CN104233132A - Heat treatment technology for improving room-temperature mechanical properties of copper-zinc-aluminium shape memory alloy - Google Patents
Heat treatment technology for improving room-temperature mechanical properties of copper-zinc-aluminium shape memory alloy Download PDFInfo
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Abstract
A heat treatment technology for improving room-temperature mechanical properties of copper-zinc-aluminium shape memory alloy is disclosed and belongs to the field of memory alloy. The technology is characterized by comprising firstly performing annealing processing on alloy obtained by using a casting method, keeping warm at 820 DEG C for 24 h, cooling along with the furnace temperature, then cutting and removing a zinc-removal layer with the thickness of 2-3 mm and casting defecting on the surface, then forging and rolling the ingot casting to prepare a plate with the thickness of 11 mm, and then employing a heat treatment technology of water quenching combined with two-stage aging treatment and oil quenching combined with two-stage aging treatment to process the plate.
Description
Technical field
The invention belongs to field of memory alloy, refer in particular to a kind of thermal treatment process improving copper-zinc-aluminum shape memory alloy room-temperature mechanical property.
Background technology
Copper-based shape memory alloy is one of the new function material of two active research and exploitations during the last ten years both at home and abroad in the past, finds that there is good shape memory effect at the tens of kinds of copper base alloys such as Cu-Zn, Cu-Zn-Al, Cu-Sn, Cu-Al-Ni, Cu-Al-Be, Cu-Sn-Si, Cu-Zn-Ga at present.Wherein most widely used is Cu-Zn-Al and Cu-Al-Ni system alloy.Although copper-based shape memory alloy has good shape memory effect and cheap price, prospect is very tempting, but due to the various defects of material itself, copper-based shape memory alloy also exists some problems in memory performance, mechanical property, limit its application and development in Practical Project.In order to improve ductility, suppress intercrystalline failure, improve fatigue lifetime and friction and wear behavior thereof, current main method has: 1. change alloy formula, 2. carries out refinement and Metamorphism treatment, 3. heat-treats.Wherein, first method realizes more complicated; It is obvious not that second method improves effect.Therefore, heat-treat nature and become the most effective means.
The present invention proposes a kind of thermal treatment process improving copper-zinc-aluminum shape memory alloy room-temperature mechanical property.
Summary of the invention
The present invention proposes a kind of thermal treatment process improving copper-zinc-aluminum shape memory alloy room-temperature mechanical property, it is characterized by: to the alloy obtained by castmethod, first carry out anneal, furnace cooling after being incubated 24 hours at 820 DEG C, then the dezincify layer and casting flaw of removing surface 2 ~ 3mm is cut, again ingot casting forged, be rolled into the thick sheet material of 11mm, then take two kinds of heat treatment modes respectively:
1, shrend adds two-stage ageing treatment, and namely 800-820 DEG C of insulation is quenched in room temperature water in 1 hour, takes out air cooling to room temperature after being then incubated 0.5 hour in preprepared 100 DEG C of boiling water, and then takes out air cooling to room temperature be incubated 0.5 hour in 50 DEG C of water after;
2, oil quenching adds two-stage ageing treatment, and namely 800-820 DEG C of insulation is quenched in room temperature machine oil for 1 hour, takes out air cooling to room temperature after being then incubated 0.5 hour in preprepared 100 DEG C of boiling water, and then takes out air cooling to room temperature be incubated 0.5 hour in 50 DEG C of water after;
The copper-zinc-aluminum shape memory alloy of room-temperature mechanical property excellence can be obtained by above method.
Embodiment
embodiment 1
Select that weight percent is Zn25.25 wt %, Al3.75 wt % respectively, Ni0.9 wt %, compound rare-earth 0.7 wt %(wherein: Nd 10 ~ 15wt%, La 10 ~ 15 wt%, Y 8 ~ 12wt%, Ce 8 ~ 12wt%, Tb 5 ~ 8 wt%, Gd 5 ~ 8 wt%, Pr+Sc+Eu+Ho+Er+Tm+Lu be 10 ~ 20wt%, Zr 3 ~ 6wt%, Ti 2 ~ 5wt%, B 2 ~ 5wt%, Yu Weitong.), surplus be the alloy of copper is test materials.Room-temperature mechanical property test is carried out respectively on WE-10 type fluid pressure type tensile testing machine and HB-3000 type Brinell testing machine.This strength of alloy 520.5MPa is recorded, elongation 7.5%, Brinell hardness 165HB without any thermal treatment.
embodiment 2
Select that weight percent is Zn25.25 wt %, Al3.75 wt % respectively, Ni0.9 wt %, compound rare-earth 0.7 wt %(wherein: Nd 10 ~ 15wt%, La 10 ~ 15 wt%, Y 8 ~ 12wt%, Ce 8 ~ 12wt%, Tb 5 ~ 8 wt%, Gd 5 ~ 8 wt%, Pr+Sc+Eu+Ho+Er+Tm+Lu be 10 ~ 20wt%, Zr 3 ~ 6wt%, Ti 2 ~ 5wt%, B 2 ~ 5wt%, Yu Weitong.), surplus be the alloy of copper is test materials.Room-temperature mechanical property test is carried out respectively on WE-10 type fluid pressure type tensile testing machine and HB-3000 type Brinell testing machine.Two-stage aging strengthening model is added through shrend, namely 800-820 DEG C of insulation is quenched in room temperature water in 1 hour, then air cooling is taken out to room temperature after being incubated 0.5 hour in preprepared 100 DEG C of boiling water, and then take out air cooling to room temperature be incubated 0.5 hour in 50 DEG C of water after, record this memorial alloy tensile strength 686.5MPa, elongation 8.9%, Brinell hardness 198HB.
