US3694196A - Aluminum alloy for galvanic anode - Google Patents
Aluminum alloy for galvanic anode Download PDFInfo
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- US3694196A US3694196A US186218A US3694196DA US3694196A US 3694196 A US3694196 A US 3694196A US 186218 A US186218 A US 186218A US 3694196D A US3694196D A US 3694196DA US 3694196 A US3694196 A US 3694196A
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- Prior art keywords
- anode
- aluminum
- alloy
- gallium
- tin
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- 229910000838 Al alloy Inorganic materials 0.000 title abstract description 11
- 229910052782 aluminium Inorganic materials 0.000 abstract description 26
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 abstract description 26
- 239000011701 zinc Substances 0.000 abstract description 24
- GYHNNYVSQQEPJS-UHFFFAOYSA-N Gallium Chemical compound [Ga] GYHNNYVSQQEPJS-UHFFFAOYSA-N 0.000 abstract description 22
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 abstract description 22
- 229910052733 gallium Inorganic materials 0.000 abstract description 22
- 229910052718 tin Inorganic materials 0.000 abstract description 22
- 229910052725 zinc Inorganic materials 0.000 abstract description 22
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 abstract description 21
- 229910052797 bismuth Inorganic materials 0.000 abstract description 20
- JCXGWMGPZLAOME-UHFFFAOYSA-N bismuth atom Chemical compound [Bi] JCXGWMGPZLAOME-UHFFFAOYSA-N 0.000 abstract description 19
- 229910045601 alloy Inorganic materials 0.000 description 32
- 239000000956 alloy Substances 0.000 description 32
- 239000011135 tin Substances 0.000 description 21
- 239000000203 mixture Substances 0.000 description 6
- 238000004090 dissolution Methods 0.000 description 4
- 230000007797 corrosion Effects 0.000 description 3
- 238000005260 corrosion Methods 0.000 description 3
- QSHDDOUJBYECFT-UHFFFAOYSA-N mercury Chemical compound [Hg] QSHDDOUJBYECFT-UHFFFAOYSA-N 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 2
- 238000005275 alloying Methods 0.000 description 2
- 239000010953 base metal Substances 0.000 description 2
- 230000000052 comparative effect Effects 0.000 description 2
- 238000010828 elution Methods 0.000 description 2
- 229910052749 magnesium Inorganic materials 0.000 description 2
- 239000011777 magnesium Substances 0.000 description 2
- 229910052753 mercury Inorganic materials 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 239000012267 brine Substances 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 230000006735 deficit Effects 0.000 description 1
- NRUQNUIWEUZVLI-UHFFFAOYSA-O diethanolammonium nitrate Chemical compound [O-][N+]([O-])=O.OCC[NH2+]CCO NRUQNUIWEUZVLI-UHFFFAOYSA-O 0.000 description 1
- ZOMNIUBKTOKEHS-UHFFFAOYSA-L dimercury dichloride Chemical class Cl[Hg][Hg]Cl ZOMNIUBKTOKEHS-UHFFFAOYSA-L 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000001747 exhibiting effect Effects 0.000 description 1
- 238000004880 explosion Methods 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 229910052738 indium Inorganic materials 0.000 description 1
- APFVFJFRJDLVQX-UHFFFAOYSA-N indium atom Chemical compound [In] APFVFJFRJDLVQX-UHFFFAOYSA-N 0.000 description 1
- 230000001939 inductive effect Effects 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 229910001092 metal group alloy Inorganic materials 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- HPALAKNZSZLMCH-UHFFFAOYSA-M sodium;chloride;hydrate Chemical compound O.[Na+].[Cl-] HPALAKNZSZLMCH-UHFFFAOYSA-M 0.000 description 1
Images
Classifications
-
- 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
Definitions
- This invention relates to a metal alloy for use as the galvanic anode, and, more particularly, to an aluminum alloy for such galvanic anode having an improved galvanic, or anode current characteristics.
- single figure is a graphical representation showing a relationship between the anode current density and the galvanic (or anode) current efiiciency of the galvanic anode made of the alloy according to the present invention.
- the aluminum alloy for the galvanic anode according to the present invention is an improvement in the known alloy of this type and purpose.
- It is another object of the present invention to provide The present invention has succeeded in developing the aluminum alloy for the galvanic anode having further improved electrical properties by adding to the alloy consisting of aluminum, zinc, and tin particular elements capable of imparting galvanic anode characteristics such as, for example, bismuth, gallium, etc.
- the resulting anode When 0.5 to 10% of zinc is added to the base aluminum, the resulting anode possesses a stabilized low anode potential and high galvanic current efiiciency.
