EP0589807B1 - Use of an aluminium alloy for making bottles for compressed gas - Google Patents
Use of an aluminium alloy for making bottles for compressed gas Download PDFInfo
- Publication number
- EP0589807B1 EP0589807B1 EP93420377A EP93420377A EP0589807B1 EP 0589807 B1 EP0589807 B1 EP 0589807B1 EP 93420377 A EP93420377 A EP 93420377A EP 93420377 A EP93420377 A EP 93420377A EP 0589807 B1 EP0589807 B1 EP 0589807B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- alloy
- stage
- compressed gas
- content
- bottles
- 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
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
- C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
- C22F1/053—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon of alloys with zinc as the next major constituent
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/10—Alloys based on aluminium with zinc as the next major constituent
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C1/00—Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge
- F17C1/14—Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge constructed of aluminium; constructed of non-magnetic steel
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2201/00—Vessel construction, in particular geometry, arrangement or size
- F17C2201/05—Size
- F17C2201/058—Size portable (<30 l)
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
- F17C2203/0634—Materials for walls or layers thereof
- F17C2203/0636—Metals
- F17C2203/0646—Aluminium
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
- F17C2203/0634—Materials for walls or layers thereof
- F17C2203/0636—Metals
- F17C2203/0648—Alloys or compositions of metals
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2209/00—Vessel construction, in particular methods of manufacturing
- F17C2209/23—Manufacturing of particular parts or at special locations
- F17C2209/232—Manufacturing of particular parts or at special locations of walls
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2260/00—Purposes of gas storage and gas handling
- F17C2260/01—Improving mechanical properties or manufacturing
- F17C2260/011—Improving strength
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2260/00—Purposes of gas storage and gas handling
- F17C2260/05—Improving chemical properties
- F17C2260/053—Reducing corrosion
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2270/00—Applications
- F17C2270/07—Applications for household use
- F17C2270/0745—Gas bottles
Definitions
- the invention relates to an AI alloy which can be used for the manufacture of bottles. of metal for compressed gases.
- the modification of the chemical composition on the one hand and the final heat treatment on the other improve the burst characteristics (facies of the tear) while maintaining the level of mechanical characteristics and resistance to corrosion under stress required.
- the alloys used according to the invention have the following weight composition (in%): 6.25 ⁇ Zn ⁇ 8.0 1.2 ⁇ Mg ⁇ 2.2 1.7 ⁇ Cu ⁇ 2.8 0.10 ⁇ Zr ⁇ 0.25 Cr ⁇ 0.05 Fe ⁇ 0.20 Fe + Si ⁇ 0.40 Mn ⁇ 0.20 Ti ⁇ 0.05 Others each ⁇ 0.05 total ⁇ 0.15 Rest: Al
- the Mg content is preferably kept below 2%, and even 1.95%, and the Zr content is preferably between 0.10 and 0.18%, the contents in Fe + Si being ⁇ 0.25% with Fe ⁇ 0.12%, an Mn content ⁇ 0.10% and / or the Zn content ⁇ 6.75.
- the manufacturing and control process are similar to those described in EP-A-0257167, but preferably the treatment of final income type T73 is replaced by an income in 3 stages, the 1st stage being carried out between 105 and 120 °. C for 6 to 12 h, the 2nd step being carried out between 170 and 190 ° C for 0.5 to 20 h and the 3rd step being carried out between 105 and 120 ° C, for 12 to 36 h.
- These steps can be carried out continuously or discontinuously (return to ambient temperature between each of them or some of them).
- the durations and temperatures actually used are chosen by a person skilled in the art so as to obtain both a high electrical conductivity (corresponding to good resistance to corrosion under tension) and a high elastic limit.
- Example 1 Replacement of Cr by Zr for two-phase income type T73.
