EP0297004B1 - Utilisation d'un procédé pour améliorer la ductilité d'un produit en alliage à transformation martensitique - Google Patents
Utilisation d'un procédé pour améliorer la ductilité d'un produit en alliage à transformation martensitique Download PDFInfo
- Publication number
- EP0297004B1 EP0297004B1 EP88420216A EP88420216A EP0297004B1 EP 0297004 B1 EP0297004 B1 EP 0297004B1 EP 88420216 A EP88420216 A EP 88420216A EP 88420216 A EP88420216 A EP 88420216A EP 0297004 B1 EP0297004 B1 EP 0297004B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- treatment
- product
- use according
- temperature
- hot
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 229910000734 martensite Inorganic materials 0.000 title claims description 23
- 230000009466 transformation Effects 0.000 title claims description 22
- 229910045601 alloy Inorganic materials 0.000 title claims description 17
- 239000000956 alloy Substances 0.000 title claims description 17
- 238000000034 method Methods 0.000 title description 13
- 230000008569 process Effects 0.000 title description 11
- 238000011282 treatment Methods 0.000 claims description 73
- 238000010438 heat treatment Methods 0.000 claims description 20
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims description 16
- 229910001285 shape-memory alloy Inorganic materials 0.000 claims description 9
- 229910004337 Ti-Ni Inorganic materials 0.000 claims description 8
- 229910011209 Ti—Ni Inorganic materials 0.000 claims description 8
- KHYBPSFKEHXSLX-UHFFFAOYSA-N iminotitanium Chemical compound [Ti]=N KHYBPSFKEHXSLX-UHFFFAOYSA-N 0.000 claims description 8
- 238000001953 recrystallisation Methods 0.000 claims description 8
- 239000007788 liquid Substances 0.000 claims description 7
- 229910052757 nitrogen Inorganic materials 0.000 claims description 7
- 229910017773 Cu-Zn-Al Inorganic materials 0.000 claims description 5
- 238000010791 quenching Methods 0.000 claims description 5
- 230000000171 quenching effect Effects 0.000 claims description 5
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 5
- 229910017535 Cu-Al-Ni Inorganic materials 0.000 claims description 4
- 229910052759 nickel Inorganic materials 0.000 claims description 4
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 claims description 3
- 229910019819 Cr—Si Inorganic materials 0.000 claims description 3
- 229910018643 Mn—Si Inorganic materials 0.000 claims description 3
- 235000011089 carbon dioxide Nutrition 0.000 claims description 3
- 239000002826 coolant Substances 0.000 claims description 3
- 229910052748 manganese Inorganic materials 0.000 claims description 2
- 239000000047 product Substances 0.000 description 24
- 230000006872 improvement Effects 0.000 description 8
- 230000000694 effects Effects 0.000 description 7
- PXHVJJICTQNCMI-UHFFFAOYSA-N nickel Substances [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 7
- 239000011265 semifinished product Substances 0.000 description 6
- 238000000265 homogenisation Methods 0.000 description 5
- 238000009864 tensile test Methods 0.000 description 5
- 229910052782 aluminium Inorganic materials 0.000 description 4
- XEEYBQQBJWHFJM-UHFFFAOYSA-N iron Substances [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 4
- 230000007704 transition Effects 0.000 description 4
- 229910052802 copper Inorganic materials 0.000 description 3
- 239000010949 copper Substances 0.000 description 3
- 238000002425 crystallisation Methods 0.000 description 3
- 230000008025 crystallization Effects 0.000 description 3
- 229910052742 iron Inorganic materials 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 3
- 230000004048 modification Effects 0.000 description 3
- 238000012986 modification Methods 0.000 description 3
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 2
- 238000000137 annealing Methods 0.000 description 2
- 229910001566 austenite Inorganic materials 0.000 description 2
- 230000008901 benefit Effects 0.000 description 2
- 239000003795 chemical substances by application Substances 0.000 description 2
- 238000007654 immersion Methods 0.000 description 2
- 229910001092 metal group alloy Inorganic materials 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 238000005507 spraying Methods 0.000 description 2
- 230000006641 stabilisation Effects 0.000 description 2
- 239000010935 stainless steel Substances 0.000 description 2
- 229910001220 stainless steel Inorganic materials 0.000 description 2
- 229910052726 zirconium Inorganic materials 0.000 description 2
- 229910017767 Cu—Al Inorganic materials 0.000 description 1
- 241000135309 Processus Species 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 238000009533 lab test Methods 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 230000000750 progressive effect Effects 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 238000002791 soaking Methods 0.000 description 1
- 238000009987 spinning Methods 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
- 238000007669 thermal treatment Methods 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 229910052725 zinc Inorganic materials 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/006—Resulting in heat recoverable alloys with a memory effect
Definitions
- the present invention relates to the use of a heat treatment for improving the ductility of a semi-finished metal alloy with martensitic transformation by means of a succession of hot and cold treatments, in particular to facilitate the transformation of semi-finished products into shape memory alloy.