- the zinc content of below 0.5% does not result in any appreciable improvement in the anode (galvanic) current efliciency.
- the zinc content exceeding 10% does not yield so remarkable an effect as in the content of less than 10%.
- Addition of tin at a rate of below 0.05% increases the anode potential and lowers the anode current efiiciency. Again, when the tin content exceeds 1.0%, the current efliciency also lowers. From this, the appropriate content of tin in the alloy is from 0.05 to 1.0%.
- the appropriate adding quantity of bismuth is found to be equal to or less than that of tin. If the adding quantity of bismuth exceeds 1.0%, adhesion of corrosion product to the anode surface increases, and the condition for elution (a state of galvanic dissolution of the anode) deteriorates. With the gallium content of below 0.005%, no current eiiiciency improves. However, within the range of from 0.005 to 0.3%, improvement in the current eiiiciency can be recognized. Further increase in the adding quantity of gallium lowers the current efficiency, while low anode potential which is one of the characteristics of this invention is resulted. However, addition of large amount of gallium causes irregularity in dissolution on the anode surface, which brings about undesirable slimming phenomenon at the dissolved portion, accompanying impairment of economic value of the alloy product, hence the quantity exceeding 1.0% is not recommendable.
- EXAMPLE An aluminum base metal (containing 0.12% of iron, 0.08% of silicon, 0.003% of copper, and remainder of aluminum) was dissolved in a graphite crucible, and, at a temperature of 680 C., zinc, tin, bismuth, and gallium are simultaneously added to the molten base metal, sufficiently agitated, and cast into an ingot of the alloy composition as shown in the following Table 2.
- anode current efliciency are as shown in the figure, from which it will be noted that the anode of this alloy maintains its high performance even at a low current density, and, while its conditions for elution may be local at the initial stage, the dissolution of the anode surface proceeds with lapse of time until the entire surface thereof dissolves with the consequence that there is no possibility of adhesion of corrosion products, and the anode can be successfully used at a high specific resistance, which greatly contributes to the corrosion engrneermg.
- Aluminum alloy for galvanic anode which consists of 05-10% zinc, 0.05-1.0% tin, 0.05-1.0% bismuth, 0.0051.0% gallium, and remainder of aluminum.
- Alloy of claim 1 consisting of 6.0% zinc, 0.05% tin, 0.1% bismuth, 0.01% gallium, and remainder of aluminum.
- Alloy of claim 1 consisting of 0.5% zinc, 0.1% tin, 0.1% bismuth, 0.01% gallium, and remainder of aluminum.
- Alloy of claim 1 consisting of 6.0% zinc, 0.05% tin, 0.05% bismuth, 0.005% gallium, and remainder of aluminum.
- Alloy of claim 1 consisting of 6.0% zinc, 0.1% tin, 0.1% bismuth, 0.01% gallium, and remainder of aluminum.
- Alloy of claim 1 consisting of 6.0% zinc, 0.1% tin, 0.05% bismuth, 0.01% gallium, and remainder of aluminum.
- the comparative alloy samples are of the known alloy composition as well as those produced by adding to the aluminum base any one of the above-mentioned alloying components.
- the alloys of the present invention in which all of the alloying components are properly combined and added to the base aluminum, exhibit the current efiiciency of higher than 90% at the anode potential of from 1.0 v. to 1.1 v., and or so at about -1.5 v.
- Alloy of claim 1 consisting of 6.0% zinc, 1.0% tin, 1.0% bismuth, 0.1% gallium, and remainder of aluminum.
- Alloy of claim 1 consisting of 10.0% zinc, 0.1% tin, 0.1% bismuth, 0.01% gallium, and remainder of aluminum.
- Alloy of claim 1 consisting of 10.0% zinc, 1.0% tin, 1.0% bismuth, 0.1% gallium, and remainder of aluminum.
- Alloy of claim 1 consisting of 2.0% zinc, 0.5% tin, 0.5% bismuth, 0.3% gallium, and remainder of aluminum.
- Alloy of claim 1 consisting of 6.0% zinc, 0.5% tin, 0.5% bismuth, 0.3% gallium, and remainder of Ga, and remainder of A l) for its anode current density aluminum.
