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EP0110190A1 - Aluminium alloys for nuclear apparatus - Google Patents

Aluminium alloys for nuclear apparatus Download PDF

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Publication number
EP0110190A1
EP0110190A1 EP83111019A EP83111019A EP0110190A1 EP 0110190 A1 EP0110190 A1 EP 0110190A1 EP 83111019 A EP83111019 A EP 83111019A EP 83111019 A EP83111019 A EP 83111019A EP 0110190 A1 EP0110190 A1 EP 0110190A1
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EP
European Patent Office
Prior art keywords
aluminium alloys
alloys
weight
balance
nuclear
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Application number
EP83111019A
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German (de)
French (fr)
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EP0110190B1 (en
Inventor
Paolo Fiorini
Giuseppe Giordano
Giovanni Piatti
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.)
Aluminia SpA
Original Assignee
Alluminio Italia SpA
Aluminia SpA
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Priority to AT83111019T priority Critical patent/ATE25467T1/en
Publication of EP0110190A1 publication Critical patent/EP0110190A1/en
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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • C22C21/06Alloys based on aluminium with magnesium as the next major constituent

Definitions

  • This invention relates to aluminium alloys possessing time-stable mechanical, physical and chemical characteristics suitable for their use in nuclear apparatus, in particular in the first wall of nuclear fusion reactors.
  • the first wall of a nuclear fusion reactor is known to require the use of materials able to withstand very critical operating conditions for a long period of time (up to 10 years), they being subjected to temperatures up to 350-400°C (with a minimum of 120°C), to neutron irradiation and to corrosion in very pure water.
  • pure aluminium Because of its low activity following neutron irradiation, pure aluminium might appear to be a material suitable for this purpose. However, when in the pure state and especially when hot, this material has low mechanical properties and low corrosion resistance, insufficient for its use for the aforesaid application.
  • hyper-pure alloys containing conventional additives of low activity would leave the problem of hot corrosion resistance in very pure water unsolved.
  • the object of the present invention is therefore to provide aluminium alloys having the necessary initial mechanical, physical and chemical characteristics for their use in nuclear apparatus, in particular in the first wall of nuclear fusion reactors, said alloys being also able to maintain said initial characteristics substantially stable with time during their use.
  • Said alloys can be prepared by the known typical casting methods for Al alloys (fusion-produced alloys).
  • suitable known cycles comprising homogenisation, extrusion a nd/or rolling, and/or other plastic deformation processes which may be necessary, as known to experts of the art.
  • Said alloys according to the invention can also be prepared (in particular alloys containing Si) by the known powder technology method.
  • a dispersed phase of Al 2 O 3 and/or Al 2 O 3 .MgO type can also be present.
  • compositions for the alloys prepared by fusion according to the invention comprise 2.5-3% of Mg, 0.1-0.5% of V, possibly 0.05-0.2% of Si, and less than 150 p.p.m. of conventional impurities, the balance to 100% being Al (quantities expressed by weight).
  • Preferred compositions for alloys prepared by powder metallurgy according to the invention comprise 0.2-1% of Mg, 0.2-1% of Si, 0.5-2% of V, and less than 150 p.p.m. of conventional impurities, the balance to 100% being Al (quantities expressed by weight). Alloys prepared by fusion are particularly suitable for maximum operating temperatures of 150-200 C for the said wall, whereas powder -produced alloys are preferred for temperatures above 200°C and up to 350-400°C.
  • a billet is cast by the semi-continuous method from an Al-Mg-V alloy which on chemical analysis shows the following composition (quantities expressed as % by weight):
  • Said billet is homogenised for 15 hours at 400°C and 24 hours at 460°C, and is then extruded at 420°C to a diameter of 14 mm. From the extrusion obtained in this manner, samples of the required size are prepared by known methods for determining tensile, physical and creep behaviour characteristics (by ASTM procedures), these characteristics being shown hereinafter (the known symbols R,
  • Example 1 The procedure of Example 1 is followed, the only difference being that the alloy composition is as follows (quantities expressed in % by weight): Mg 2.68%; V 0.21%; Fe 12 p.p.m.; Si 11 p.p.m.; Cu 10 p.p.m.; Mn 5 p.p.m.; Ni 3 p.p.m.; Zn 2 p.p.m.; Ti less than 1 p.p.m.; Al balance to 100%.
  • the alloy composition is as follows (quantities expressed in % by weight): Mg 2.68%; V 0.21%; Fe 12 p.p.m.; Si 11 p.p.m.; Cu 10 p.p.m.; Mn 5 p.p.m.; Ni 3 p.p.m.; Zn 2 p.p.m.; Ti less than 1 p.p.m.; Al balance to 100%.
  • Powdered Al (purity 99.99%), Mg, Si and V were used (in the weight proportions of Mg 0.97%, V 1.1%, Si 0.71%, Al balance to 100%) to prepare by the known powder metallurgy method a Al-Mg-Si-V alloy in the form of a billet of size 80 mm diameter x 200 mm, using the following main basic parameters: sintering temperature 580°C; sintering time 24 hours; hot compacting at 580°C with a pressure of 550 N/mm 2 ; billet extrusion at 450°C to a diameter of 10 mm; solution heat-treatment for 2 hours at 520°C; rapid quenching followed by ageing at 150 0 C for 15 hours.
  • said extruded billet shows the following composition (% by weight): Mg 0.66%; V 1.07%; Si 0.65%; Fe 80 p.p.m.; Cu 12 p.p.m.; Mn 7 p.p.m.; Zn 3 p.p.m.; Ni 2 p.p.m.; Ti less than 1 p.p.m.; Al balance to 100%.
  • said alloys have good resistance to corrosion in a moist environment, both at room temperature and under hot conditions (100-150°C), and in addition have excellent weldability by all the typical methods for aluminium, and good workability for producing semi-finished products, even of complex form.
  • the alloys according to the invention are suitable for use in nuclear apparatus components, in particular in the first wall of nuclear fusion reactors, in accordance with the objects of the invention itself.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Manufacture And Refinement Of Metals (AREA)
  • Powder Metallurgy (AREA)

