EP0035601A1 - Procédé de fabrication d'un alliage-mémoire - Google Patents

Procédé de fabrication d'un alliage-mémoire Download PDF

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Publication number
EP0035601A1
EP0035601A1 EP80200184A EP80200184A EP0035601A1 EP 0035601 A1 EP0035601 A1 EP 0035601A1 EP 80200184 A EP80200184 A EP 80200184A EP 80200184 A EP80200184 A EP 80200184A EP 0035601 A1 EP0035601 A1 EP 0035601A1
Authority
EP
European Patent Office
Prior art keywords
powder
copper
temperature
stream
weight
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.)
Granted
Application number
EP80200184A
Other languages
German (de)
English (en)
Other versions
EP0035601B1 (fr
Inventor
Keith Dr. Melton
Olivier Dr. Mercier
Helmut Dr. Riegger
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
BBC Brown Boveri AG Switzerland
Original Assignee
BBC Brown Boveri AG Switzerland
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by BBC Brown Boveri AG Switzerland filed Critical BBC Brown Boveri AG Switzerland
Priority to EP80200184A priority Critical patent/EP0035601B1/fr
Priority to DE8080200184T priority patent/DE3065931D1/de
Priority to JP2850481A priority patent/JPS56136942A/ja
Priority to US06/239,626 priority patent/US4365996A/en
Publication of EP0035601A1 publication Critical patent/EP0035601A1/fr
Application granted granted Critical
Publication of EP0035601B1 publication Critical patent/EP0035601B1/fr
Expired legal-status Critical Current

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Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/006Resulting in heat recoverable alloys with a memory effect
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/04Making non-ferrous alloys by powder metallurgy
    • C22C1/0425Copper-based alloys

