FR2691982A1 - Stainless steel composition for parts used in high vacuum and low temperature. - Google Patents

Stainless steel composition for parts used in high vacuum and low temperature. Download PDF

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Publication number
FR2691982A1
FR2691982A1 FR9206771A FR9206771A FR2691982A1 FR 2691982 A1 FR2691982 A1 FR 2691982A1 FR 9206771 A FR9206771 A FR 9206771A FR 9206771 A FR9206771 A FR 9206771A FR 2691982 A1 FR2691982 A1 FR 2691982A1
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weight
stainless steel
low temperature
steel composition
high vacuum
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FR9206771A
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FR2691982B1 (en
Inventor
Bourrat Jean
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Aubert and Duval SA
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Aubert and Duval SA
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Priority to FR9206771A priority Critical patent/FR2691982B1/en
Application filed by Aubert and Duval SA filed Critical Aubert and Duval SA
Priority to EP93401364A priority patent/EP0573335B1/en
Priority to DK93401364.0T priority patent/DK0573335T3/en
Priority to DE69308234T priority patent/DE69308234T2/en
Priority to AT93401364T priority patent/ATE149212T1/en
Priority to ES93401364T priority patent/ES2048128T3/en
Priority to DE93401364T priority patent/DE573335T1/en
Publication of FR2691982A1 publication Critical patent/FR2691982A1/en
Priority to GR940300003T priority patent/GR940300003T1/en
Application granted granted Critical
Publication of FR2691982B1 publication Critical patent/FR2691982B1/en
Priority to GR970400588T priority patent/GR3022903T3/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/58Ferrous alloys, e.g. steel alloys containing chromium with nickel with more than 1.5% by weight of manganese

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Treatment Of Steel In Its Molten State (AREA)
  • Soft Magnetic Materials (AREA)
  • Compositions Of Macromolecular Compounds (AREA)
  • Hard Magnetic Materials (AREA)
  • Manufacture And Refinement Of Metals (AREA)
  • Crucibles And Fluidized-Bed Furnaces (AREA)

Abstract

Stainless steel composition containing from 19 to 22 % by weight of chromium, from 8 to 11 % by weight of nickel, from 2.50 to 4.25 % by weight of manganese, from 2.00 to 3.00 % by weight of molybdenum, from 0.25 to 0.80 % by weight of niobium, from 0.35 to 0.50 % by weight of nitrogen, up to 0.08 % by weight of carbon, up to 0.75 % of silicon, up to 0.025 % by weight of phosphorus, up to 0.01 % by weight of sulphur, the remainder being iron and possible impurities, which has undergone refining in an AOD reactor and optionally remelting under slag. Such a composition makes it possible to produce articles which, after heat treatment and optional work-hardening, exhibit mechanical characteristics, sealing properties and an amagnetism enabling them to be employed in ultravacuum and at very low temperature.

Description

L'invention concerne une composition d'acier inoxydable pour piècesThe invention relates to a composition of stainless steel for parts

utilisées en ultravide et à basse température, ayant en particulier des propriétés  ultraviolet and low temperature, having in particular properties

mécaniques, une étanchéité et un amagnétisme accrus.  mechanical, increased water resistance and amagnetism.

La réalisation d'installations d'analyse des particules élémentaires notamment nécessite l'utilisation d'aciers inoxydables devant présenter les propriétés suivantes: étanchéité au travers des pièces du fait de la différence de pression qui existe entre l'enceinte sous vide (à plus de 10-1 torr, 1,33 10-é Pa> et la pression atmosphérique régnant à l'extérieur, étanchéité des joints de type couteau lors des assemblages sans soudure en présence de la même différence de pression, propriétés mécaniques tant en résistance à la traction qu'en ténacité jusqu'à des températures très basses allant jusau'à 1,8 K amagnétisme jusqu'à 1,8 K afin de ne pas perturber  The realization of elementary particle analysis facilities in particular requires the use of stainless steels having the following properties: sealing through the parts because of the pressure difference that exists between the vacuum chamber (more than 10-1 torr, 1.33 10 -Ep> and outside atmospheric pressure, sealing of knife-type joints during seamless joints in the presence of the same pressure difference, mechanical properties both in resistance to traction in toughness up to very low temperatures up to 1.8 K amagnetism up to 1.8 K so as not to disturb

le trajet des particules.the path of the particles.