- Document EP-A-0 161 952 discloses a process for educating a metal alloy object with martensitic transformation "with shape memory", this process consisting in imposing on the object, over one or more cycles , a series of thermal and / or mechanical stresses, the object being for example, in each cycle, treated in the austenitic phase then deformed and cooled in the martensitic phase. This education process is used to impart better memory accuracy.
- alloys with martensitic transformation exhibit poor cold deformability, which is particularly troublesome when they have to be delivered in half: products of thick or small diameter, for example between 0.5 and 3 mm.
- This insufficient ductility with respect to deformations such as rolling, drawing, drawing or hammering particularly affects the transformation into semi-finished products of certain shape memory alloys.
- alloys of the Ti-Ni 50/50 at% and Cu-Al 14 at% -Ni 4 at% types typically have deformation rates between anneals of 10% or less, which makes their cold transformation excessively long and expensive.
- the subject of the invention is the use of a heat treatment of a semi-product in martensitic transformation alloy, comprising in succession a cold treatment below the temperature M s of the start of martensitic transformation of the semi-product and a hot treatment at a temperature at least equal to 700 ° C., in order to improve the ductility of said semi-finished product with regard to its successive working, characterized in that after working said semi-working, it is subjected to a cycle of said heat treatment , the cold treatment of said cycle being carried out at a temperature both below -50 ° C and (M s -50 ° C), and the hot treatment does not result in recrystallization of the product unless it is the last heat treatment.
- Said semi-finished product is optionally subjected to at least one additional cycle following said first cycle, the cold treatment of this additional cycle being at a temperature below both -50 ° C and (M s -30 ° C) and its treatment hot being at temperature at least equal to 600 ° C. and not causing the recrystallization of said semi-finished product when it is not the last heat treatment.
- the cold and hot treatments of the successive cycles are alternated.
- each hot or cold heat treatment After each hot or cold heat treatment, the product is usually brought back to room temperature for practical reasons.
- Each hot treatment has an effect of homogenization and relaxation of internal constraints, incomplete relaxation since there is no recrystallization, the residual stresses then having a favorable effect for the cold treatment which follows it.
- Each cold treatment leads to a crystallization of fine martensite, and the succession of treatments results in homogenization with softening of the matrix and, in the martensitic phase, an increasingly fine crystallization and tending towards isotropy.
- the method of the invention makes it possible to obtain, in one or more cycles depending on the alloy considered, an exceptional ductility resulting, for example, by a multiplication by 3 of the elongation at break of the tensile test, the improvement product ductility at martensitic transformation treated is progressive, the improvement effect of each of the successive cycles decreasing, so that in practice we can limit our to at most 5 cycles and typically to 3 cycles, 80 to 95% of the improvement possible ductility then being obtained.
- the minimum temperature of the hot treatment (s) can be compared to "M s " like the temperature of the cold treatment (s) during any subsequent cycles, this hot treatment temperature then remaining at least equal to 600 ° C.
