US3278300A - Aluminum alloys for electric conductors - Google Patents

Aluminum alloys for electric conductors Download PDF

Info

Publication number
US3278300A
US3278300A US373559A US37355964A US3278300A US 3278300 A US3278300 A US 3278300A US 373559 A US373559 A US 373559A US 37355964 A US37355964 A US 37355964A US 3278300 A US3278300 A US 3278300A
Authority
US
United States
Prior art keywords
alloy
aluminum
alloys
conductor
strength
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
Application number
US373559A
Inventor
Koike Kichizo
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Furukawa Electric Co Ltd
Original Assignee
Furukawa Electric Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Furukawa Electric Co Ltd filed Critical Furukawa Electric Co Ltd
Application granted granted Critical
Publication of US3278300A publication Critical patent/US3278300A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01BCABLES; CONDUCTORS; INSULATORS; SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING OR DIELECTRIC PROPERTIES
    • H01B1/00Conductors or conductive bodies characterised by the conductive materials; Selection of materials as conductors
    • H01B1/02Conductors or conductive bodies characterised by the conductive materials; Selection of materials as conductors mainly consisting of metals or alloys
    • H01B1/023Alloys based on aluminium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium

Definitions

  • Aluminum cable steel reinforced has been conventionally used for overhead power transmission lines: however, improved heat resistance and current carrying capacity of aluminum alloy conductors have long been required considering special transmission conditions such as bus conductors in heavy capacity power station, transmission lines having a load factor of 0.5 or less (single purpose transmission lines for connecting thermal power station and pumping-up power station), and for emergency transmission line for two circuits parallel operation in case of fault of a single circuit, etc.
  • various aluminum alloys for electric conductors have been studied, and an alloy including zirconium is disclosed in Japanese Patent No. 261,993.
  • the heat resistance of Al-Zr alloys is improved as the Zr content is increased, on the other hand; the electric conductivity is reduced as zirconium increases, so that addition quantity of zirconium should be considerably limited in order to obtain an alloy having high electric conductivity and low ohmic loss.
  • the heat resistance becomes very low, not adapted for the heat resistant conductive alloy conductors.
  • Aldrey alloys have been used for overhead power transmission as well as for aluminum cable steel reinforced; however, being a heat treated product, the said alloy needs a series of treatments in the process of manufacturing such as solution heat treatment-aging-wire drawing-aging, which make the alloy rather costly, and also, being an age hardening alloy, it has a disadvantage that the continuous operation temperature of the conductor cannot be made higher than that of an ordinary aluminum wire.
  • Al-Mg alloys for instance 5005 alloy, have been put into use; however, it being a solid solution type, it is difficult to increase its electric conductivity more than 55% when the tensile strength is not less than 25 kg/mm?
  • magnesium content must be reduced at the sacrifice of mechanical properties such as tensile strength and fatigue strength.
  • overhead transmission line conductor is required to have excellent sag-tension characteristics, vibration fatigue strength, creep characteristics, etc.
  • the principal object of the invention is to obviate the defects of the conventional conductors and to provide aluminum base alloys having increased electric conductivity and substantially equivalent heat resistance to that of the conventional heat resisting conductive alloys,
  • Another object of the invention is to provide aluminum alloys having high mechanical strength, high heat resistance and conductivity by improving the mechanical strength of conventional heat resistant aluminum alloy conductors.
  • a further object of the invention is to provide non-heat treatable aluminum alloys having excellent strength and high conductivity to be manufactured by the same process as ordinary aluminum conductors.
  • the essential ingredients of the alloys of the invention consist of (Ll-0.5% of iron, 06-30% of Re, and the remainder of aluminum.