Definitions

  • the invention is based on a method for producing a memory alloy according to the preamble of claim 1.
  • Memory alloys based on the Cu / Al / Ni system are known and have been described in various publications (e.g. U.S. Patent No. 3,783,037). Such memory alloys, which belong to the general type with the ⁇ high-temperature phase, are generally produced by melt metallurgy.
  • the invention has for its object to provide a manufacturing method for memory alloys based on copper, aluminum and nickel, which leads to dense, compact bodies with good mechanical properties and at the same time to exactly reproducible values of the transition temperature and other variables related to the memory effect.
  • the essence of the new process is not to start from elementary powders or from a starting powder corresponding to the final alloy, but to use a mixture of pre-alloyed powders and specially composed powder mixtures. This allows the required ductility to be optimally adapted to the processing process with extensive freedom in terms of composition.
  • the grain size of the crystallite of the finished body can largely be predetermined. Grain growth is not to be feared. Coherent oxide skins that prevent homogenization and impair mechanical properties are avoided. If a certain small percentage is present, the metal oxides are present in finely divided form as dispersoids and have a beneficial effect on the mechanical properties of the end product, preventing grain growth.
  • the following sample was mixed in a tumble mixer for 10 min: 240 g of this powder mixture were filled into a rubber tube with an inner diameter of 20 mm and pressed isostatically at a pressure of 8000 bar to a cylinder with a diameter of 18 mm and a height of 220 mm.
  • the green compact was reduced and presintered in a hydrogen stream at a temperature of 950 ° C. for 1 h and then sintered in a stream of argon at a temperature of 950 ° C. for 19 h.
  • the raw sintered body was turned to a diameter of 17 mm and introduced into a soft-annealed copper tube with an outer diameter of 20 mm and completely encapsulated by covering the ends with plugs and soldering under an argon atmosphere.
  • thermomechanical processing consisted of round hammering at 950 ° C, with the diameter of the rod being 18 mm in the first round hammering stitch and every subsequent one Stitch was reduced by 2 mm each.
  • the procedure was such that 2 thermomechanical operations were followed by homogenization annealing.
  • the rod hammered down to 8 mm in diameter was finally subjected to a final annealing in a stream of argon for 15 minutes at a temperature of 950 ° C. and immediately quenched in water.
  • the test showed a density of 99.5 - 99.8% of the theoretical value for the workpiece.
  • thermomechanical machining / homogenization can be continued for as long as required until the final shape of the workpiece is reached. When the theoretical density is reached, further homogenization is generally no longer necessary.
  • Example I The powders given in Example I were weighed out as follows and mixed in a tumble mixer for 15 minutes: 240 g of this powder mixture were filled into a soft annealed copper tube with an inner diameter of 18 mm and a wall thickness of 2 mm and completely encapsulated by covering the ends and soldering under an argon atmosphere. The tube and powder were then isostatically pressed at a pressure of 10,000 bar, and the compact was reduced and presintered in a hydrogen / nitrogen stream at a temperature of 750 ° C. for 2 h and then in a stream of argon at a temperature of 800 ° C. for 25 h sintered.
  • the workpiece was then alternately subjected to 2 round hammer operations and a homogenization anneal at 900 ° C each, similar to Example I.
  • the rod hammered down to 6 mm was subjected to a final annealing at 1000 ° C. for 10 minutes in a stream of argon and quenched in water.
  • the density was 99.5% of the theoretical value.
  • Example I The powders given in Example I were weighed out as follows and mixed in a tumble mixer for 12 minutes: 240 g of this powder mixture were filled into a soft annealed tombac tube with an inner diameter of 20 mm and a wall thickness of 1.6 mm and completely encapsulated by covering the ends and soldering under an argon atmosphere. The tube and powder were then isostatically pressed at a pressure of 12,000 bar and the compact was reduced and presintered in a hydrogen stream at a temperature of 850 ° C. for 1 Y2 h and then sintered in a stream of argon at a temperature of 820 ° C. for 22 h.
  • the workpiece was then reduced in 2 round hammer passes at a temperature of 900 C to 18 or 16 mm in diameter and homogenized in a stream of argon at 920 ° C for 1 h. This was followed by two round hammer stitches at 900 ° C, so that the rod finally had a diameter of 13 mm.
  • the rod was rolled down in several successive hot rolling operations, each with 20-25% reduction in cross section, to form a strip 1.5 mm thick and 20 mm wide. After a final annealing at 950 ° C. for 12 minutes, the strip was quenched in water. The density of the finished tape was 99.7%.