En outre, il faut que l'acier inoxydable puisse supporter, sans altération des propriétés précédentes, le traitement de dégazage à 950 'C que certains utilisateurs doivent lui faire subir dans quelques  In addition, it is necessary that the stainless steel can withstand, without altering the above properties, the degassing treatment at 950 'C that some users must make him undergo in a few

applications.applications.

Jusqu'à présent la solution la plus courante consistait à utiliser la nuance E-Z 2 CND 17 13 + Az ayant la composition nominale suivante en poids Carbone 0,03 Chrome 17,00 Nickel 14,00 Molybdène 2,80 Azote 0,15 Fer Complément  Until now, the most common solution was to use the grade E-Z 2 CND 17 13 + Az having the following nominal composition by weight Carbon 0.03 Chromium 17.00 Nickel 14.00 Molybdenum 2.80 Nitrogen 0.15 Iron Complement

et possédant des propriétés types qui seront données ci-  and having typical properties which will be given below

après. Or il a maintenant été trouvé que l'on obtient des propriétés encore améliorées en utilisant une composition d'acier inoxydable à haute teneur en azote  after. However, it has now been found that even improved properties are obtained by using a stainless steel composition with a high nitrogen content.

et contenant du niobium et du manganèse.  and containing niobium and manganese.

Selon l'invention, on utilise un acier inoxydable ayant une composition comprise dans les limites suivantes % en poids Carbone jusqu'à 0,08 Chrome 19 22 Nickel 8 11 Manganèse 2,50 4,25 Molybdène 2,00 3,00 Silicium jusqu'à 0,75 Phosphore jusqu'à 0,025 Soufre jusqu'à 0,01 Niobium 0,25 0,80  According to the invention, a stainless steel having a composition within the following limits is used.% By weight Carbon up to 0.08 Chromium 19 22 Nickel 8 11 Manganese 2.50 4.25 Molybdenum 2.00 3.00 Silicon up to to 0.75 Phosphorus up to 0.025 Sulfur up to 0.01 Niobium 0.25 0.80

Azote 0,35 0,50.Nitrogen 0.35 0.50.

Fer Complément La teneur en azote confère & l'acier deux propriétés essentielles: une phase austénitique stable & basse température, ce qui permet de conserver l'amagnétisme en condition cryogénique. des caractéristiques mécaniques élevées dans un large domaine de température y compris dans le domaine  Iron Complement The nitrogen content gives steel two essential properties: a stable austenitic phase & low temperature, which makes it possible to preserve non magnetism in cryogenic condition. high mechanical characteristics in a wide temperature range including in the field

cryogénique.cryogenic.

L'addition de manganèse est nécessaire pour assurer  The addition of manganese is necessary to ensure

la solubilité d'une telle teneur en azote.  the solubility of such a nitrogen content.

L'addition de nobium sert à stabiliser le carbone et par suite renforce la tenue à la corrosion Cette addition améliore la tenue à chaud de la nuance et renforce, indirectement, par affinage du grain la limite  The addition of nobium serves to stabilize the carbon and consequently reinforces the corrosion resistance. This addition improves the heat resistance of the grade and reinforces, indirectly, by refining the grain the limit.

élastique à basse température.elastic at low temperature.

Les aciers selon la présente invention sont obtenus de manière classique par élaboration au four à arc et subissent ensuite un affinage par le procédé AOD (encore appelé "affinage en réacteur AOD") ("argon oxygen decarburization", décarburation à l'argon-oxygène) qui permet d'obtenir sans difficultés la faible teneur en  The steels according to the present invention are conventionally obtained by elaboration in an arc furnace and then undergo refining by the AOD process (also called "AOD reactor refining") ("argon oxygen decarburization", argon-oxygen decarburization). ) which makes it possible to obtain without difficulty the low content of

carbone recherchée.sought carbon.

