

5. The method according to claim 3 , in which the compressor is designed such that it ejects compressed air only in its upper portion over the torsion tube.

6. The method according to claim 3 , in which the compressor comprises a bladed wheel ( 51 ) associated with a volute ( 52 ) of the compressor.

7. The method according to claim 1 , in which the rim comprises a closed web ( 7 ) that is able to redirect a flow of air generated by the compressor towards the brake discs.

8. The method according to claim 1 , in which the rim comprises openings in the web ( 7 ).

9. The method according to claim 8 , in which the openings ( 60 ) comprise covers ( 61 ) that are able to at least partially block said openings.

10. The method according to claim 1 , in which the compressor comprises straight blades.

11. The method according to claim 1 , in which the compressor comprises curved blades.