  • Example I The powders given in Example I were weighed out as follows and mixed in a tumble mixer for 10 min. 250 g of this powder mixture were filled into a rubber tube with an inner diameter of 35 mm and pressed isostatically at a pressure of 12,000 bar to a cylinder with a diameter of 31 mm and a height of 80 mm. The green compact was reduced in a hydrogen stream at a temperature of 920 ° C. for 1 h and presintered and then sintered in a stream of argon at a temperature of 950 ° C. for 20 h. The raw sintered body was turned to a diameter of 30 mm, inserted in the recipient of an extrusion press and pressed at a temperature of 780 ° C.
  • the reduction ratio (decrease in cross-section) was 11: 1.
  • the rod was then homogenized at a temperature of 920 ° C. for 30 minutes and then pulled down in 2 passes on a warming bench at a temperature of 750 ° C. to an edge length of 6 mm. After the final one Annealing at 900 ° C for 15 min in a stream of argon, the rod was quenched in water. The density of the finished rod was 99.8% of the theoretical value.
  • Example 1 The powders given in Example 1 were weighed out as follows and mixed in a tumble mixer for 15 minutes: 1000 g of this powder mixture were filled into a plastic tube with an inner diameter of 66 mm and pressed isostatically at a pressure of 12,000 bar into a cylinder with a diameter of 60 mm and a height of 80 mm.
  • the green compact was reduced in a hydrogen / nitrogen stream at a temperature of 880 ° C. for 1 h and presintered and then sintered in a stream of argon at a temperature of 930 ° C. for 25 h.
  • the raw sintered body was turned to a diameter of 58 mm, in a soft-annealed box made of soft iron with an outer diameter of 64 mm was inserted and completely encapsulated by placing the lid and soldering in an argon atmosphere.
  • the workpiece produced in this way was subjected to thermomechanical processing under a hot press, interrupted by homogenization annealing. By alternately upsetting and annealing at 900 ° C, the height of the cylinder was successively reduced to approx. 32 mm, whereby the material condensed to approx. 95% of the theoretical density and now the die. had a corresponding diameter of 70 mm. After an additional homogenization annealing at 950 ° C.
  • the preformed circular plate with parallel flat end faces was turned into a forge with a reduced diameter.
  • the 20 mm thick plate had a radial bead of 5 x 5 mm on the upper side and a central recess of 20 mm diameter and 5 mm axial depth on the lower side.
  • the plate was quenched in water. The density was 99.2 - 99.5% of the theoretical value.
  • the powder mixtures can be within the following limits:
  • Isotatic pressing preferably requires pressures of at least 8000 bar.
  • the reduction and presintering of the compact can expediently take place in the temperature range from 700 to 1000 ° C. for at least 30 minutes in a stream of hydrogen or hydrogen / nitrogen.
  • the sintering of the compact must be carried out above the temperature of the eutectoid transformation, ie at a temperature of at least 700 ° C. for 10 hours in an argon flow to achieve the most homogeneous structure possible.
  • thermomechanical processing which can consist of hot pressing, hot extrusion, hot forging, hot rolling, hot drawing and / or hot round hammering, should be carried out at temperatures between 700 and 1000 ° C, as well as the intermediate homogenization in the inert gas flow (intermediate annealing) at at least 700 ° C for at least 30 min.
  • the final annealing in a stream of argon is carried out at temperatures between 700 and 1050 ° C ( ⁇ mixed crystal region) for 10 to 15 minutes and the workpiece is then immediately quenched in water.
  • thermomechanical processing it is advisable to encapsulate the material beforehand in a ductile metallic shell that does not chemically react with it, which is removed mechanically or chemically at the end of the shaping as a surface layer in most applications.
  • Soft-annealed metals and alloys such as copper, copper alloys and soft iron are particularly suitable as materials for the casing. Encapsulation can take place immediately before the thermomechanical processing, in that the sintered body undergoes a mechanical surface treatment beforehand by turning, milling, planing, etc., or the powder can be filled directly into a suitable tube, a can, etc., instead of into a rubber or plastic tube will.
  • the powder metallurgical method according to the invention enables the production of workpieces from a memory alloy of the Cu / Al and Cu / Al / Ni type, which are produced in a conventional manner, ie by melt metallurgy Bodies have a fine-grained structure and optionally contain dispersoids in the form of finely divided oxide particles.
  • the mechanical properties, in particular the elongation, notch toughness and the working capacity of such workpieces are significantly better than those of cast and / or hot-kneaded bodies. This opens up a further area of application for this type of alloy.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Powder Metallurgy (AREA)
  • Heat Treatment Of Nonferrous Metals Or Alloys (AREA)
EP80200184A 1980-03-03 1980-03-03 Procédé de fabrication d'un alliage-mémoire Expired EP0035601B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
EP80200184A EP0035601B1 (fr) 1980-03-03 1980-03-03 Procédé de fabrication d'un alliage-mémoire
DE8080200184T DE3065931D1 (en) 1980-03-03 1980-03-03 Process for making a memory alloy
JP2850481A JPS56136942A (en) 1980-03-03 1981-03-02 Production of copper - aluminum - nickel memory alloy
US06/239,626 US4365996A (en) 1980-03-03 1981-03-02 Method of producing a memory alloy