  • the reason for limiting the iron and Re contents to the above values in the invention is that for iron and Re contents of less than 0.1% and 0.6% respectively, heat resistance increase is not effective and that for iron content of more than 0.5%, heat resistance increase is saturated, which may possibly deteriorate electric conductivity and corrosion resistance.
  • the preferable composition of the alloys of the invention is 0.6l.5% of Re, 0.15-0.25 of iron and the remainder of aluminum.
  • the preferred composition of said alloy is 0.6-1.5% of Re, 0.150.25% of iron, 0.04-0.06% of zirconium and the remainder of aluminum.
  • the tensile strength of the aluminum conductor made of said alloys of the invention consisting of Al-Fe-Re or Al-Fe-Re-Zr is substantially the same as that of EC. grade aluminum (99.60 Al) conductor.
  • the inventor has found that addition of a small quantity of magnesium to Al-Fe Re alloy increases the mechanical strength without impairing electric conductivity and heat resistance. That is, the alloy developed consists of 0.10.5% of iron, 0.63.0% of Re, 0.020.6% of magnesium and the remainder of aluminum. A magnesium content of 0.020.l% greatly improves the characteristics of heat resistant high strength aluminum alloy;
  • a magnesium content of 0.10.6% improves characteristics of high strength heat resistant conductive aluminum alloy.
  • the alloys of the invention can be grouped into two categories, namely, an alloy consisting of 0.10.5% of iron, 0.63.0% of Re, 0.020.1% of magnesium and the remainder of aluminum, and an alloy consisting of 0.10.5% of iron, 06-30% of Re, 0.10.6% of magnesium and the remainder of aluminum.
  • the alloy of the invention has about 35% higher electric conductivity than conventional ones for the same tensile strength, and has higher tensile strength for the same electric conductivity.
  • No'rE.Rc used had the following composition:
  • Table 4 100 0. 130 0. 160 C. i 190 C. I 220 C.
  • the alloy of the invention being hardened by heating instead of softening is due not to simple precipitation hardening but to a particular phenomenon related to the reciprocal action between solute foreign atoms and dislocations caused by cold working.
  • Aluminum alloy wire of the EXAMPLE 5 mventlon' 0 6 R m The quaternary alloys consisting of Fe-Re-Zr-Al in the naindcr.
  • Table 9 were made into wires of 3.0 Do. Conductor grade alum 10 2.9 mm. dra. to measure the tensile strength and con wire 0.18 0.08 Do. ductivity at room temperature and to determine the rate of increase and decrease in tensile strength by measuring Table 6 Electric Tensile Rate of Creep Name of Alloy conducstrength increase and charactivity (kg/mm?) decrease teristic (percent) (percent) (percent) Aluminum alloy wire of the invention:
  • the rate of increase and decrease is expressed in terms tensile strength after heating them at 120 C. for days of a ratio of the tensile strength after the wire is heated and by measuring the same strength after cooling them at C. for 500 hours to the tensile strength at room down to room temperature. The results are shown in temperature before heating.
  • the creep characteristic is Table 10.
  • the aluminum alloy conductor of the invention has a higher conductivity Electric and a better anti-softening characteristic after heating for 5 Tensile conducand delong time, and more excellent creep characteristics at high Name 01 figfggg g 253 temperatures than conventional aluminum conductor.
  • (stren th) EXAMPLE 4 Quaternary alloys consisting of Fe-Re-Zr-Al in the r Aluminum conductor the proportion shown in Table 7 were made into wires of 2.9 inventivm (23) 21. 8 00. 3 +4. 8 mm. dra. by ordinary working methods to measure their 220 m8 +9.3 conductivity and tensile strength, and the results are or (ig) ?3-2 $2 shown in Table 7.
  • the rates of increase and decrease of 5005 'i i 0 5: 'Igfg tensile strength after heating at the predetermined temp Aldrey alloy conductor 5&2 perature for 2 hours are shown in Table 8.
  • the aluminum alloy of the invention maintains substantially the same tensile strength at 150 C. as at room temperature.
  • EXAMPLE 8 The alloys having composition shown in Table 15 were made into wires of 2.9 mm. dia. It is clearly shown in Table 15 that the workability for wire drawing and bendability decrease as Mg content and Re content increase.
  • the (ll-0.6% of magnesium, and the remainder of alumiresults are shown in Table 16. num.
  • loys have better heat resistance and electric conductivity than the conventional heat resistant aluminum alloys.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Conductive Materials (AREA)

