NO117749B - - Google Patents
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- Publication number
- NO117749B NO117749B NO166134A NO16613466A NO117749B NO 117749 B NO117749 B NO 117749B NO 166134 A NO166134 A NO 166134A NO 16613466 A NO16613466 A NO 16613466A NO 117749 B NO117749 B NO 117749B
- Authority
- NO
- Norway
- Prior art keywords
- percent
- silicon
- copper
- per cent
- magnesium
- Prior art date
Links
- 229910045601 alloy Inorganic materials 0.000 claims description 25
- 239000000956 alloy Substances 0.000 claims description 25
- 229910052710 silicon Inorganic materials 0.000 claims description 19
- 239000010703 silicon Substances 0.000 claims description 19
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 18
- 239000010949 copper Substances 0.000 claims description 18
- 229910052802 copper Inorganic materials 0.000 claims description 18
- 239000000945 filler Substances 0.000 claims description 16
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims description 10
- 229910052749 magnesium Inorganic materials 0.000 claims description 10
- 239000011777 magnesium Substances 0.000 claims description 10
- 238000003466 welding Methods 0.000 claims description 9
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 6
- 239000010936 titanium Substances 0.000 claims description 6
- 229910052719 titanium Inorganic materials 0.000 claims description 6
- 229910052751 metal Inorganic materials 0.000 claims description 5
- 239000002184 metal Substances 0.000 claims description 5
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 4
- 229910000861 Mg alloy Inorganic materials 0.000 claims description 4
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical group [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 4
- 229910052782 aluminium Inorganic materials 0.000 claims description 4
- -1 aluminum-silicon-copper-magnesium Chemical compound 0.000 claims description 4
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 claims description 3
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 claims description 3
- 239000011701 zinc Substances 0.000 claims description 3
- 229910052725 zinc Inorganic materials 0.000 claims description 3
- 229910052742 iron Inorganic materials 0.000 claims description 2
- 150000002739 metals Chemical class 0.000 claims description 2
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 17
- 239000012895 dilution Substances 0.000 description 14
- 238000010790 dilution Methods 0.000 description 14
- 239000000203 mixture Substances 0.000 description 7
- 239000010953 base metal Substances 0.000 description 5
- 239000004411 aluminium Substances 0.000 description 3
- 229910000838 Al alloy Inorganic materials 0.000 description 2
- 238000005336 cracking Methods 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 229910000881 Cu alloy Inorganic materials 0.000 description 1
- 229910000737 Duralumin Inorganic materials 0.000 description 1
- PXGOKWXKJXAPGV-UHFFFAOYSA-N Fluorine Chemical compound FF PXGOKWXKJXAPGV-UHFFFAOYSA-N 0.000 description 1
- JRBRVDCKNXZZGH-UHFFFAOYSA-N alumane;copper Chemical compound [AlH3].[Cu] JRBRVDCKNXZZGH-UHFFFAOYSA-N 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 239000011737 fluorine Substances 0.000 description 1
- 229910052731 fluorine Inorganic materials 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21S—NON-PORTABLE LIGHTING DEVICES; SYSTEMS THEREOF; VEHICLE LIGHTING DEVICES SPECIALLY ADAPTED FOR VEHICLE EXTERIORS
- F21S8/00—Lighting devices intended for fixed installation
- F21S8/02—Lighting devices intended for fixed installation of recess-mounted type, e.g. downlighters
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21W—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES F21K, F21L, F21S and F21V, RELATING TO USES OR APPLICATIONS OF LIGHTING DEVICES OR SYSTEMS
- F21W2111/00—Use or application of lighting devices or systems for signalling, marking or indicating, not provided for in codes F21W2102/00 – F21W2107/00
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21W—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES F21K, F21L, F21S and F21V, RELATING TO USES OR APPLICATIONS OF LIGHTING DEVICES OR SYSTEMS
- F21W2111/00—Use or application of lighting devices or systems for signalling, marking or indicating, not provided for in codes F21W2102/00 – F21W2107/00
- F21W2111/02—Use or application of lighting devices or systems for signalling, marking or indicating, not provided for in codes F21W2102/00 – F21W2107/00 for roads, paths or the like
Description
Fyll-legering for sveisning av aluminium-silisium-kobber-niagnesium-legeringer. Filler alloy for welding aluminium-silicon-copper-niagnesium alloys.