embodiment 3
Select that weight percent is Zn25.25 wt %, Al3.75 wt % respectively, Ni0.9 wt %, compound rare-earth 0.7 wt %(wherein: Nd 10 ~ 15wt%, La 10 ~ 15 wt%, Y 8 ~ 12wt%, Ce 8 ~ 12wt%, Tb 5 ~ 8 wt%, Gd 5 ~ 8 wt%, Pr+Sc+Eu+Ho+Er+Tm+Lu be 10 ~ 20wt%, Zr 3 ~ 6wt%, Ti 2 ~ 5wt%, B 2 ~ 5wt%, Yu Weitong.), surplus be the alloy of copper is test materials.Room-temperature mechanical property test is carried out respectively on WE-10 type fluid pressure type tensile testing machine and HB-3000 type Brinell testing machine.Two-stage aging strengthening model is added through shrend, namely 800-820 DEG C of insulation is quenched in room temperature water in 1 hour, then air cooling is taken out to room temperature after being incubated 0.5 hour in preprepared 100 DEG C of boiling water, and then take out air cooling to room temperature be incubated 0.5 hour in 50 DEG C of water after, record this memorial alloy tensile strength 695.5MPa, elongation 9.5%, Brinell hardness 186HB.
Claims (2)
1. one kind is improved the thermal treatment process of copper-zinc-aluminum shape memory alloy room-temperature mechanical property, it is characterized by: to the alloy obtained by castmethod, first carry out anneal, furnace cooling after being incubated 24 hours at 820 DEG C, then the dezincify layer and casting flaw of removing surface 2 ~ 3mm is cut, again ingot casting is forged, be rolled into the sheet material that 11mm is thick, then two kinds of heat treatment modes are taked respectively: shrend adds two-stage ageing treatment, namely 800-820 DEG C of insulation is quenched in room temperature water in 1 hour, then air cooling is taken out to room temperature after being incubated 0.5 hour in preprepared 100 DEG C of boiling water, and then take out air cooling to room temperature be incubated 0.5 hour in 50 DEG C of water after, oil quenching adds two-stage ageing treatment, and namely 800-820 DEG C of insulation is quenched in room temperature machine oil for 1 hour, takes out air cooling to room temperature after being then incubated 0.5 hour in preprepared 100 DEG C of boiling water, and then takes out air cooling to room temperature be incubated 0.5 hour in 50 DEG C of water after.
2. a kind of thermal treatment process improving copper-zinc-aluminum shape memory alloy room-temperature mechanical property according to claim 1, thermal treatment process preferably can add two-stage ageing treatment by oil quenching, this memorial alloy tensile strength 695.5MPa after thermal treatment, elongation 9.5%, Brinell hardness 186HB.
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
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CN110527934A (en) * | 2019-10-14 | 2019-12-03 | 河北工业大学 | A kind of preparation method of high-intensity high-damping CuAlMn marmem |
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JPS6075561A (en) * | 1983-09-30 | 1985-04-27 | Sumitomo Special Metals Co Ltd | Heat treatment of shape memory cu alloy |
CN1792339A (en) * | 2005-10-25 | 2006-06-28 | 哈尔滨工程大学 | Method for making NiTi alloy ossicular fixator of easy taken-out type |
CN101033516A (en) * | 2006-12-29 | 2007-09-12 | 江苏大学 | Copper-zinc-aluminum shape memory alloy abrasion resistance material and manufacturing method for the same |
CN101050493A (en) * | 2007-05-16 | 2007-10-10 | 镇江忆诺唯记忆合金有限公司 | Shape memory alloy of composite rare earth, copper, zinc, and aluminum in use for fabricating dissipation of energy device of engineering structural framework |
CN101240388A (en) * | 2008-03-18 | 2008-08-13 | 镇江忆诺唯记忆合金有限公司 | Method for increasing composite rare earth copper-zinc-aluminum shape memory alloy double-pass memory effect |
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Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS6075561A (en) * | 1983-09-30 | 1985-04-27 | Sumitomo Special Metals Co Ltd | Heat treatment of shape memory cu alloy |
CN1792339A (en) * | 2005-10-25 | 2006-06-28 | 哈尔滨工程大学 | Method for making NiTi alloy ossicular fixator of easy taken-out type |
CN101033516A (en) * | 2006-12-29 | 2007-09-12 | 江苏大学 | Copper-zinc-aluminum shape memory alloy abrasion resistance material and manufacturing method for the same |
CN101050493A (en) * | 2007-05-16 | 2007-10-10 | 镇江忆诺唯记忆合金有限公司 | Shape memory alloy of composite rare earth, copper, zinc, and aluminum in use for fabricating dissipation of energy device of engineering structural framework |
CN101240388A (en) * | 2008-03-18 | 2008-08-13 | 镇江忆诺唯记忆合金有限公司 | Method for increasing composite rare earth copper-zinc-aluminum shape memory alloy double-pass memory effect |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
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CN110527934A (en) * | 2019-10-14 | 2019-12-03 | 河北工业大学 | A kind of preparation method of high-intensity high-damping CuAlMn marmem |
CN110527934B (en) * | 2019-10-14 | 2020-08-04 | 河北工业大学 | Preparation method of high-strength high-damping CuAlMn shape memory alloy |
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Application publication date: 20141224 |