- the following example shows the gain that can be obtained by performing a returned in three stages to the bottles manufactured in alloy 2 according to the range of the previous example.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Organic Chemistry (AREA)
- Metallurgy (AREA)
- Materials Engineering (AREA)
- Crystallography & Structural Chemistry (AREA)
- Thermal Sciences (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Heat Treatment Of Steel (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
- Shaping Metal By Deep-Drawing, Or The Like (AREA)
- Superconductors And Manufacturing Methods Therefor (AREA)
- Catalysts (AREA)
- Air Bags (AREA)
- Pressure Vessels And Lids Thereof (AREA)
- Metal Extraction Processes (AREA)
- Press Drives And Press Lines (AREA)
- Forging (AREA)
- Materials For Medical Uses (AREA)
Abstract
Description
L'invention concerne un alliage d'AI utilisable pour la fabrication de bouteilles métalliques pour gaz comprimés.The invention relates to an AI alloy which can be used for the manufacture of bottles. of metal for compressed gases.
Dans sa demande EP-A-0257167, la demanderesse a revendiqué un alliage type 7000 particulièrement adapté à l'emploi considéré ci-dessus.In its application EP-A-0257167, the applicant claimed an alloy type 7000 particularly suitable for the use considered above.
Cependant, celle-ci s'est aperçue que dans certains cas, la modification de la composition chimique d'une part et du traitement thermique final d'autre part permettent d'améliorer les caractéristiques d'éclatement (faciès de la déchirure) en conservant le niveau de caractéristiques mécaniques et de résistance à la corrosion sous contrainte requises.However, the latter noted that in certain cases, the modification of the chemical composition on the one hand and the final heat treatment on the other improve the burst characteristics (facies of the tear) while maintaining the level of mechanical characteristics and resistance to corrosion under stress required.
Par ailleurs, l'article de P.K. BALASUBRAMANIAN "Extrusion of Al Zn Mg Cu Zr Alloys" Materials Science and Technology, vol.1, n° 6, 1985, pages 470-474, décrit l'extrusion de tubes en divers alliages Al Zn Mg Cu Zr qui peuvent résister à des essais de pression jusqu'à 550 MPa.Furthermore, the article by P.K. BALASUBRAMANIAN "Extrusion of Al Zn Mg Cu Zr Alloys "Materials Science and Technology, vol.1, n ° 6, 1985, pages 470-474, describes the extrusion of tubes of various Al Zn Mg Cu Zr alloys that can resist pressure tests up to 550 MPa.
Les alliages utilisés selon l'invention possèdent la composition pondérale suivante
(en %) :
6,25 ≤ Zn ≤ 8,0
1,2 ≤ Mg ≤ 2,2
1,7 ≤ Cu ≤ 2,8
0,10 ≤ Zr ≤ 0,25
Cr ≤ 0,05
Fe ≤ 0,20
Fe+Si ≤ 0,40
Mn ≤ 0,20
Ti ≤ 0,05
Autres chacun ≤ 0,05
total ≤ 0,15
Reste : AlThe alloys used according to the invention have the following weight composition (in%):
6.25 ≤ Zn ≤ 8.0
1.2 ≤ Mg ≤ 2.2
1.7 ≤ Cu ≤ 2.8
0.10 ≤ Zr ≤ 0.25
Cr ≤ 0.05
Fe ≤ 0.20
Fe + Si ≤ 0.40
Mn ≤ 0.20
Ti ≤ 0.05
Others each ≤ 0.05
total ≤ 0.15
Rest: Al
La teneur en Mg est tenue de préférence en-dessous de 2%, et même 1,95%, et la teneur en Zr est de préférence comprise entre 0,10 et 0,18 %, les teneurs en Fe+ Si étant ≤ 0,25 % avec Fe ≤ 0,12 %, une teneur en Mn ≤ 0,10 % et/ou la teneur en Zn ≥ 6,75. The Mg content is preferably kept below 2%, and even 1.95%, and the Zr content is preferably between 0.10 and 0.18%, the contents in Fe + Si being ≤ 0.25% with Fe ≤ 0.12%, an Mn content ≤ 0.10% and / or the Zn content ≥ 6.75.
