Bearing support for an aircraft engine manufactured by additive manufacturing
A bearing support for an aircraft engine, manufactured, in one piece, by powder-bed additive manufacturing from a manufacturing platform, including a cylindrical element including an annular stiffener with a cross-section that changes along its circumference, this stiffener being formed with alternating portions having a Γ-shaped cross-section, needing to be supported during the manufacture, and portions having a Y-shaped cross-section that are not supported during the manufacture.
1. A bearing support for an aircraft engine, manufactured in one piece by a powder-bed additive manufacturing from a manufacturing platform, comprising a cylindrical element including an annular stiffener with a cross-section that changes along a circumference of the annular stiffener, said stiffener being formed with a plurality of first portions having a first cross-section, as a first radial cross-section of the cylindrical element, of a shape corresponding to letter Γ needing to be supported during the additive manufacturing, alternating with a plurality of second portions having a second cross-section, as a second radial cross-section of the cylindrical element, of a shape corresponding to letter Y not supported during the additive manufacturing.
2. The bearing support according to claim 1 , wherein each of the second portions comprises a first ramp that extends beyond the cylindrical element and a second ramp that extends beyond the first ramp to join the cylindrical element.
3. The bearing support according to claim 1 , wherein the cylindrical element comprises a recess at each of the second portions.
4. The bearing support according to claim 1 , wherein at least one of the first portions forms a fastening portion coming from a machining of an excess thickness formed by the additive manufacturing.
5. An aircraft engine comprising the bearing support according to claim 1 .
6. A method for obtaining, via the additive manufacturing, the bearing support according to claim 1 , said method comprising a step of forming, by the additive manufacturing, a blank part in a single piece on the manufacturing platform, and a step of manufacturing the stiffener comprising forming supports that support only the first portions.