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP80200184A EP0035601B1 (fr) 1980-03-03 1980-03-03 Procédé de fabrication d'un alliage-mémoire

Publications (2)

Publication Number Publication Date
EP0035601A1 true EP0035601A1 (fr) 1981-09-16
EP0035601B1 EP0035601B1 (fr) 1983-12-21

Family

ID=8186966

Family Applications (1)

Application Number Title Priority Date Filing Date
EP80200184A Expired EP0035601B1 (fr) 1980-03-03 1980-03-03 Procédé de fabrication d'un alliage-mémoire

Country Status (4)

Country Link
US (1) US4365996A (fr)
EP (1) EP0035601B1 (fr)
JP (1) JPS56136942A (fr)
DE (1) DE3065931D1 (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0045985A1 (fr) * 1980-08-07 1982-02-17 BBC Aktiengesellschaft Brown, Boveri & Cie. Procédé de fabrication d'un alliage à mémoire à base de cuivre
EP0086012A3 (en) * 1982-02-05 1983-09-21 Bbc Aktiengesellschaft Brown, Boveri & Cie. Process for generating a reversible two-way memory effect in a component made from an alloy showing a one-way effect
EP0035070B1 (fr) * 1980-03-03 1985-05-15 BBC Aktiengesellschaft Brown, Boveri & Cie. Alliage-mémoire à base d'une solution solide riche en cuivre ou en nickel

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6029406A (ja) * 1983-07-27 1985-02-14 Tohoku Metal Ind Ltd 焼結体の製造方法
US4464205A (en) * 1983-11-25 1984-08-07 Cabot Corporation Wrought P/M processing for master alloy powder
US4759293A (en) * 1986-06-30 1988-07-26 Davis Jr Thomas O Article using shape-memory alloy to improve and/or control the speed of recovery
US4839479A (en) * 1986-06-30 1989-06-13 Davis Jr Thomas O Article using shape-memory alloy to improve and/or control the speed of recovery
US4836979A (en) * 1988-06-14 1989-06-06 Inco Limited Manufacture of composite structures
US5443615A (en) * 1991-02-08 1995-08-22 Honda Giken Kogyo Kabushiki Kaisha Molded ceramic articles
JPH083133B2 (ja) * 1990-07-12 1996-01-17 日立粉末冶金株式会社 船外機用バルブシート材およびその製造方法
US5344605A (en) * 1991-11-22 1994-09-06 Sumitomo Electric Industries, Ltd. Method of degassing and solidifying an aluminum alloy powder
US6132486A (en) * 1998-11-09 2000-10-17 Symmco, Inc. Powdered metal admixture and process
JP4424810B2 (ja) * 2000-03-27 2010-03-03 株式会社小松製作所 焼結材料
US6548013B2 (en) * 2001-01-24 2003-04-15 Scimed Life Systems, Inc. Processing of particulate Ni-Ti alloy to achieve desired shape and properties
JP4282284B2 (ja) * 2001-08-22 2009-06-17 株式会社小松製作所 履帯
DE102005032544B4 (de) * 2004-07-14 2011-01-20 Hitachi Powdered Metals Co., Ltd., Matsudo Abriebsresistente gesinterte Aluminiumlegierung mit hoher Festigkeit und Herstellugsverfahren hierfür
US10245639B2 (en) * 2012-07-31 2019-04-02 United Technologies Corporation Powder metallurgy method for making components
DE112020006054T5 (de) 2019-12-11 2022-12-29 Diamet Corporation Verfahren zur Herstellung einer Cu-Ni-Al-basierten Sinterlegierung
CN113684389B (zh) * 2021-08-16 2022-07-29 大连大学 一种控制γ相分布提高Co-Ni-Al磁记忆合金超弹性的方法

Citations (5)