Si la teneur en Zr est supérieure à 0,25%, on constate la présence de gros précipités qui induisent de graves difficultés lors de la coulée et la structure est non recristallisée. Pour les teneurs en Zr ≤ 0,10%, la structure est recristallisée, mais à gros grains.If the Zr content is greater than 0.25%, we observe the presence of large precipitates which cause serious difficulties during casting and structure is not recrystallized. For Zr contents ≤ 0.10%, the structure is recrystallized, but with large grains.
Le procédé de fabrication et de contrôle sont semblables à ceux décrits
dans EP-A-0257167, mais, de préférence, le traitement de revenu final type
T73 est remplacé par un revenu en 3 étapes, la 1ère étape étant effectuée
entre 105 et 120°C pendant 6 à 12 h, la 2ème étape étant effectuée entre
170 et 190°C pendant 0,5 à 20 h et la 3ème étape étant effectuée entre 105
et 120°C, pendant 12 à 36 h.
Ces étapes peuvent être effectuées de manière continue ou discontinue
(retour à la température ambiante entre chacune d'elles ou certaines
d'entre elles).
Les durées et températures effectivement utilisées sont choisies par
l'homme de métier de manière à obtenir à la fois une conductibilité
électrique élevée (correspondant à une bonne résistance à la corrosion
sous tension) et une limite élastique élevée.
L'amélioration des caractéristiques de fissuration est probablement due,
mais c'est là une hypothèse, au fait que la structure est mieux
recristallisée (le Zr étant un élément anti-recristallisant moins puissant
que le Cr), la perte relative de résistance à la corrosion sous tension
étant compensée par le revenu final triple.The manufacturing and control process are similar to those described in EP-A-0257167, but preferably the treatment of final income type T73 is replaced by an income in 3 stages, the 1st stage being carried out between 105 and 120 °. C for 6 to 12 h, the 2nd step being carried out between 170 and 190 ° C for 0.5 to 20 h and the 3rd step being carried out between 105 and 120 ° C, for 12 to 36 h.
These steps can be carried out continuously or discontinuously (return to ambient temperature between each of them or some of them).
The durations and temperatures actually used are chosen by a person skilled in the art so as to obtain both a high electrical conductivity (corresponding to good resistance to corrosion under tension) and a high elastic limit.
The improvement in the cracking characteristics is probably due, but this is an assumption, to the fact that the structure is better recrystallized (Zr being an anti-recrystallizing element less powerful than Cr), the relative loss of resistance to corrosion under tension being compensated by the triple final income.
L'invention sera mieux comprise à l'aide des exemples suivants :The invention will be better understood using the following examples:
Deux alliages, l'un conforme à la demande EP-A-0257167- alliage 1, l'autre
semblable mis à part le fait qu'on a remplacé le chrome par le
zirconium -alliage 2- ont été élaborés et transformés en bouteilles de 6
litres suivant la gamme de fabrication ci-après :
Coulée de billettes de diamètre 165 mm
Sciage en lopins
Réchauffage des lopins
Filage inverse à chaud d'étuis
Etirage à chaud
Etirage à froid
Usinage du fond
Mise à longueur
Ogivage à chaud
Perçage du goulot et usinage
Décapage
Mise en solution
Trempe
Revenu 6h à 105°C + 15h à 170°C.Two alloys, one in accordance with the request EP-A-0257167- alloy 1, the other similar apart from the fact that chromium has been replaced by zirconium -alloy 2- have been prepared and transformed into bottles of 6 liters according to the following production range:
165 mm diameter billet casting
Sawing into plots
Reheating plots
Hot reverse spinning of cases
Hot drawing
Cold drawing
Bottom machining
Cut to length
Hot icing
Bottom drilling and machining
Pickling
Dissolution
Quenching
Income 6 hours at 105 ° C + 3 hours at 170 ° C.
