Method of building up an aluminum alloy part
View Patent ↗A method of building up an aluminum alloy part by welding is disclosed. The method includes the steps of manually depositing a layer of aluminum alloy powder on the part in a build-up zone and welding the powder layer onto the part by laser welding. A mask having an opening of dimensions corresponding to the dimensions of the build-up zone is positioned on the part and the layer of powder is deposited on the part both in the build-up zone and overlaps onto the mask around the build-up zone. The height of the powder layer relative to the surface of the part is calibrated prior to the welding step.
1. A method of building up an aluminum alloy part by welding and using a scraper that includes at least one support foot that rests an outer surface of said aluminum alloy part, and a scraper blade that is set back relative to the at least one support foot, the aluminum alloy part having a build-up zone to be built-up, the method comprising:
using a mask with an opening having substantially a same dimension as a peripheral section of the build-up zone, said mask having a predetermined thickness;
positioning the mask on said part by causing said opening to correspond with the build-up zone;
manually depositing a powder layer of aluminum alloy powder on the build-up zone, said powder layer overlapping onto said mask around said build-up zone;
placing the support foot of the scraper on the outer surface of said aluminum alloy part and smoothing the powder layer with the scraper to a calibrated height relative to the outer surface of said part, the calibrated height being larger than the thickness of the mask and the calibrated height corresponding to a distance between the scraper blade and the outer surface of said part; and
welding said powder layer onto said part by laser welding so as to build-up the build-up zone.
2. The method according to claim 1 , wherein the distance between the scraper blade and the outer surface of said part is adjustable, and said distance is adjusted to correspond to the calibrated height of the powder layer.
3. The method according to claim 1 , wherein, after the welding step, the part is leveled by machining in the build-up zone.
4. The method according to claim 1 , wherein said mask is made of aluminum alloy sheet.
5. The method according to claim 1 , wherein said part is a turbomachine part.
6. The method according to claim 1 , further comprising removing said mask after welding said powder layer onto said part by laser welding.
7. The method according to claim 1 , wherein the powder layer is welded onto said part and said mask by laser welding, the method further comprising removing the mask with the powder being welded thereon.
8. The method according to claim 1 , wherein the calibrated height of powder layer relative to the outer surface of said part is at least equal to a maximum depth of a depression in the build-up zone.
9. The method according to claim 1 , wherein the layer of aluminum alloy powder manually deposited on the build-up zone includes a first sublayer formed by a first plurality of beads of powder which are parallel and spaced apart at a pitch P, and a second sublayer formed by as second plurality of beads of powder which are spaced apart at the pitch P and offset by a distance P/2 relative to the first plurality of beads of powder.
10. The method according to claim 1 , wherein the support foot of the scraper includes a first vertical portion that extends vertically downwards and a second horizontal portion that forms a horizontal support strip which rests on the outer surface of said part.
11. The method according to claim 2 , wherein the scraper blade includes two oblong openings which are vertically oriented, and the scraper includes two screw-and-nut assemblies which are fastened in the scraper through the oblong openings.
12. The method according to claim 5 , wherein said part is a turbojet fan casing of a low pressure compressor module of a turbojet.
13. The method according to claim 12 , wherein said turbojet fan casing is built-up without removing said casing from the low pressure compressor module of the turbojet.
14. A method of building up an aluminum alloy turbojet fan casing of a low pressure compressor module of a turbojet by welding, said turbojet fan casing having a build-up zone to be built-up, the method comprising:
identifying the build-up zone to be built-up on said turbojet fan casing;
keeping said turbojet fan casing on the low pressure compressor module of the turbojet;
using a mask with an opening having substantially a same dimension as a peripheral section of the build-up zone, said mask having a predetermined thickness;
positioning the mask on said turbojet fan casing by causing said opening to correspond with the build-up zone;
manually depositing a powder layer of aluminum alloy powder on the build-up zone, said powder layer overlapping onto said mask around said build-up zone;
smoothing the powder layer to a calibrated height relative to an outer surface of said turbojet fan casing, the calibrated height being larger than the thickness of the mask; and
welding said powder layer onto said turbojet fan casing by laser welding without removing said turbojet fan casing from the low pressure compressor module of the turbojet.