Description

United States Patent 3,278,300 ALUMINUM ALLOYS FOR ELECTRIC CONDUCTORS Kichizo Koike, Kiyotaki, Nikko, Japan, assignor to The lFurukawa Electric Company Limited, Tolryo, Japan, a corporation of Japan N0 Drawing. Filed June 8, 1964, Ser. No. 373,559 Claims priority, application Japan, June 12, 1963, 38/311,424, 38/311,425, 38/321,426 4 Claims. (Cl. 75-138) This invention relates to improved aluminum alloys, more particularly to heat resistant aluminum alloy conductors and high strength heat resistant aluminum alloys for electric conductors.
Aluminum cable steel reinforced has been conventionally used for overhead power transmission lines: however, improved heat resistance and current carrying capacity of aluminum alloy conductors have long been required considering special transmission conditions such as bus conductors in heavy capacity power station, transmission lines having a load factor of 0.5 or less (single purpose transmission lines for connecting thermal power station and pumping-up power station), and for emergency transmission line for two circuits parallel operation in case of fault of a single circuit, etc. To meet the above requirements, various aluminum alloys for electric conductors have been studied, and an alloy including zirconium is disclosed in Japanese Patent No. 261,993. The heat resistance of Al-Zr alloys is improved as the Zr content is increased, on the other hand; the electric conductivity is reduced as zirconium increases, so that addition quantity of zirconium should be considerably limited in order to obtain an alloy having high electric conductivity and low ohmic loss. Within the said limitation, the heat resistance becomes very low, not adapted for the heat resistant conductive alloy conductors.
Aldrey alloys have been used for overhead power transmission as well as for aluminum cable steel reinforced; however, being a heat treated product, the said alloy needs a series of treatments in the process of manufacturing such as solution heat treatment-aging-wire drawing-aging, which make the alloy rather costly, and also, being an age hardening alloy, it has a disadvantage that the continuous operation temperature of the conductor cannot be made higher than that of an ordinary aluminum wire. As a non-heat treatable high strength aluminum alloy, Al-Mg alloys, for instance 5005 alloy, have been put into use; however, it being a solid solution type, it is difficult to increase its electric conductivity more than 55% when the tensile strength is not less than 25 kg/mm? To increase electric conductivity, magnesium content must be reduced at the sacrifice of mechanical properties such as tensile strength and fatigue strength.
In addition to the high heat resistance, conductivity, tensile strength, and low manufacturing cost, overhead transmission line conductor is required to have excellent sag-tension characteristics, vibration fatigue strength, creep characteristics, etc.
The principal object of the invention is to obviate the defects of the conventional conductors and to provide aluminum base alloys having increased electric conductivity and substantially equivalent heat resistance to that of the conventional heat resisting conductive alloys,
Another object of the invention is to provide aluminum alloys having high mechanical strength, high heat resistance and conductivity by improving the mechanical strength of conventional heat resistant aluminum alloy conductors.
A further object of the invention is to provide non-heat treatable aluminum alloys having excellent strength and high conductivity to be manufactured by the same process as ordinary aluminum conductors.
In order to attain the above objects, various researches were made on many multi-element alloys and the inventor has succeeded in obtaining aluminum alloys which have (1) high conductivity and heat resistance, or (2) high conductivity and heat resistance and substantially excellent mechanical strength, or (3) much higher conductivity than conventional heat resistant Al-alloys or high strength Al-alloys by adding to aluminum Misch metal having any composition of one or more of rare earth metals such as cerium or lanthanum (hereafter abridged as Re) and further a small amount of iron and also by adding to said aluminum-Re-iron alloy, a suitable quantity of zirconium or magnesium depending on the objects of use.
The essential ingredients of the alloys of the invention consist of (Ll-0.5% of iron, 06-30% of Re, and the remainder of aluminum. The reason for limiting the iron and Re contents to the above values in the invention is that for iron and Re contents of less than 0.1% and 0.6% respectively, heat resistance increase is not effective and that for iron content of more than 0.5%, heat resistance increase is saturated, which may possibly deteriorate electric conductivity and corrosion resistance.
The preferable composition of the alloys of the invention is 0.6l.5% of Re, 0.15-0.25 of iron and the remainder of aluminum.
To improve the heat resistance of said ternary conductive aluminum alloys of Al-Fe-Re, the effect of addition of quaternary element was thoroughly investigated, and it has been ascertained that the addition of a small quantity of zirconium is very effective. The alloy developed was composed of 06-30% of Re, (ll-0.5% of iron, 0.0 10.1% of zirconium and the remainder of aluminum. The reason for limiting the zirconium content of 0.0 1-0.1% is that at less than 0.01% of zirconium, heat resistance increase is not effective and that at more than 0.1%, the heat resistance increase is saturated while electric conductivity is reduced to less than 58% of I.A.C.S. and is unsuitable for conductor application.
The preferred composition of said alloy is 0.6-1.5% of Re, 0.150.25% of iron, 0.04-0.06% of zirconium and the remainder of aluminum.