La composition pondérale (en %) de ces 2 alliages est donnée dans le
tableau suivant :
Les caractéristiques obtenues sur les bouteilles correspondantes sont les
suivantes :
Dans des conditions pour lesquelles les caractéristiques de l'éclatement sont correctes (fissure longitudinale dans sa plus grande partie, non ramifiée, limitée à un secteur d'angle ± 90° autour de la fissure principale, limitée vers le fond et vers le goulot à des zones dont l'épaisseur est inférieure à 1,5 fois l'épaisseur du corps), la longueur développée de la fissure a été remarquée comme un bon indice de l'aptitude à l'éclatement : plus la fissure est longue, plus on se rapproche des conditions pour lesquelles l'éclatement serait mauvais.In conditions for which the burst characteristics are correct (longitudinal crack for the most part, not branched, limited to a sector of angle ± 90 ° around the crack main, limited towards the bottom and towards the neck to areas of which the thickness is less than 1.5 times the thickness of the body), the length developed from the crack was noted as a good indication of suitability bursting: the longer the crack, the closer we get to conditions for which the burst would be bad.
Les résultats présentés ci-dessus montrent que le remplacement du chrome par du zirconium permet d'améliorer très sensiblement la qualité de l'éclatement, mais au détriment de la résistance à la corrosion sous contrainte et, faiblement, de la résistance mécanique. Toutefois, les deux séries de bouteilles sont adaptées à l'emploi.The results presented above show that the replacement of chromium with zirconium makes it possible to very significantly improve the quality of bursting, but at the expense of corrosion resistance under stress and, weakly, mechanical strength. However, both series of bottles are suitable for use.
Pour un type de revenu donné, en l'occurrence un revenu bipalier, la résistance mécanique et la résistance à la corrosion sous contrainte sont liées de façon biunivoque, ce qui fait qu'il vaut mieux parler d'une perte sur le compromis résistance mécanique/résistance à la corrosion sous contrainte. Autrement dit, le remplacement du chrome par le zirconium affecte négativement la résistance à la corrosion ou la résistance mécanique, selon la durée du maintien au deuxième palier que l'on choisit.For a given type of income, in this case two-tier income, the mechanical strength and resistance to stress corrosion are unequivocally linked, which makes it better to speak of a loss on the compromise between mechanical strength and corrosion resistance under constraint. In other words, the replacement of chromium by zirconium negatively affects corrosion resistance or resistance mechanical, depending on how long you maintain the second level you choose.
L'exemple suivant montre le gain que l'on peut obtenir en effectuant un revenu en trois étapes sur les bouteilles fabriquées dans l'alliage 2 selon la gamme de l'exemple précédent.The following example shows the gain that can be obtained by performing a returned in three stages to the bottles manufactured in alloy 2 according to the range of the previous example.
La conductivité électrique est prise comme indicateur de la résistance à
la corrosion sous contrainte, conformément à une pratique courante. Toutes
les valeurs du tableau ci-dessous sont des moyennes de 3 valeurs
individuelles.
A l'aide de ce tableau, on peut établir les points suivants :
- le revenu à 3 étapes permet d'améliorer le compromis résistance à la corrosion sous contrainte/résistance mécanique. Entre le revenu A et le revenu C, la conductivité augmente de manière importante, avec un léger gain de résistance mécanique. L'augmentation de conductivité se traduit bien par une augmentation de la résistance à la corrosion sous contrainte puisqu'on n'a pas de rupture à 60 j sous 280 MPa.
- le revenu tri-paliers avec un deuxième palier à 190°C conduit à un compromis résistance à la corrosion sous contrainte/résistance mécanique à peine meilleur que celui obtenu avec un revenu bipalier. Le domaine de température intéressant pour le deuxième palier est donc limité vers le haut à 190°C.
- grâce au revenu tri-paliers, le compromis résistance à la corrosion sous contrainte/résistance mécanique obtenu avec l'alliage 2 est équivalent à celui obtenu avec l'alliage 1 traité avec un revenu bi-palier. On bénéficie alors pleinement de l'influence du zirconium sur la qualité de l'éclatement, puisque la longueur moyenne des fissures est passée de 497 mm avec l'alliage au chrome à 430 mm avec l'alliage au zirconium.
- 3-stage tempering improves the compromise between stress corrosion resistance and mechanical resistance. Between income A and income C, the conductivity increases significantly, with a slight gain in mechanical strength. The increase in conductivity translates well into an increase in resistance to corrosion under stress since there is no rupture at 60 d at 280 MPa.