Når aluminium-legeringer sveises under anvendelse av et fyllmateriale, opptrer der en fortynning av fyllmaterialet ved iblanding av grunnmetallet i en utstrek-ning som varierer med arten av sømmen og med sveiseteknikken. Denne fortynning har betydelig innflytelse på sammensetningen av sveisesømmen, og det er funnet at fyllmetallet i sveisesømmen kan for-tynnes opptil 80 pst. eller mer når der sveises en skjøt hvor kantene er utført med butt mot hverandre anliggende, rette kanter. When aluminum alloys are welded using a filler material, a dilution of the filler material occurs when the base metal is mixed in to an extent that varies with the nature of the seam and with the welding technique. This dilution has a significant influence on the composition of the weld seam, and it has been found that the filler metal in the weld seam can be diluted up to 80 per cent or more when a joint is welded where the edges are made with blunt, straight edges abutting each other.
Ved fremstillingen av hulkilskjøt kan In the production of hollow wedge joints can
fortynningen imidlertid være så liten som 25 pst. Det vil derfor ses at enhver fyll-stav av en viss sammensetning vil frem-bringe sveisesømmer med sterkt varierende sammensetning og egenskaper i avhen-gighet av typen av skjøten som den brukes for. however, the dilution be as small as 25 per cent. It will therefore be seen that any filler rod of a certain composition will produce weld seams with greatly varying composition and properties depending on the type of joint for which it is used.
Foreliggende oppfinnelse angår sveisning av aluminium-silisium-koblber-magnesium-legeringer og går ut på en fyll-legering som gjør det mulig å fremstille en sveisesøm under sterkt varierende omsten-digheter og med varierende fortynning, hvor sammensetningen av sømmen i alle tilfelle innen visse grenser forblir tilfredsstillende. De aluminium-silisium-kobber-magnesium-legeringer som fyll-legeringen ifølge oppfinnelsen er beregnet for, kan inneholde mellom 3,5 og 5 pst. kobber, og for de i handelen forekommende legeringer ligger grensene for kobberinnholdet i alminnelighet på mellom 3,9 og 4,5 pst. Le-geringene inneholder gjerne silisium i en mengde på mellom 0,5 og 1,2 pst., og magnesium i en mengde på omkring 0,5 pst. The present invention relates to the welding of aluminium-silicon-cobbler-magnesium alloys and is based on a filler alloy which makes it possible to produce a weld seam under widely varying circumstances and with varying dilution, where the composition of the seam is in all cases within certain limits remain satisfactory. The aluminum-silicon-copper-magnesium alloys for which the filler alloy according to the invention is intended can contain between 3.5 and 5 percent copper, and for the commercially available alloys the limits for the copper content are generally between 3.9 and 4.5 per cent. The alloys usually contain silicon in an amount of between 0.5 and 1.2 per cent, and magnesium in an amount of around 0.5 per cent.
Fyll-legeringen ifølge oppfinnelsen inneholder mellom 5,5 og 7,5 pst. kobber, mellom 3,0 og 4,0 pst. silisium, mellom 0,3 og 1,0 pst. magnesium og mellom 0,1 og 0,8 pst. titan. Videre kan fyll-legeringen inneholde én eller flere av følgende bestandde-ler: Opptil 1,0 pst. mangan, opptil 1,0 pst. jern, og opptil 0,8 pst. sink. Resten av legeringen utgjøres av aluminium. The filler alloy according to the invention contains between 5.5 and 7.5 percent copper, between 3.0 and 4.0 percent silicon, between 0.3 and 1.0 percent magnesium and between 0.1 and 0.8 pst titanium. Furthermore, the filler alloy may contain one or more of the following components: Up to 1.0 percent manganese, up to 1.0 percent iron, and up to 0.8 percent zinc. The rest of the alloy is made up of aluminium.
En foretrukken sammensetning av fyll-legeringen er 7,0 pst. kobber, 3,5 pst. silisium, 0,6 pst. magnesium og 0,5 pst. titan, mens resten i det vesentligste utgjøres av aluminium. A preferred composition of the filler alloy is 7.0% copper, 3.5% silicon, 0.6% magnesium and 0.5% titanium, while the rest is essentially aluminium.
Fyll-legeringen ifølge oppfinnelsen gir tilfredsstillende sammensetning av sveisesømmer ved sveisning av de foran angitte legeringer ved opptil 70 pst. fortynning. For sveiseforbindelser av en form som gir større fortynning enn 70 pst. er det sann-synligvis mer tilfredsstillende å bruke en aluminiumlegering som inneholder 10 pst. silisium og 4 pst. kobber. The filler alloy according to the invention provides a satisfactory composition of weld seams when welding the above-mentioned alloys at up to 70 percent dilution. For weld joints of a form which gives greater dilution than 70 per cent, it is probably more satisfactory to use an aluminum alloy containing 10 per cent silicon and 4 per cent copper.