Afin de diminuer la teneur en inclusions, on peut soumettre l'acier obtenu à une refusion sous laitier, en particulier lorsqu'on désire réaliser avec la composition des parois minces et des Joints de type couteau En effet la faible teneur inclusionnaire garantit une étanchéité supérieure Ce traitement n'est  In order to reduce the content of inclusions, the steel obtained can be subjected to slag remelting, in particular when it is desired to produce with the composition thin walls and knife-type seals. Indeed, the low inclusion content guarantees superior sealing. This treatment is

toutefois pas obligatoire.however not required.

Les pièces préparées à partir d'une composition selon la présente invention subissent un traitement thermique à une température de 10001100 'C avec refroidissement sous air, huile ou eau selon la dimension des pièces,  The parts prepared from a composition according to the present invention undergo a heat treatment at a temperature of 1000 ° C. under cooling in air, oil or water depending on the size of the pieces,

pour donner un état hypertrempé.to give a hyper-tempered state.

On peut également pratiquer après 1 'hypertrempe un écrouissage à la température ambiante par laminage,  It is also possible, after the quenching, to temper at room temperature by rolling.

étirage ou tréfilage.drawing or drawing.

Le tableau 1 ci-dessous regroupe un certain nombre de mesures de résistance mécanique effectuées par trois laboratoires sur des barres d'acier selon la présente invention. La composition spécifique de l'acier utilisé pour la réalisation des barres d'essai est la suivante Barre O 31,75 0 12 O 12 0 45 hypertrempé hypertrempé écroui hypertrempé Carbone 0,033 O 035 0,02 ? 0,035 Chrome 20,89 20,69 20,10 20,69 Nickel 9,22 9,73 9,09 9,73 Manganèse 4,14 3,92 4,00 3,92 Molybdène 2,10 2,14 2, 10 2,14 Silicium 0,36 0,42 0,37 0,42 Phosphore 0,022 0,021 0,021 0,021 Soufre < 0,002 < 0,002 < 0,002 < 0,002 Niobium 0,32 0,30 0,30 0,30 Azote 0,42 0,427 0,419 0,427 On note dans les compositions des traces d'impuretés  Table 1 below groups together a number of strength measurements made by three laboratories on steel bars according to the present invention. The specific composition of the steel used for the production of the test bars is as follows: Bar O 31.75 0 12 O 12 0 45 hyper-hardened hyper-tempered hardened high-tempered carbon 0.033 O 035 0.02? 0.035 Chromium 20.89 20.69 20.10 20.69 Nickel 9.22 9.73 9.09 9.73 Manganese 4.14 3.92 4.00 3.92 Molybdenum 2.10 2.14 2, 10 2.14 Silicon 0.36 0.42 0.37 0.42 Phosphorus 0.022 0.021 0.021 0.021 Sulfur <0.002 <0.002 <0.002 <0.002 Niobium 0.32 0.30 0.30 0.30 Nitrogen 0.42 0.427 0.419 0.427 We note in the compositions traces of impurities

telles que de l'aluminium, du cuivre et du cobalt.  such as aluminum, copper and cobalt.

TABLEAU 1TABLE 1

barre I. Etat Thermique j hypertrempé _ No du  bar I. Thermal state i super-tempered _

Labora-labora-

toire TempératureTemperature area

300 K 1 71 K (*) | 2 &K 1 1,8 K K300 K 1 71 K (*) | 2 & K 1 1.8 K K

Rm M Pa Rp 0,2 % M Pa 41,6 E G Pa l Rm M Pa I Rp 0,2 % M Pa  Rm M Pa Rp 0.2% M Pa 41.6 E G Pa l Rm M Pa I Rp 0.2% M Pa

1663 11141663 1114

E G Pa Rm M Pa Rp 0,2 % M Pa E G Pa F. Rm M Pa I  E G Pa Rm M Pa Rp 0.2% M Pa E G Pa F. Rm M Pa I

Rp 0,2 %.Rp 0.2%.