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Publication number Priority date Publication date Assignee Title
DE2129125A1 (de) * 1970-06-11 1971-12-16 Olin Corp Verfahren zur Verarbeitung von Aluminiumbronzen
US3783037A (en) * 1969-11-12 1974-01-01 Fulmer Res Inst Ltd Treatment of alloys
DE2006066B2 (de) * 1969-03-03 1975-01-16 Allmaenna Svenska Elektriska Ab, Vaesteraas (Schweden) Verfahren zum isostatischen Heißpressen von aus pulverförmigem Material vorgepreßten Körpern und Ofen zur Durchführung des Verfahrens
GB1404889A (en) * 1972-12-19 1975-09-03 Federal Mogul Corp Process for producing billets by compacting powder
DE2856082A1 (de) * 1977-12-28 1979-07-12 Leuven Res & Dev Vzw Verfahren zum herstellen von festen koerpern aus kupfer-zink-aluminium-legierungen

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US2210671A (en) * 1940-03-16 1940-08-06 Westinghouse Electric & Mfg Co Copper base alloy
US2430419A (en) * 1945-02-02 1947-11-04 Walter W Edens Welding rod
FR1068305A (fr) * 1952-12-13 1954-06-24 Pechiney Appareillage pour la fabrication de l'urée
US3117002A (en) * 1960-02-16 1964-01-07 Ampco Metal Inc Aluminum bronze alloy having improved wear resistance by the addition of cobalt, chromium, and manganese
US3091527A (en) * 1961-01-27 1963-05-28 Leeds & Northrup Co Copper base alloys particularly suited for precision resistance
US3333950A (en) * 1964-10-06 1967-08-01 Engelhard Ind Inc Metal composition for powder metallurgy moldings and method for production
US4113475A (en) * 1976-04-09 1978-09-12 Kennecott Copper Corporation Tarnish resistant copper alloy
US4158719A (en) * 1977-06-09 1979-06-19 Carpenter Technology Corporation Low expansion low resistivity composite powder metallurgy member and method of making the same
JPS54104301A (en) * 1978-02-02 1979-08-16 Nippon Dia Clevite Co Porous sound absorber of aluminum or aluminum alloy
US4310354A (en) * 1980-01-10 1982-01-12 Special Metals Corporation Process for producing a shape memory effect alloy having a desired transition temperature

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2006066B2 (de) * 1969-03-03 1975-01-16 Allmaenna Svenska Elektriska Ab, Vaesteraas (Schweden) Verfahren zum isostatischen Heißpressen von aus pulverförmigem Material vorgepreßten Körpern und Ofen zur Durchführung des Verfahrens
US3783037A (en) * 1969-11-12 1974-01-01 Fulmer Res Inst Ltd Treatment of alloys
DE2129125A1 (de) * 1970-06-11 1971-12-16 Olin Corp Verfahren zur Verarbeitung von Aluminiumbronzen
GB1404889A (en) * 1972-12-19 1975-09-03 Federal Mogul Corp Process for producing billets by compacting powder
DE2856082A1 (de) * 1977-12-28 1979-07-12 Leuven Res & Dev Vzw Verfahren zum herstellen von festen koerpern aus kupfer-zink-aluminium-legierungen

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0035070B1 (fr) * 1980-03-03 1985-05-15 BBC Aktiengesellschaft Brown, Boveri & Cie. Alliage-mémoire à base d'une solution solide riche en cuivre ou en nickel
EP0045985A1 (fr) * 1980-08-07 1982-02-17 BBC Aktiengesellschaft Brown, Boveri & Cie. Procédé de fabrication d'un alliage à mémoire à base de cuivre
EP0086012A3 (en) * 1982-02-05 1983-09-21 Bbc Aktiengesellschaft Brown, Boveri & Cie. Process for generating a reversible two-way memory effect in a component made from an alloy showing a one-way effect

Also Published As

Publication number Publication date
US4365996A (en) 1982-12-28
EP0035601B1 (fr) 1983-12-21
JPS56136942A (en) 1981-10-26
DE3065931D1 (en) 1984-01-26

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