Method of manufacturing a component covered with an abradable coating

1. A method of fabricating a part covered in an abradable coating, the method comprising the following steps:

providing a blank for the part, the blank having a housing opening out into the surface of the blank through at least one opening;

filling the housing with an abradable material in powder form; and

hot-rolling the blank and the abradable material together so as to sinter the abradable material and cause it to adhere to the blank, in order to obtain an abradable coating,

wherein, during the rolling step, pressure is exerted on the abradable material through the opening.

2. A fabrication method according to claim 1 , wherein said housing is filled with the abradable material through the opening, and wherein the opening is closed hermetically with a sheath before the rolling step.

3. A fabrication method according to claim 1 , wherein:

the opening is covered with a sheath that presents at least one vacuum orifice and at least one filling orifice;

a vacuum is established inside said housing by using said vacuum orifice, and said housing is filled with the abradable material by using said filling orifice; and

said vacuum orifice and said filling orifice are closed in leaktight manner before the rolling step.

4. A fabrication method according to claim 1 , wherein the rolling step comprises a preheating first step during which the blank is heated to a rolling temperature, with the sintering of the abradable material taking place, at least in part, during this first step, and a second step during which the blank and the abradable material are rolled together at the rolling temperature.

5. A fabrication method according to claim 1 , wherein during the step of filling the housing, the abradable material is deposited as a plurality of layers of different kinds.

6. A fabrication method according to claim 1 , wherein the abradable material in powder form comprises a base powder that, after sintering, constitutes the matrix of the abradable coating, together with secondary particles mixed with the base powder and facilitating fragmentation of the abradable coating.

7. A fabrication method according to claim 1 , wherein said housing is a groove defined by a bottom wall, two side walls surrounding the bottom wall, and two outer lips situated extending the side walls towards the center of the groove in such a manner that the groove presents a generally C-shaped profile in cross-section.

8. A fabrication method according to claim 1 , wherein the blank is formed by hot rolling together at least two sub-portions, and wherein the step of rolling together the sub-portions and the step of rolling together the blank and the abradable material are performed simultaneously as a single operation.

9. A fabrication method according to claim 1 , wherein after the rolling step, the blank and/or the coating of abradable material is/are machined.

10. A fabrication method according to claim 1 , wherein, during the rolling step, one of the rolling mandrels is in contact with the surface into which the housing opens out and exerts a pressure thereon.

11. A fabrication method according to claim 1 , wherein the fabricated part is a turbomachine casing having a radially inner face, at least a portion of the radially inner face being covered by the abradable coating.