Med et grunnmetall som har et kobberinnhold på 3,9 pst. vil den foretrukne legering ha et kobberinnhold i sveisen på 4,8 pst. ved 70 pst. fortynning og 6,25 pst. ved 25 pst. fortynning. Ved den øvre kob-bergrense på 4,5 pst. kobber i grunnmetallet inneholder sveisen 5,25 pst. kobber ved 70 pst. fortynning og 6,4 pst. kobber ved With a base metal having a copper content of 3.9 percent, the preferred alloy will have a copper content in the weld of 4.8 percent at 70 percent dilution and 6.25 percent at 25 percent dilution. At the upper copper limit of 4.5 percent copper in the base metal, the weld contains 5.25 percent copper at 70 percent dilution and 6.4 percent copper at
25 pst. fortynning. 25 percent dilution.
Ved anvendelse av den foretrukne legering er silisiuminnholdet i sveisen med 0,5 pst. silisiuminnhold i grunnmetallet 1,4 pst. silisium ved 70 pst. fortynning og 2,7 pst. silisium ved 25 pst. fortynning. Med et grunnmetall som inneholder 1,2 pst. silisium vil sveisen inneholde 1,9 pst. silisium ved 70 pst. fortynning og 2,9 pst. silisium ved 25 pst. fortynning. Virkningen av sili-siumet er å gjøre aluminium-kobberlege-ringene mindre tilbøyelige til å sprekke. Ved anvendelse av et sveisemetall med et innhold på omkring 5 pst. kobber er et silisiuminnhold på omkring 2 pst. mest fordelaktig, og det er liten fordel i å øke silisiuminnholdet vesentlig over dette innhold, da sveisens egenskaper ved høyere silisiuminnhold blir dårligere og sveisen ved eld-ning blir «trett» (sluggish). When using the preferred alloy, the silicon content in the weld with 0.5 percent silicon content in the base metal is 1.4 percent silicon at 70 percent dilution and 2.7 percent silicon at 25 percent dilution. With a base metal containing 1.2 percent silicon, the weld will contain 1.9 percent silicon at 70 percent dilution and 2.9 percent silicon at 25 percent dilution. The effect of the silicon is to make the aluminium-copper alloy rings less prone to cracking. When using a weld metal with a content of around 5 per cent copper, a silicon content of around 2 per cent is most advantageous, and there is little advantage in increasing the silicon content significantly above this content, as the properties of the weld become worse at a higher silicon content and the weld at Firing becomes "tired" (sluggish).
Det er ikke mulig å eliminere magnesium fra sveisemetallet og heller ikke er det noen vesentlig fordel å øke magnesium-innholdet utover det som i alminnelighet er tilstede i vandig duraluminium-legeringer. Et høyere magnesiuminnhold gir større styrke, men lavere strekkbarhet. Et pas-sende kompromiss for grensene for magnesiuminnhold i fyll-legeringen er fra 0,3 pst. til 0,6 pst. It is not possible to eliminate magnesium from the weld metal, nor is there any significant advantage to increasing the magnesium content beyond what is generally present in aqueous duralumin alloys. A higher magnesium content gives greater strength, but lower extensibility. A suitable compromise for the limits of magnesium content in the filler alloy is from 0.3 percent to 0.6 percent.
Det skal bemerkes at det fra sveitsisk patent nr. 231.935 er kjent å anvende en fyll-legering for sveisning av aluminium-silisium-kobber-magnesium-legeringer, hvilken fyll-legering består av 3—5 pst. kobber, 1—2 pst. silisium, 0—0,5 pst. magnesium, 0,1—0,5 pst. titan, 0—1 pst. mangan, 0—0,2 pst. fluor og ubetydelige meng-der av andre metaller, f. eks. sink, mens resten er aluminium. It should be noted that from Swiss patent no. 231,935 it is known to use a filler alloy for welding aluminum-silicon-copper-magnesium alloys, which filler alloy consists of 3-5 percent copper, 1-2 percent silicon, 0-0.5% magnesium, 0.1-0.5% titanium, 0-1% manganese, 0-0.2% fluorine and negligible amounts of other metals, e.g. zinc, while the rest is aluminium.