- the product in order to maintain the homogenized or partially homogenized state produced by the hot treatment or by each of the hot treatments, it is preferable to cool the product by quenching, typically a quenching with water, after this or these hot treatments .
- the product to be treated When the product to be treated is in the hot-worked state, it is it is it is preferable to start the first cycle of treatments according to the invention, which may be the only cycle of treatments, with its cold treatment.
- the heat treatments of the invention can be brief, which is a great advantage for industrial manufacturing: typically from a few seconds to 5 min for cold treatments, from 30 s to 20 min for hot treatments, processed products most often having a diameter or thickness of between 0.2 and 20 mm.
- Common cooling agents for cold treatments are liquid nitrogen (-196 ° C) and dry ice (-70 ° C), the former making it possible to treat all temperature alloys under good conditions " M s "at least equal to -145 ° C.
- Cold treatments can be carried out by soaking in the cooling agent or by passing through this agent, or by spraying this agent.
- Washers 3 mm thick cut from the bars of the three compositions were each co-laminated at around 900 ° C. between two stainless steel washers of the AISI 304 type. The assessment of the ductility is then made by simple test of folding. The laminated washers, separated from their stainless steel covers, were then immersed 3 to 4 min in liquid nitrogen, then after returning to the ambient treated 1 min at a temperature between 800 ° and 900 ° C and quenched at water, all of these cold and hot treatments constituting the first cycle of the process according to the invention. An increase in the ductility was not very noticeable for (CI) whose cold treatment temperature is 46 ° C below M s , and very clear for (C2) and (C3).
- the sequence (T3) in this case shows the surprising effect on A% of a single cycle of heat treatments according to the invention.
- the temperature at the start of recrystallization for a hot treatment of 10 min is, for the present alloy, from 910 to 920 ° C. and that risks of burns appear only above 950 ° C.
- the considerable increase in tensile elongation here corresponds to a possibility of deformation with elongation of approximately 35%, before the following annealing or softening heat treatment, instead of less than 10% previously.
Landscapes
- Chemical & Material Sciences (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Heat Treatment Of Steel (AREA)
- Heat Treatment Of Articles (AREA)
- Heat Treatment Of Sheet Steel (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8709272A FR2617187B1 (fr) | 1987-06-24 | 1987-06-24 | Procede d'amelioration de la ductilite d'un produit en alliage a transformation martensitique et son utilisation |
FR8709272 | 1987-06-24 |
Publications (3)
Publication Number | Publication Date |
---|---|
EP0297004A2 EP0297004A2 (fr) | 1988-12-28 |
EP0297004A3 EP0297004A3 (en) | 1989-06-28 |
EP0297004B1 true EP0297004B1 (fr) | 1991-05-08 |
Family
ID=9352719
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP88420216A Expired - Lifetime EP0297004B1 (fr) | 1987-06-24 | 1988-06-22 | Utilisation d'un procédé pour améliorer la ductilité d'un produit en alliage à transformation martensitique |
Country Status (5)
Country | Link |
---|---|
US (1) | US4878954A (enrdf_load_stackoverflow) |
EP (1) | EP0297004B1 (enrdf_load_stackoverflow) |