- Alloy pf claim 1 cor istlng of 6.0% zir c, 1.0% Referenges Cited glndmilfigzi. blsmuth, 0.3% galhum, and remamder of UNITED STATES PATENTS 14. Alloy 9f claim 1 consistlng of 2.0% zix c, 1.0% 3,616,420 10/1971 Brougham 75-146 b1smuth, 0.5% gallium, and remamder of 5 RICHARD O DEAN Primary Examiner 15. Alloy of claim 1 consisti ng of 6.0% zin c, 1.0% US CL tm, 1.0% blsmuth, 0.5% galllum, and remalnder of aluminum. 75-140; 204-148, 197, 293
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Prevention Of Electric Corrosion (AREA)
Abstract
ALUMINUM ALLOY FOR GALVANIC ANODE HAVING IMPROVED ANODE POTENIAL AND ANODE CURRENT EFFICIENCY WHICH CONSISTS OF ALUMINUM BASE AND SPECIFIC QUANTITIES OF ZINC, TIN, BISMUTH, GALLIUM CAPABLE OF IMPARTING TO THE BASE ALUMINUM THESE REQUIRED GALVANIC ANODE CHARACTERISTICS.
Description
Sept. 26, 1972 KAZUO TODA ETAL 3,694,196
ALUMINUM ALLOY FOR GALVANIC ANODE Filed Oct. 4, 1971 0.65 o'.: '1 lb ANODE CURRENT DENSITY z) KAZUO TODA,
TOSUKE MURAI, CHIKATOSHI MIURA and YUICHI TAMURA,
INVENTOR United States Patent US. Cl. 75-146 15 Claims ABSTRACT OF THE DISCLOSURE Aluminum alloy for galvanic anode having improved anode potential and anode current efiiciency which consists of aluminum base and specific quantities of zinc, tin, bismuth, gallium capable of imparting to the base aluminum these required galvanic anode characteristics.
This invention relates to a metal alloy for use as the galvanic anode, and, more particularly, to an aluminum alloy for such galvanic anode having an improved galvanic, or anode current characteristics.
"ice
an improved galvanic anode which is easily produced by proper combination of those elements capable of imparting to the aluminum base the requisite galvanic anode characteristics, is not dangerous of inducing explosion, etc. at the time of use, and does not contaminate the surrounding circumstances.
' It is other object of the present invention to provide an aluminum alloy for the galvanic anode of an improved properties, which consists of 0.5-10% zinc, 0.05- 1.0% tin, 0.05-1.0% bismuth, and ODDS-1.0% gallium, and remainder of aluminum.
The foregoing objects as well as the details of this invention will be readily understood from the following description, when read in connection with the preferred examples thereof as well as the accompanying drawing.
In the drawing, single figure is a graphical representation showing a relationship between the anode current density and the galvanic (or anode) current efiiciency of the galvanic anode made of the alloy according to the present invention.
The aluminum alloy for the galvanic anode according to the present invention is an improvement in the known alloy of this type and purpose.
For the known type of the aluminum alloys, there are various kinds such as shown in the following Table l.
TABLE 1 Composition (percent) Ca Cd In Sn Li Zn Al either one or both: 0.11.0{ Remainder. in total 1-10 Do. 0. 5-20 D0. 0. 5-20 DO. 0. 005-0 1 1- 0. 5-20 DO. 0. 520 D0.
There have so far been known various aluminum alloys for the galvanic anode of difierent compositions, in which those elements capable of imparting to aluminum the required galvanic anode characteristics (a low electrode potential and high anode current efliciency) such as, for example, mercury, gallium, indium, tin, magnesium, zinc, etc. are added. (vide: Material Protection, vol. 5 (1966), No. 12, pp. 15-18) Of these alloys, the mercury-containing alloy anode not only requires particular caution :in removing mercury vapor to be generated at the time of its production, but also is liable to contaminate the circumstances surrounding the place where the anode is used. Also, the magnesium-containing alloy is highly dangerous of causing iniiammation due to impact or shock, hence the place for its use is naturally limited.
It is therefore the primary object of the present invention to provide an improved galvanic anode having a low anode potential and a high anode current efficiency, as well as exhibiting uniform dissolution at anode consumption.
It is another object of the present invention to provide The present invention has succeeded in developing the aluminum alloy for the galvanic anode having further improved electrical properties by adding to the alloy consisting of aluminum, zinc, and tin particular elements capable of imparting galvanic anode characteristics such as, for example, bismuth, gallium, etc.