M Pa 31,75 hypertrempé 3 942 605 45 210,3 1768 1325 42 187,2 2048 1700 26 204,3 187,2  M Pa 31.75 hyper-tempered 3 942 605 45 210.3 1768 1325 42 187.2 2048 1700 26 204.3 187.2

1828 1345 32 2057 1700 22 217,61828 1345 32 2057 1700 22 217.6

12 hypertrempé 2 1007 587 39,6 1954 1374 19,4 2426 2300 1,5  12 hyper-tempered 2 1007 587 39.6 1954 1374 19.4 2426 2300 1.5

2 1007 595 39,6 1984 1404 18,3 _ _2 1007 595 39.6 1984 1404 18.3 _ _

1 1125 887 211 1125 887 21

12 écroui 2 1060 990 24 1981 1804 18,4  12 hardened 2 1060 990 24 1981 1804 18.4

2 1079 1008 '26,4 1981 1804 16,62 1079 1008 '26, 4 1981 1804 16.6

12,5 t écroui I12.5 t hardened I

1088 8631088 863

26 189 | 1942 1597 l 20,5 | 198,7 13,3 ,5 I I  26 189 | 1942 1597 l 20.5 | 198.7 13.3, 5 I I

(O 3 H(O 3 H

valeur hypertrempé moyenne 650 320 50 1350 700 40 1480 790 28 R typique lm C\ Rm =nrésistance Rp = limite élastique Ao = allongement E = module d'élasticité (*) pour Labo 2 la température d'essai est non contrôlée et vraisemblablement proche de 95/100 K u C KJ (OD (. al (.0 r-i 0) U) -P. p-, - - - - L Les résultats obtenus montrent clairement qu'il est possible d'obtenir avec les aciers en question, tant à l'état hypertrempé qu'écroui, des caractéristiques mécaniques Rm et Rp 0,2 % élevées, tout en conservant une ductilité suffisante A cet égard, on notera que pour des applications à des températures inférieures ou égales à 20 K, il n'est pas conseillé de partir d'un acier préalablement écroui, car les résultats ci-dessus montrent que le gain sur la limite élastique et la charge de rupture est faible alors que la ductilité est  average hyper-tempered value 650 320 50 1350 700 40 1480 790 28 R typical lm C \ Rm = nresistance Rp = yield strength Ao = elongation E = modulus of elasticity (*) for Labo 2 the test temperature is uncontrolled and presumably close The results obtained clearly show that it is possible to obtain, with the steels in question, from 95/100 K K (OD (.alpha..sub.0) .sub.p). both in the quenched and quenched state, mechanical characteristics Rm and Rp 0.2% high, while maintaining a sufficient ductility In this respect, it will be noted that for applications at temperatures of less than or equal to 20 K, It is not advisable to start from a previously hardened steel, because the results above show that the gain on the elastic limit and the breaking load is low, whereas the ductility is

sensiblement dégradée.significantly degraded.

Le taux d'écrouissage que l'on applique éventuellement est fonction des caractéristiques mécaniques que l'on souhaite obtenir et la figure unique montre l'évolution des caractéristiques mécaniques Rm et  The rate of hardening that one applies possibly depends on the mechanical characteristics that one wishes to obtain and the single figure shows the evolution of the mechanical characteristics Rm and

Rp 0,2 % en fonction du taux d'écrouissage.  Rp 0.2% depending on the rate of work hardening.

Le tableau 2 ci-dessous donne des résultats concernant la susceptibilité magnétique d'un acier  Table 2 below gives results concerning the magnetic susceptibility of a steel

inoxydable selon la présente invention.  stainless according to the present invention.