JP (1) | JPS6421042A (enrdf_load_stackoverflow) |
DE (1) | DE3862691D1 (enrdf_load_stackoverflow) |
FR (1) | FR2617187B1 (enrdf_load_stackoverflow) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0328319A (ja) * | 1989-06-26 | 1991-02-06 | Nisshin Steel Co Ltd | ステンレス鋼製のパイプ継手およびその製造法 |
JPH0645822B2 (ja) * | 1990-04-18 | 1994-06-15 | 川崎製鉄株式会社 | マルテンサイト系ステンレス鋼管の製造方法 |
FR2699263B1 (fr) * | 1992-12-15 | 1995-01-27 | Cryotechnologies | Refroidisseur muni d'un doigt froid équipé d'un coupleur thermique. |
US6106642A (en) | 1998-02-19 | 2000-08-22 | Boston Scientific Limited | Process for the improved ductility of nitinol |
US6149742A (en) * | 1998-05-26 | 2000-11-21 | Lockheed Martin Corporation | Process for conditioning shape memory alloys |
WO2003064717A1 (en) * | 2002-02-01 | 2003-08-07 | Mide Technology Corporation | Enhery aborbring shape memory alloys |
DE102004052962A1 (de) * | 2004-10-29 | 2006-05-04 | Linde Ag | Absperrarmatur und Verfahren zur Herstellung einer Absperrarmatur |
CN102011038B (zh) * | 2010-12-15 | 2012-02-29 | 河北师范大学 | Mn50Ni50-xAlx高温铁磁形状记忆合金材料及其制备方法 |
CN114570948B (zh) * | 2022-02-15 | 2023-04-11 | 中南大学 | 一种对增材制造形状记忆合金零件控形的后处理方法 |
CN115807199B (zh) * | 2022-11-24 | 2023-12-22 | 新疆大学 | 一种同时提高块体非晶合金复合材料屈服强度和塑性的方法 |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4067752A (en) * | 1973-11-19 | 1978-01-10 | Raychem Corporation | Austenitic aging of metallic compositions |
EP0035069B1 (de) * | 1980-03-03 | 1983-12-21 | BBC Aktiengesellschaft Brown, Boveri & Cie. | Formgedächtnislegierung auf der Basis von Cu/Al oder Cu/Al/Ni und Verfahren zur Stabilisierung des Zweiwegeffektes |
US4304613A (en) * | 1980-05-12 | 1981-12-08 | The United States Of America As Represented By The Secretary Of The Navy | TiNi Base alloy shape memory enhancement through thermal and mechanical processing |
JPS58151445A (ja) * | 1982-02-27 | 1983-09-08 | Tohoku Metal Ind Ltd | 可逆形状記憶効果を有するチタンニツケル合金およびその製造方法 |
EP0095798B1 (en) * | 1982-05-13 | 1987-04-08 | Leuven Research & Development V.Z.W. | Process for thermally treating heat recoverable metallic articles and articles thereby obtained |
US4502896A (en) * | 1984-04-04 | 1985-03-05 | Raychem Corporation | Method of processing beta-phase nickel/titanium-base alloys and articles produced therefrom |
FR2563055A1 (fr) * | 1984-04-12 | 1985-10-18 | Souriau & Cie | Procede de realisation de connecteur |
DE3573932D1 (en) * | 1984-09-07 | 1989-11-30 | Nippon Steel Corp | Shape memory alloy and method for producing the same |
JPS63654A (ja) * | 1986-06-19 | 1988-01-05 | Fujitsu Ltd | プロセッサ間の通信制御方法 |
JP2606842B2 (ja) * | 1987-05-30 | 1997-05-07 | 株式会社東芝 | 電気掃除機 |
JP2506853B2 (ja) * | 1987-11-25 | 1996-06-12 | 松下電器産業株式会社 | 調理器 |
-
1987
- 1987-06-24 FR FR8709272A patent/FR2617187B1/fr not_active Expired
-
1988
- 1988-06-17 US US07/208,035 patent/US4878954A/en not_active Expired - Fee Related
- 1988-06-22 EP EP88420216A patent/EP0297004B1/fr not_active Expired - Lifetime
- 1988-06-22 DE DE8888420216T patent/DE3862691D1/de not_active Expired - Fee Related
- 1988-06-22 JP JP63154540A patent/JPS6421042A/ja active Granted
Also Published As
Publication number | Publication date |
---|---|
DE3862691D1 (de) | 1991-06-13 |
JPS6421042A (en) | 1989-01-24 |
US4878954A (en) | 1989-11-07 |
EP0297004A2 (fr) | 1988-12-28 |
FR2617187A1 (fr) | 1988-12-30 |
EP0297004A3 (en) | 1989-06-28 |
JPH036986B2 (enrdf_load_stackoverflow) | 1991-01-31 |
FR2617187B1 (fr) | 1989-10-20 |
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