When 0.5 to 10% of zinc is added to the base aluminum, the resulting anode possesses a stabilized low anode potential and high galvanic current efiiciency. The zinc content of below 0.5% does not result in any appreciable improvement in the anode (galvanic) current efliciency. On the other hand, the zinc content exceeding 10% does not yield so remarkable an effect as in the content of less than 10%. Addition of tin at a rate of below 0.05% increases the anode potential and lowers the anode current efiiciency. Again, when the tin content exceeds 1.0%, the current efliciency also lowers. From this, the appropriate content of tin in the alloy is from 0.05 to 1.0%. From experimental results, the appropriate adding quantity of bismuth is found to be equal to or less than that of tin. If the adding quantity of bismuth exceeds 1.0%, adhesion of corrosion product to the anode surface increases, and the condition for elution (a state of galvanic dissolution of the anode) deteriorates. With the gallium content of below 0.005%, no current eiiiciency improves. However, within the range of from 0.005 to 0.3%, improvement in the current eiiiciency can be recognized. Further increase in the adding quantity of gallium lowers the current efficiency, while low anode potential which is one of the characteristics of this invention is resulted. However, addition of large amount of gallium causes irregularity in dissolution on the anode surface, which brings about undesirable slimming phenomenon at the dissolved portion, accompanying impairment of economic value of the alloy product, hence the quantity exceeding 1.0% is not recommendable.
In order to enable skilled persons in the art to readily reduce this invention into practice, the following preferred example is presented.
EXAMPLE An aluminum base metal (containing 0.12% of iron, 0.08% of silicon, 0.003% of copper, and remainder of aluminum) was dissolved in a graphite crucible, and, at a temperature of 680 C., zinc, tin, bismuth, and gallium are simultaneously added to the molten base metal, sufficiently agitated, and cast into an ingot of the alloy composition as shown in the following Table 2.
For the purpose of comparison, various kinds of alloy sample were cast in the same manner as in the preceding.
These sample alloys were subjected to tests for their anode potential and current efficiency by causing anode current to flow through artificial brine at an anodic current density of 1 ma./cm. the results of which are as shown in Table 2 below.
and anode current efliciency are as shown in the figure, from which it will be noted that the anode of this alloy maintains its high performance even at a low current density, and, while its conditions for elution may be local at the initial stage, the dissolution of the anode surface proceeds with lapse of time until the entire surface thereof dissolves with the consequence that there is no possibility of adhesion of corrosion products, and the anode can be successfully used at a high specific resistance, which greatly contributes to the corrosion engrneermg.
What we claim is:
1. Aluminum alloy for galvanic anode which consists of 05-10% zinc, 0.05-1.0% tin, 0.05-1.0% bismuth, 0.0051.0% gallium, and remainder of aluminum.
2. Alloy of claim 1 consisting of 6.0% zinc, 0.05% tin, 0.1% bismuth, 0.01% gallium, and remainder of aluminum.
3. Alloy of claim 1 consisting of 0.5% zinc, 0.1% tin, 0.1% bismuth, 0.01% gallium, and remainder of aluminum.
4. Alloy of claim 1 consisting of 6.0% zinc, 0.05% tin, 0.05% bismuth, 0.005% gallium, and remainder of aluminum.
5. Alloy of claim 1 consisting of 6.0% zinc, 0.1% tin, 0.1% bismuth, 0.01% gallium, and remainder of aluminum.
6. Alloy of claim 1 consisting of 6.0% zinc, 0.1% tin, 0.05% bismuth, 0.01% gallium, and remainder of aluminum.
7. Alloy of claim 1 consisting of 6.0% zinc, 1.0% tin,
TABLE 2 Anode potential after Anode Composition (percent) 240 hours current of galvanic efficiency Sample No. Zn Sn Bi Ga Al action 1v.) (percent) Inventive alloys:
6. 0 0. 05 0. 1 0. 01 Remainder 0. 99 95 0.5 0.1 0 1 0.01 d 1.03 01 6. 0 0. 05 0. 05 1. 10 96 6. 0 0. 1 0. l l. 09 91 6. 0 0. 1 0. 05 -1. 11 95 6. 0 1. 0 0. 1 --1. 05 90 6.0 1.0 1.0 1.02 91 10. 0 0. 1 0. 1 1. 11 96 10. 0 l. 0 1. 0 1. 01 97 2. 0 0. 5 0. 5 1. 41 78 6.0 0. 5 0.5 l. 68 6. 0 1. 0 1. 0 l. 46 64 2. 0 1. 0 1. 0 -1. 52 76 6. 0 1.0 1.0 l. 53 75 Note-Electric potentials indicated in this table are the values of the electrode referred to as saturated calomel electrode.
The comparative alloy samples are of the known alloy composition as well as those produced by adding to the aluminum base any one of the above-mentioned alloying components.
As seen from the above table, no satisfactory results in the anode potential or current cfiiciency can be obtained with the comparative alloy samples. In contrast to this, the alloys of the present invention, in which all of the alloying components are properly combined and added to the base aluminum, exhibit the current efiiciency of higher than 90% at the anode potential of from 1.0 v. to 1.1 v., and or so at about -1.5 v.