Abstract

Aluminium alloys having the following composition (% by weight):
  • - Mg 0.2-4.0%
  • - V 0.1-2.0%
  • - Si (in case) 0.05-1.0%
  • - other possible elements: total quantity less than 1000 p.p.m.
  • - Al balance to 100%.
The use of said alloys in nuclear apparatus, in particular in the first wall of nuclear fusion reactors.

Description

    Background of the Invention
  • This invention relates to aluminium alloys possessing time-stable mechanical, physical and chemical characteristics suitable for their use in nuclear apparatus, in particular in the first wall of nuclear fusion reactors.
  • The first wall of a nuclear fusion reactor is known to require the use of materials able to withstand very critical operating conditions for a long period of time (up to 10 years), they being subjected to temperatures up to 350-400°C (with a minimum of 120°C), to neutron irradiation and to corrosion in very pure water.
  • Because of its low activity following neutron irradiation, pure aluminium might appear to be a material suitable for this purpose. However, when in the pure state and especially when hot, this material has low mechanical properties and low corrosion resistance, insufficient for its use for the aforesaid application.
  • This deficiency of pure aluminium could be overcome by using its known commercial alloys containing additives such as Si, Zn, Cu, Mg, Fe, Ni, Cr, Mn and Zr.
  • However, most of said additives are unsuitable for the aforesaid application in that activation problems arise when under neutron irradiation.
  • The use of hyper-pure alloys containing conventional additives of low activity would leave the problem of hot corrosion resistance in very pure water unsolved.
  • Summary of the Invention
  • The object of the present invention is therefore to provide aluminium alloys having the necessary initial mechanical, physical and chemical characteristics for their use in nuclear apparatus, in particular in the first wall of nuclear fusion reactors, said alloys being also able to maintain said initial characteristics substantially stable with time during their use.
  • Said object is attained according to the present invention by aluminium alloys containing Mg in a quantity of between 0.2 and 4% by weight, V in a quantity of between 0.1 and 2.0% by weight, possibly Si in a quantity of between 0 and 1% by weight, and conventional impurities (such as Cu, Mn, Cr, Ti, Zn, Ni, B, Fe) in
  • a total quantity of less than 1000 p.p.m. by weight, the balance to 100% being represented by A1.
  • Said alloys can be prepared by the known typical casting methods for Al alloys (fusion-produced alloys).
  • In order to obtain the relative required semi-finished products, suitable known cycles are used comprising homogenisation, extrusion and/or rolling, and/or other plastic deformation processes which may be necessary, as known to experts of the art.
  • Said alloys according to the invention can also be prepared (in particular alloys containing Si) by the known powder technology method.
  • In this case, a dispersed phase of Al2O3 and/or Al2O3.MgO type can also be present.
  • Preferred Embodiments of the Invention
  • Preferred compositions for the alloys prepared by fusion according to the invention comprise 2.5-3% of Mg, 0.1-0.5% of V, possibly 0.05-0.2% of Si, and less than 150 p.p.m. of conventional impurities, the balance to 100% being Al (quantities expressed by weight). Preferred compositions for alloys prepared by powder metallurgy according to the invention comprise 0.2-1% of Mg, 0.2-1% of Si, 0.5-2% of V, and less than 150 p.p.m. of conventional impurities, the balance to 100% being Al (quantities expressed by weight). Alloys prepared by fusion are particularly suitable for maximum operating temperatures of 150-200 C for the said wall, whereas powder -produced alloys are preferred for temperatures above 200°C and up to 350-400°C.