- the tri-level income with a second level at 190 ° C leads to a compromise in resistance to stress corrosion / mechanical resistance hardly better than that obtained with two-bearing income. The temperature range of interest for the second level is therefore limited upwards to 190 ° C.
- thanks to tri-level tempering, the compromise between stress corrosion resistance and mechanical strength obtained with alloy 2 is equivalent to that obtained with alloy 1 treated with bi-level tempering. We then fully benefit from the influence of zirconium on the quality of bursting, since the average length of the cracks went from 497 mm with the chrome alloy to 430 mm with the zirconium alloy.
Claims (8)
- Use of an alloy containing, in % by weight
6.25 ≤ Zn 8.0 Mn ≤ 0.20
1.2 ≤ Mg ≤ 2.2 Ti ≤ 0.05
1.7 ≤ Cu ≤ 2.8
0.10 ≤ Zr ≤ 0.25 Others in each case ≤ 0.05
Fe ≤ 0.20 " in total ≤ 0.15
Si+Fe ≤ 0.40 Balance Al
Cr ≤ 0.05
for the production of bottles for compressed gas. - Use of an Al alloy according to Claim 1, having a content of Mg of ≤ 2.0.
- Use of an Al alloy according to either of Claims 1 or 2, having a content of Mg of ≤ 1.95%.
- Use of an Al alloy according to either of Claims 1 or 3, having a content of Zn of ≥ 6.75.
- Use of an alloy according to one of Claims 1 to 4, having contents of Fe and Si such that Fe is ≤ 0.12% and Fe+Si is ≤ 0.25%.
- Use of an alloy according to one of Claims 1 to 5, having a content of Mn ≤ 0.10%.
- Use of an alloy according to one of Claims 1 to 6, having a content of Zr of between 0.10 and 0.18.
- Process for producing bottles for compressed gas according to one of Claims 1 to 7, characterized in that the final ageing is carried out in 3 stages:1st stage: between 105 and 120°C for 6 to 12 h2nd stage: between 170 and 190°C for 0.5 to 20 h3rd stage: between 105 and 120°C for 12 to 36 h.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9211502A FR2695942B1 (en) | 1992-09-22 | 1992-09-22 | Aluminum alloy for pressurized hollow bodies. |
FR9211502 | 1992-09-22 |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0589807A1 EP0589807A1 (en) | 1994-03-30 |
EP0589807B1 true EP0589807B1 (en) | 1998-06-10 |
Family
ID=9433935
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP93420377A Expired - Lifetime EP0589807B1 (en) | 1992-09-22 | 1993-09-20 | Use of an aluminium alloy for making bottles for compressed gas |
Country Status (10)
Country | Link |
---|---|
EP (1) | EP0589807B1 (en) |
JP (1) | JPH06256882A (en) |
AT (1) | ATE167237T1 (en) |
AU (1) | AU670114B2 (en) |
BR (1) | BR9303846A (en) |
CA (1) | CA2106320C (en) |
DE (1) | DE69319051T2 (en) |
DK (1) | DK0589807T3 (en) |
ES (1) | ES2118209T3 (en) |
FR (1) | FR2695942B1 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10301710B2 (en) | 2005-01-19 | 2019-05-28 | Otto Fuchs Kg | Aluminum alloy that is not sensitive to quenching, as well as method for the production of a semi-finished product |
EP3670690A1 (en) | 2018-12-20 | 2020-06-24 | Constellium Issoire | Al-zn-cu-mg alloys and their manufacturing process |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2805282B1 (en) * | 2000-02-23 | 2002-04-12 | Gerzat Metallurg | A1ZNMGCU ALLOY PRESSURE HOLLOW BODY PROCESS |