The measured results of the alloy composition according to the present invention as shown in Sample No. 4 of Table 2 above (6.0% Zn, 0.1% Su, 0.1% Bi, 0.01%
0.1% bismuth, 0.06% gallium, and remainder of aluminum.
8. Alloy of claim 1 consisting of 6.0% zinc, 1.0% tin, 1.0% bismuth, 0.1% gallium, and remainder of aluminum.
9. Alloy of claim 1 consisting of 10.0% zinc, 0.1% tin, 0.1% bismuth, 0.01% gallium, and remainder of aluminum.
10. Alloy of claim 1 consisting of 10.0% zinc, 1.0% tin, 1.0% bismuth, 0.1% gallium, and remainder of aluminum.
11. Alloy of claim 1 consisting of 2.0% zinc, 0.5% tin, 0.5% bismuth, 0.3% gallium, and remainder of aluminum.
12. Alloy of claim 1 consisting of 6.0% zinc, 0.5% tin, 0.5% bismuth, 0.3% gallium, and remainder of Ga, and remainder of A l) for its anode current density aluminum.
13. Alloy pf claim 1 cor istlng of 6.0% zir c, 1.0% Referenges Cited glndmilfigzi. blsmuth, 0.3% galhum, and remamder of UNITED STATES PATENTS 14. Alloy 9f claim 1 consistlng of 2.0% zix c, 1.0% 3,616,420 10/1971 Brougham 75-146 b1smuth, 0.5% gallium, and remamder of 5 RICHARD O DEAN Primary Examiner 15. Alloy of claim 1 consisti ng of 6.0% zin c, 1.0% US CL tm, 1.0% blsmuth, 0.5% galllum, and remalnder of aluminum. 75-140; 204-148, 197, 293
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP45087521A JPS4838285B1 (en) | 1970-10-07 | 1970-10-07 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3694196A true US3694196A (en) | 1972-09-26 |
Family
ID=13917282
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US186218A Expired - Lifetime US3694196A (en) | 1970-10-07 | 1971-10-04 | Aluminum alloy for galvanic anode |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US3694196A (en) |
| JP (1) | JPS4838285B1 (en) |
| DE (1) | DE2150102A1 (en) |
| GB (1) | GB1358899A (en) |
| NO (1) | NO127628B (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2305506A1 (en) * | 1975-03-24 | 1976-10-22 | British Aluminium Co Ltd | IMPROVEMENTS TO ALUMINUM-BASED ALLOYS |
| US4141725A (en) * | 1977-02-14 | 1979-02-27 | Nihon Boshoku Kogyo Kabushiki Kaisha | Aluminum alloy for galvanic anode |
| US4166755A (en) * | 1977-11-02 | 1979-09-04 | Swiss Aluminium Ltd. | Aluminum alloy capacitor foil and method of making |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS55164U (en) * | 1979-05-30 | 1980-01-05 | ||
| JPS5518600U (en) * | 1979-06-18 | 1980-02-05 | ||
| DE3522166C1 (en) * | 1985-06-21 | 1986-08-07 | Daimler-Benz Ag, 7000 Stuttgart | Use of aluminum and an aluminum alloy for the production of fiber-reinforced aluminum castings |
| FR2713244B1 (en) * | 1993-10-29 | 1996-01-12 | France Etat Armement | Consumable cathode protection anode made of aluminum alloy. |
-
1970
- 1970-10-07 JP JP45087521A patent/JPS4838285B1/ja active Pending
-
1971
- 1971-10-04 US US186218A patent/US3694196A/en not_active Expired - Lifetime
- 1971-10-06 NO NO03660/71*[A patent/NO127628B/no unknown
- 1971-10-07 GB GB4671671A patent/GB1358899A/en not_active Expired
- 1971-10-07 DE DE19712150102 patent/DE2150102A1/en active Pending
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2305506A1 (en) * | 1975-03-24 | 1976-10-22 | British Aluminium Co Ltd | IMPROVEMENTS TO ALUMINUM-BASED ALLOYS |
| US4141725A (en) * | 1977-02-14 | 1979-02-27 | Nihon Boshoku Kogyo Kabushiki Kaisha | Aluminum alloy for galvanic anode |
| US4166755A (en) * | 1977-11-02 | 1979-09-04 | Swiss Aluminium Ltd. | Aluminum alloy capacitor foil and method of making |
Also Published As
| Publication number | Publication date |
|---|---|
| NO127628B (en) | 1973-07-23 |
| JPS4838285B1 (en) | 1973-11-16 |
| DE2150102A1 (en) | 1972-04-13 |
| GB1358899A (en) | 1974-07-03 |
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