  • The examples given hereinafter by way of non-limiting illustration describe the alloys according to the present invention in greater detail.
  • Example 1
  • A billet is cast by the semi-continuous method from an Al-Mg-V alloy which on chemical analysis shows the following composition (quantities expressed as % by weight):
    • Mg 2.69%; V 0.11%; Fe 100 p.p.m.; Si 11 p.p.m.; Cu 10 p.p.m.;
    • Mn 5 p.p.m.; Zn 2 p.p.m.; Ni 3 p.p.m.; Ti less than 1 p.p.m.;
    • A1 balance to 100%.
  • Said billet is homogenised for 15 hours at 400°C and 24 hours at 460°C, and is then extruded at 420°C to a diameter of 14 mm. From the extrusion obtained in this manner, samples of the required size are prepared by known methods for determining tensile, physical and creep behaviour characteristics (by ASTM procedures), these characteristics being shown hereinafter (the known symbols R,
  • Rp 0.2, A and σ being used to indicate respectively the ultimate tensile stress, 0.2% yield strength, ultimate elongation and breaking stress):
    • - Tensile characteristics:
      Figure imgb0001
    • - Physical characteristics
      • - Electrical resistivity at -196°C: 1.890 µΩcm
      • - Coefficient of linear expansion between 20 and 200°C: 26.2 MK-1
    • - Creep behaviour:
      Figure imgb0002
      Figure imgb0003
      Figure imgb0004
    Example 2
  • The procedure of Example 1 is followed, the only difference being that the alloy composition is as follows (quantities expressed in % by weight): Mg 2.68%; V 0.21%; Fe 12 p.p.m.; Si 11 p.p.m.; Cu 10 p.p.m.; Mn 5 p.p.m.; Ni 3 p.p.m.; Zn 2 p.p.m.; Ti less than 1 p.p.m.; Al balance to 100%.
  • The characteristics of said alloy are as follows:
    • - Tensile characteristics:
      Figure imgb0005
    • - Physical characteristics:
      • - Electrical resistivity at -196°C: 2.110 µΩ cm
      • - Coefficient of linear expansion between 20 and 200°C: 25.2 MK-1
    • - Creep behaviour:
      Figure imgb0006
    Example 3
  • Powdered Al (purity 99.99%), Mg, Si and V were used (in the weight proportions of Mg 0.97%, V 1.1%, Si 0.71%, Al balance to 100%) to prepare by the known powder metallurgy method a Al-Mg-Si-V alloy in the form of a billet of size 80 mm diameter x 200 mm, using the following main basic parameters: sintering temperature 580°C; sintering time 24 hours; hot compacting at 580°C with a pressure of 550 N/mm2; billet extrusion at 450°C to a diameter of 10 mm; solution heat-treatment for 2 hours at 520°C; rapid quenching followed by ageing at 1500C for 15 hours.
  • On chemical analysis, said extruded billet shows the following composition (% by weight): Mg 0.66%; V 1.07%; Si 0.65%; Fe 80 p.p.m.; Cu 12 p.p.m.; Mn 7 p.p.m.; Zn 3 p.p.m.; Ni 2 p.p.m.; Ti less than 1 p.p.m.; Al balance to 100%.
  • The characteristics of said alloy are as follows:
    • - Tensile characteristics:
      Figure imgb0007
    • - Physical characteristics:
      • - Density: 2.71 Mg M-3
      • - Electrical resistivity at -196°C: 1.530 µ Ω cm
  • The mechanical and physical characteristics of the three alloys described heretofore by way of example satisfy - as is apparent to an expert of the art - the requirements for their use in the primary wall of nuclear fusion reactors.
  • Moreover, said alloys have good resistance to corrosion in a moist environment, both at room temperature and under hot conditions (100-150°C), and in addition have excellent weldability by all the typical methods for aluminium, and good workability for producing semi-finished products, even of complex form.
  • From the aforegoing description and examples, the alloys according to the invention are suitable for use in nuclear apparatus components, in particular in the first wall of nuclear fusion reactors, in accordance with the objects of the invention itself.