Legeringen ifølge foreliggende oppfinnelse adskiller seg fra sammensetningen av legeringen som er angitt i patentet, når bortses fra titaninholdet. Kobberinnholdet skal ifølge foreliggende oppfinnelse være fra 5,5—7,5 pst., mens der i det sveitsiske patent er tale om et kobbérinnhold på 3— 5,5 pst. For såvidt angår silisiuminnholdet er forskjellen ennå større, da der ifølge foreliggende oppfinnelse er angitt 3—4 pst., mens der i det sveitsiske patent er angitt 1—2 pst. De foreliggende forskjeller resul-terer i en legering som gir meget bedre motstandsdyktighet mot sveisesprekker, som praktisk talt fullstendig unngås. Opp-finnerne har funnet det nødvendig å anvende et forholdsvis høyt kobberinnhold i legeringen, ikke bare for å forbedre mot-standsdyktigheten mot sprekkdannelse, men også for å oppnå en maksimalstyrke av skjøten uten oppløsningsvarm behandling etter sveisingen. I det sveitsiske pa-tentskrift angis at en slik varm behandling er nødvendig etter sveisningen for oppnå-else av en sterk sveis. Selv om en slik opp-varming også kan anvendes ved en legering ifølge foreliggende oppfinnelse, er dette hverken nødvendig eller fordelaktig. The alloy according to the present invention differs from the composition of the alloy stated in the patent, apart from the titanium content. According to the present invention, the copper content must be from 5.5-7.5 per cent, while in the Swiss patent there is a copper content of 3-5.5 per cent. As far as the silicon content is concerned, the difference is even greater, since according to the present invention there 3-4 per cent is stated, while in the Swiss patent 1-2 per cent is stated. The present differences result in an alloy that provides much better resistance to welding cracks, which is practically completely avoided. The inventors have found it necessary to use a relatively high copper content in the alloy, not only to improve the resistance to cracking, but also to achieve a maximum strength of the joint without solution heat treatment after welding. In the Swiss patent, it is stated that such a hot treatment is necessary after welding to achieve a strong weld. Although such heating can also be used with an alloy according to the present invention, this is neither necessary nor advantageous.
Claims (2)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IT2884465 | 1965-12-28 |
Publications (1)
Publication Number | Publication Date |
---|---|
NO117749B true NO117749B (en) | 1969-09-22 |
Family
ID=11224304
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
NO166134A NO117749B (en) | 1965-12-28 | 1966-12-23 |
Country Status (10)
Country | Link |
---|---|
AT (1) | AT284960B (en) |
BE (1) | BE691499A (en) |
CH (1) | CH445640A (en) |
DE (1) | DE1539378A1 (en) |
ES (1) | ES325142A1 (en) |
GB (1) | GB1098560A (en) |
GR (1) | GR31996B (en) |
NL (1) | NL6618012A (en) |
NO (1) | NO117749B (en) |
SE (1) | SE336622B (en) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB8512622D0 (en) * | 1985-05-18 | 1985-06-19 | Ranton & Co Ltd | Electrical accessory fixing systems |
CH678567A5 (en) * | 1989-08-02 | 1991-09-30 | Henapot Ag | |
DE19919080A1 (en) * | 1999-04-27 | 2000-11-02 | Insta Elektro Gmbh & Co Kg | Lighting device for illuminating surfaces and spaces incorporates light-emitting semiconductor elements acting as sources of light supplied with a power source and controlled by electronic components. |
DE10322177A1 (en) * | 2003-05-16 | 2004-12-02 | Ludwig Leuchten Kg | LED downlight |
GB0510462D0 (en) * | 2005-05-23 | 2005-06-29 | Aurora Ltd | Casing mounted lamps |
ITUB20160590A1 (en) * | 2016-02-09 | 2017-08-09 | Beghelli Spa | BUILT-IN LIGHTING DEVICE |
-
1966
- 1966-04-05 ES ES0325142A patent/ES325142A1/en not_active Expired
- 1966-12-20 BE BE691499D patent/BE691499A/xx unknown
- 1966-12-21 CH CH1831266A patent/CH445640A/en unknown
- 1966-12-22 GB GB57449/66A patent/GB1098560A/en not_active Expired
- 1966-12-22 NL NL6618012A patent/NL6618012A/xx unknown
- 1966-12-23 NO NO166134A patent/NO117749B/no unknown
- 1966-12-27 AT AT1187766A patent/AT284960B/en not_active IP Right Cessation
- 1966-12-28 SE SE17835/66A patent/SE336622B/xx unknown
- 1966-12-28 DE DE19661539378 patent/DE1539378A1/en active Pending
-
1967
- 1967-01-24 GR GR670131996A patent/GR31996B/en unknown
Also Published As
Publication number | Publication date |
---|---|
GB1098560A (en) | 1968-01-10 |
SE336622B (en) | 1971-07-12 |
ES325142A1 (en) | 1967-01-01 |
CH445640A (en) | 1967-10-31 |
DE1539378A1 (en) | 1970-07-16 |
GR31996B (en) | 1967-05-02 |
BE691499A (en) | 1967-05-29 |
NL6618012A (en) | 1967-06-29 |
AT284960B (en) | 1970-10-12 |
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