TABLEAU 2TABLE 2

H 0,005 oe 1000 oe Susceptibilité magnétique à 1,8 K 5 10-a 5 10-3 La matériau est donc classé comme amagnétique à la température de 1,8 K. On voit donc que les compositions d'acier inoxydable selon la présente invention donnent des pièces ayant des caractéristiques mécaniques et des propriétés amagnétiques qui les rendent particulièrement30 appropriées pour la réalisation d'installations en ultravide et/ou à très basse température; elles trouvent une application particulière dans les installations d'analyse des particules Elémentaires et la réalisation  H 0.005 oe 1000 oe Magnetic susceptibility to 1.8 K 5 10-a 5 10-3 The material is therefore classified as non-magnetic at the temperature of 1.8 K. It is thus seen that the stainless steel compositions according to the present invention give parts having mechanical characteristics and non-magnetic properties which make them particularly suitable for the realization of ultrahigh and / or very low temperature installations; they find a particular application in the systems of analysis of the elementary particles and the realization

de moteurs cryogéniques.cryogenic engines.

Claims (3)

REVENDICATIONS 1. Composition d'acier inoxydable contenant de 19 à 22 % en poids de chrome, de 8 à 11 % en poids de nickel, de 2,50 à 4,25 % en poids de manganèse, de 2,00 à 3,00 % en poids de molybdène, de 0,25 à 0,80 % en poids de niobium, de 0,35 & 0,50 % en poids d'azote, Jusqu'à 0,08 % en poids de carbone, jusqu'à 0,75 % de silicium, Jusqu'à 0,025 % en poids de phosphore, jusqu'à 0,01 % en poids de soufre, le complément étant du fer et d'éventuelles impuretés, ayant subi un affinage en réacteur AOD et  1. Stainless steel composition containing from 19 to 22% by weight of chromium, from 8 to 11% by weight of nickel, from 2.50 to 4.25% by weight of manganese, from 2.00 to 3.00 % by weight of molybdenum, from 0.25 to 0.80% by weight of niobium, from 0.35% to 0.50% by weight of nitrogen, up to 0.08% by weight of carbon, up to 0.75% of silicon, up to 0.025% by weight of phosphorus, up to 0.01% by weight of sulfur, the balance being iron and any impurities, having undergone refining in AOD reactor and éventuellement une refusion sous laitier.  possibly a slag remelting. 2. Pièces destinées à la réalisation de dispositifs fonctionnant en ultravide et à basse température, obtenues à partir de la composition d'acier inoxydable selon la revendication 1, avec un traitement thermique &  2. Parts intended for the production of devices operating in ultra-high vacuum and at low temperature, obtained from the stainless steel composition according to claim 1, with a heat treatment & 1000-1100 'C.1000-1100 ° C. 3. Pièces selon la revendication 2, ayant subi un  3. Parts according to claim 2, having undergone écrouissage à la température ambiante.  hardening at room temperature.
FR9206771A 1992-06-04 1992-06-04 Stainless steel composition for parts used in ultrahigh vacuum and low temperature. Expired - Fee Related FR2691982B1 (en)

Priority Applications (9)

Application Number Priority Date Filing Date Title
FR9206771A FR2691982B1 (en) 1992-06-04 1992-06-04 Stainless steel composition for parts used in ultrahigh vacuum and low temperature.
DK93401364.0T DK0573335T3 (en) 1992-06-04 1993-05-28 Stainless steel alloy for parts used under ultra-vacuum and at low temperatures
DE69308234T DE69308234T2 (en) 1992-06-04 1993-05-28 Stainless steel composition for components, usable in high vacuum and at low temperature
AT93401364T ATE149212T1 (en) 1992-06-04 1993-05-28 STAINLESS STEEL COMPOSITION FOR COMPONENTS USABLE IN HIGH VACUUM AND LOW TEMPERATURE
EP93401364A EP0573335B1 (en) 1992-06-04 1993-05-28 Stainless steel composition for construction parts, used in high vacuum and at low temperature
ES93401364T ES2048128T3 (en) 1992-06-04 1993-05-28 STAINLESS STEEL COMPOSITION FOR PARTS USED IN ULTRAVACIO AND LOW TEMPERATURE.
DE93401364T DE573335T1 (en) 1992-06-04 1993-05-28 Stainless steel composition for components, usable in high vacuum and at low temperature.
GR940300003T GR940300003T1 (en) 1992-06-04 1994-02-28 Stainless steel composition for construction parts, used in high vacuum and at low temperature
GR970400588T GR3022903T3 (en) 1992-06-04 1997-03-26 Stainless steel composition for construction parts, used in high vacuum and at low temperature

