Process for manufacturing hot-forged parts made of a magnesium alloy
View Patent ↗A process for manufacturing a process for manufacturing a part made of a magnesium alloy is disclosed. The process includes a step of forging a block of the alloy followed by a heat treatment. The alloy is a casting alloy based on 85% magnesium, and containing, by weight: 0.2 to 1.3% zinc; 2 to 4.5% neodymium; 0.2 to 7.0% rare-earth metal with an atomic number from 62 to 71; 0.2 to 1% zirconium. The forging is carried out at a temperature above 400° C. In particular the temperature is set between 420 and 430° C. and the forging step comprises a plastic deformation carried out at a slow rate. The process allows one to produce parts such as elements of casing for aeronautical machines, operating at a temperature of around 200° C. and having good aging properties.
1. A process for manufacturing a part made of a magnesium alloy, comprising:
forging a block of the magnesium alloy in a closed die; and
heat treating the forged block,
wherein the alloy is a casting alloy, comprising, by weight:
85% magnesium;
0.2 to 1.3% zinc;
2 to 4.5% neodymium;
0.2 to 7.0% rare-earth metal with an atomic number from 62 to 71; and
0.2 to 1% zirconium,
wherein
the forging comprises a plastic deformation obtained by conducting the forging at a temperature above 400° C., and
at a forging rate which is less than 40 mm/s, which is a rate of displacement of a forging slide of the closed die, and
wherein yield strength of the part is reduced by less than 15% after 10,000 hours of aging at 180° C.
2. The process as claimed in claim 1 , wherein the temperature of the forging is between 420 and 430° C.
3. The process as claimed in claim 1 , wherein the rate of displacement of the forging slide is between 10 and 30 mm/s.
4. The process as claimed in claim 3 , wherein the rate of displacement is 20 mm/s.
5. The process as claimed in claim 1 , wherein the block of the magnesium alloy is a cast block.
6. The process as claimed in claim 5 , wherein the cast block is pre-wrought prior to forging.
7. The process as claimed in claim 1 , wherein the heat treating comprises:
solution heat treating,
quenching, and
tempering at a temperature between 200° C. and 250° C.
8. The process as claimed in claim 7 , wherein the tempering temperature is between 200° C. and 225° C.
9. The process as claimed in claim 7 , wherein the tempering temperature is between 225° C. and 250° C.
10. The process as claimed in claim 1 , wherein
the zinc content is 0.2 to 0.5%,
the neodymium content is 2.6 to 3.1%, and
the gadolinium content is 1.0 to 1.7%.
11. The process as claimed in claim 1 , wherein a tensile strength of the obtained part is reduced by about 15% after 10,000 hours of aging at 180° C.
12. The process as claimed in claim 7 , wherein the tempering is conducted for a time greater than 16 hours.