Claims (7)

1. Aluminium alloys characterised by the following composition (component quantities expressed in % by weight):
- Mg from 0.2 to 4.0%
- V from 0.1 to 2.0%
- other possible'components: total quantity less than 1000 p.p.m.
- A1 balance to 100%
2. Aluminium alloys as claimed in claim 1, characterised by also containing Si in a quantity of between 0.05 and 1% by weight.
3. Aluminium alloys as claimed in claim 2, wherein the Si quantity is between 0.4 and 0.8% by weight.
4. Aluminium alloys as claimed in claim 1, wherein the component quantities (expressed in % by weight) are:
- Mg from 2.5 to 3.0%
- V from 0.1 to 0.5%
- other possible components: total quantity less than 150 p.p.m.
- Al balance to 100%
5. Aluminium alloys as claimed in claims 1 and 2, wherein the component quantities (expressed as % by weight) are:
- Mg from 0.2 to 1%
- V from 0.5 to 2%
- Si from 0.2 to 1%
- other possible components: total quantity less than 150 p.p.m.
- Al balance to 100%
6. Use of aluminium alloys as claimed in claims 1 to 5 in components of apparatus which are subjected to neutron irradiation during their operation.
7. Use of aluminium alloys as claimed in claims 1 to 5 in the first wall of nuclear fusion reactors.
EP83111019A 1982-11-26 1983-11-04 Aluminium alloys for nuclear apparatus Expired EP0110190B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AT83111019T ATE25467T1 (en) 1982-11-26 1983-11-04 ALUMINUM ALLOYS FOR NUCLEAR INSTALLATIONS.

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
IT24457/82A IT1154589B (en) 1982-11-26 1982-11-26 ALUMINUM ALLOYS FOR NUCLEAR EQUIPMENT
IT2445782 1982-11-26

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EP0110190A1 true EP0110190A1 (en) 1984-06-13
EP0110190B1 EP0110190B1 (en) 1987-02-11

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AT (1) ATE25467T1 (en)
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IT (1) IT1154589B (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2173214A (en) * 1985-04-02 1986-10-08 Aluminum Co Of America Powder metallurgy
EP0808911A1 (en) * 1996-05-22 1997-11-26 Alusuisse Technology & Management AG Component
EP0967294A1 (en) * 1998-06-26 1999-12-29 ALUMINIUM RHEINFELDEN GmbH Treatment of an aluminium melt

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1903842A (en) * 1932-05-20 1933-04-18 Court C Titus Aluminum alloy
FR808156A (en) * 1935-07-26 1937-01-30 Ig Farbenindustrie Ag Aluminum alloys and their applications
FR1034260A (en) * 1951-03-21 1953-07-21 Aluminum and vanadium based alloy
US3236632A (en) * 1964-12-01 1966-02-22 Dow Chemical Co High strength aluminum alloy for pellet extrusion and product
US4043840A (en) * 1976-07-09 1977-08-23 Swiss Aluminium Ltd. Aluminum alloys possessing improved resistance weldability

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1903842A (en) * 1932-05-20 1933-04-18 Court C Titus Aluminum alloy
FR808156A (en) * 1935-07-26 1937-01-30 Ig Farbenindustrie Ag Aluminum alloys and their applications
FR1034260A (en) * 1951-03-21 1953-07-21 Aluminum and vanadium based alloy
US3236632A (en) * 1964-12-01 1966-02-22 Dow Chemical Co High strength aluminum alloy for pellet extrusion and product
US4043840A (en) * 1976-07-09 1977-08-23 Swiss Aluminium Ltd. Aluminum alloys possessing improved resistance weldability

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2173214A (en) * 1985-04-02 1986-10-08 Aluminum Co Of America Powder metallurgy
EP0808911A1 (en) * 1996-05-22 1997-11-26 Alusuisse Technology & Management AG Component
EP0967294A1 (en) * 1998-06-26 1999-12-29 ALUMINIUM RHEINFELDEN GmbH Treatment of an aluminium melt
WO2000000654A1 (en) * 1998-06-26 2000-01-06 Aluminium Rheinfelden Gmbh Treatment of an aluminium alloy melt
US6994759B1 (en) 1998-06-26 2006-02-07 Aluminium Rheinfelden Gmbh Treatment of an aluminum alloy melt

Also Published As

Publication number Publication date
DE3369796D1 (en) 1987-03-19
EP0110190B1 (en) 1987-02-11
IT8224457A1 (en) 1984-05-26
IT8224457A0 (en) 1982-11-26
IT1154589B (en) 1987-01-21
ATE25467T1 (en) 1987-02-15

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