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9206771A FR2691982B1 (en) 1992-06-04 1992-06-04 Stainless steel composition for parts used in ultrahigh vacuum and low temperature.

Publications (2)

Publication Number Publication Date
FR2691982A1 true FR2691982A1 (en) 1993-12-10
FR2691982B1 FR2691982B1 (en) 1994-08-26

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FR9206771A Expired - Fee Related FR2691982B1 (en) 1992-06-04 1992-06-04 Stainless steel composition for parts used in ultrahigh vacuum and low temperature.

Country Status (7)

Country Link
EP (1) EP0573335B1 (en)
AT (1) ATE149212T1 (en)
DE (2) DE69308234T2 (en)
DK (1) DK0573335T3 (en)
ES (1) ES2048128T3 (en)
FR (1) FR2691982B1 (en)
GR (2) GR940300003T1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1055011A1 (en) * 1997-12-23 2000-11-29 Allegheny Ludlum Corporation Austenitic stainless steel including columbium
BR112013030258B1 (en) 2011-05-26 2019-10-08 Upl, L.L.C. D/B/A United Pipelines Of America Llc AUSTENIC STAINLESS STEEL, METAL BASED, FORGED STEEL AND CAST STEEL UNDERSTANDING THE SAME AND PREPARATION METHOD OF SUCH STAINLESS STEEL

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1205289B (en) * 1964-05-27 1965-11-18 Phoenix Rheinrohr Ag Use of an austenitic steel alloy as a material for welded components that are exposed to attack by sea water and / or the sea atmosphere
FR2228119A1 (en) * 1973-05-04 1974-11-29 Nippon Steel Corp
SU521350A1 (en) * 1974-07-16 1976-07-15 Физико-Механический Институт Ордена Ленина Ан Украинской Сср Corrosion Resistant Steel
FR2372902A1 (en) * 1976-12-02 1978-06-30 Allegheny Ludlum Ind Inc HOT DUCTILE AUSTENITIC STAINLESS STEEL

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1205289B (en) * 1964-05-27 1965-11-18 Phoenix Rheinrohr Ag Use of an austenitic steel alloy as a material for welded components that are exposed to attack by sea water and / or the sea atmosphere
FR2228119A1 (en) * 1973-05-04 1974-11-29 Nippon Steel Corp
SU521350A1 (en) * 1974-07-16 1976-07-15 Физико-Механический Институт Ордена Ленина Ан Украинской Сср Corrosion Resistant Steel
FR2372902A1 (en) * 1976-12-02 1978-06-30 Allegheny Ludlum Ind Inc HOT DUCTILE AUSTENITIC STAINLESS STEEL

Also Published As

Publication number Publication date
GR940300003T1 (en) 1994-02-28
DE69308234D1 (en) 1997-04-03
FR2691982B1 (en) 1994-08-26
DE573335T1 (en) 1994-04-21
GR3022903T3 (en) 1997-06-30
ATE149212T1 (en) 1997-03-15
DK0573335T3 (en) 1997-03-17
EP0573335B1 (en) 1997-02-26
DE69308234T2 (en) 1997-06-12
ES2048128T1 (en) 1994-03-16
ES2048128T3 (en) 1997-05-01
EP0573335A1 (en) 1993-12-08

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