CA2528614C (en) * | 2003-06-24 | 2012-06-05 | Pechiney Rhenalu | Products made from al/zn/mg/cu alloys with improved compromise between static mechanical properties and tolerance to damage |
ES2393706T3 (en) * | 2003-12-16 | 2012-12-27 | Constellium France | Modeled product in the form of laminated sheet and structure element for Al-Zn-Cu-Mg alloy aircraft |
JP5276341B2 (en) * | 2008-03-18 | 2013-08-28 | 株式会社神戸製鋼所 | Aluminum alloy material for high pressure gas containers with excellent hydrogen embrittlement resistance |
FR2977297B1 (en) * | 2011-06-29 | 2015-01-16 | Air Liquide | ALUMINUM BOTTLE FOR MIXTURE GAS NO / NITROGEN |
FR2977298B1 (en) * | 2011-06-29 | 2015-02-06 | Air Liquide | ALUMINUM BOTTLE FOR MIXTURE GAS NO / NITROGEN |
FR3068370B1 (en) * | 2017-07-03 | 2019-08-02 | Constellium Issoire | AL-ZN-CU-MG ALLOYS AND PROCESS FOR PRODUCING THE SAME |
CN111876639A (en) * | 2020-08-06 | 2020-11-03 | 北部湾大学 | 7000 series aluminum alloy for automobile upright column and manufacturing method of plate thereof |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2409320A1 (en) * | 1977-11-21 | 1979-06-15 | Pechiney Aluminium | PROCESS FOR THERMAL TREATMENT OF THICK PRODUCTS IN ALUMINUM ALLOYS OF THE 7000 SERIES CONTAINING COPPER |
FR2510231A1 (en) * | 1981-07-22 | 1983-01-28 | Gerzat Metallurg | METHOD FOR MANUFACTURING HOLLOW BODIES UNDER PRESSURE OF ALUMINUM ALLOYS |
FR2517702B1 (en) * | 1981-12-03 | 1985-11-15 | Gerzat Metallurg | |
FR2601967B1 (en) * | 1986-07-24 | 1992-04-03 | Cerzat Ste Metallurg | AL-BASED ALLOY FOR HOLLOW BODIES UNDER PRESSURE. |
-
1992
- 1992-09-22 FR FR9211502A patent/FR2695942B1/en not_active Expired - Lifetime
-
1993
- 1993-09-16 CA CA002106320A patent/CA2106320C/en not_active Expired - Lifetime
- 1993-09-20 DK DK93420377T patent/DK0589807T3/en active
- 1993-09-20 ES ES93420377T patent/ES2118209T3/en not_active Expired - Lifetime
- 1993-09-20 AT AT93420377T patent/ATE167237T1/en active
- 1993-09-20 EP EP93420377A patent/EP0589807B1/en not_active Expired - Lifetime
- 1993-09-20 DE DE69319051T patent/DE69319051T2/en not_active Expired - Lifetime
- 1993-09-21 BR BR9303846A patent/BR9303846A/en unknown
- 1993-09-21 AU AU47511/93A patent/AU670114B2/en not_active Expired
- 1993-09-21 JP JP5234641A patent/JPH06256882A/en active Pending
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10301710B2 (en) | 2005-01-19 | 2019-05-28 | Otto Fuchs Kg | Aluminum alloy that is not sensitive to quenching, as well as method for the production of a semi-finished product |
EP3670690A1 (en) | 2018-12-20 | 2020-06-24 | Constellium Issoire | Al-zn-cu-mg alloys and their manufacturing process |
Also Published As
Publication number | Publication date |
---|---|
CA2106320A1 (en) | 1994-03-23 |
FR2695942A1 (en) | 1994-03-25 |
ES2118209T3 (en) | 1998-09-16 |
BR9303846A (en) | 1994-03-29 |
JPH06256882A (en) | 1994-09-13 |
DK0589807T3 (en) | 1999-03-22 |
CA2106320C (en) | 2003-11-18 |
AU670114B2 (en) | 1996-07-04 |
FR2695942B1 (en) | 1994-11-18 |
ATE167237T1 (en) | 1998-06-15 |
EP0589807A1 (en) | 1994-03-30 |
DE69319051T2 (en) | 1998-12-10 |
AU4751193A (en) | 1994-03-31 |
DE69319051D1 (en) | 1998-07-16 |
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