The tensile strength of the aluminum conductor made of said alloys of the invention consisting of Al-Fe-Re or Al-Fe-Re-Zr is substantially the same as that of EC. grade aluminum (99.60 Al) conductor. As a result of further research to develop a high strength heat resistant aluminum alloy, the inventor has found that addition of a small quantity of magnesium to Al-Fe Re alloy increases the mechanical strength without impairing electric conductivity and heat resistance. That is, the alloy developed consists of 0.10.5% of iron, 0.63.0% of Re, 0.020.6% of magnesium and the remainder of aluminum. A magnesium content of 0.020.l% greatly improves the characteristics of heat resistant high strength aluminum alloy;
a magnesium content of 0.10.6% improves characteristics of high strength heat resistant conductive aluminum alloy. The alloys of the invention can be grouped into two categories, namely, an alloy consisting of 0.10.5% of iron, 0.63.0% of Re, 0.020.1% of magnesium and the remainder of aluminum, and an alloy consisting of 0.10.5% of iron, 06-30% of Re, 0.10.6% of magnesium and the remainder of aluminum.
When the Fe-Re-Mg-Al alloy wire is compared with the conventional 5005 wire and Aldrey alloy or 6201 wire, the alloy of the invention has about 35% higher electric conductivity than conventional ones for the same tensile strength, and has higher tensile strength for the same electric conductivity.
Tensile Electric strength conductivity (kg/mm?) (I.A.C.S.,
percent) Conductor of the alloy of the invention- G3 5005 alloy conductor 24 55 Aldrey alloy conductor-.. 32
To the aluminum base metal of 99.99% purity, 0.01% and 0.25% of iron were added, and, to each mixture, 024.0% of Re was added. Cast 4 X 4.5 wire bars of the composition indicated in Table 4 were hot rolled to 13 mm. dia. redrawn rod and were drawn into 4.0 mm. dia. wire by ordinary working methods, and the tensile strength was measured after heating it at 150 C. for 1 hour. The rate of increase and decrease of the tensile strength was compared with the value measured at the beginning of the test. The results are shown in Table 1.
No'rE.Rc used had the following composition:
Cerium 45% Lanthanum 35% Neodymium... 15% 93% Praseody1niun1 4% Samarium Remainder Iron- 5% Magnesium, Silic 2% As seen from the above table, the anti-softening characteristic on heating is greatly improved by adding a little amount of iron, and, for Re content of more than 0.6%, the alloy is hardened by heating. The lower limits of iron and Re were, therefore, taken as 0.1% and 0.6% respectively.
4- EXAMPLE 2 By the use of alloys having a composition shown in Table 2, Wires were produced through the process of casting-rolling-% wire rod-wire drawing-2.9 mm. dia. The conductivity and tensile strength of drawn wires are shown in Table 3.
The above samples were further subjected to heating at C., C., C., C., and 220 C., for 2 hours each, and then the tensile strengths were measured to obtain the rate of increase and decrease. The results are shown in Table 4.
Table 4 100 0. 130 0. 160 C. i 190 C. I 220 C.
Pcrcent Percent Percent Percent Percent Judging from Tables 3 and 4, the hardening characteristic on annealing increases as the Re content increases, and, for the same Re content, Fe 0.5% has less hardening than Fe 0.25%. In case the conductivity is higher than 58% I.A.C.S., the upper limits for the iron and Re contents are limited to 0.5% and 3.0% respectively.
It seems that the alloy of the invention being hardened by heating instead of softening is due not to simple precipitation hardening but to a particular phenomenon related to the reciprocal action between solute foreign atoms and dislocations caused by cold working.
EXAMPLE 3 Alloys having the composition of Table 5 were made into wires of 3.2 mm. dia. to compare their characteristics with those of conductor grade aluminum wire with regard to conductivity, tensile strength, anti-softening characteristic on heating, and creep characteristic; the results are shown in Table 6.
Table It is apparent from comparison of Table 4 and the above tables that the anti-softening characteristic after Fe Si Re A1 heating of Al-Fe-Re alloy is greatly improved by adding Name otalloy (pcr- (per- (pcr- (percent) a small quantity of zirconium, and the effects are parcem) cont) cent) 5 ticularly remarkable in the high temperature zone.
Aluminum alloy wire of the EXAMPLE 5 mventlon' 0 6 R m The quaternary alloys consisting of Fe-Re-Zr-Al in the naindcr.
2.0 Do. proportion shown 1n Table 9 were made into wires of 3.0 Do. Conductor grade alum 10 2.9 mm. dra. to measure the tensile strength and con wire 0.18 0.08 Do. ductivity at room temperature and to determine the rate of increase and decrease in tensile strength by measuring Table 6 Electric Tensile Rate of Creep Name of Alloy conducstrength increase and charactivity (kg/mm?) decrease teristic (percent) (percent) (percent) Aluminum alloy wire of the invention:
01. s 18. 2 +1.1 0. 04 60.2 19. 8 +3. 5 0. 021 (16 5s. 5 21. 0 +13. 0 0. 012 Conductor grade aluminum wire"-.. 62. 4 17. 9 +6. 2 0. 074
The rate of increase and decrease is expressed in terms tensile strength after heating them at 120 C. for days of a ratio of the tensile strength after the wire is heated and by measuring the same strength after cooling them at C. for 500 hours to the tensile strength at room down to room temperature. The results are shown in temperature before heating. The creep characteristic is Table 10.
Table 9 Zr Re Fe Si Mg Name f alloy (per- (per- (per- (per- (per- Al (percent) cent) cent) cent) cent) cent) Aluminum alloy conductor of the invention:
(23) 0. 02 0. 7 Remainder.
0.04 0.7 Do. 5 0. 05 2.0 Do. Ordinaryaluminum conducton. Do. 5005 alloy conductor Do. Aldrey alloy conductor Do.
a strain after the wire is subjected to a stress of 27 Table 10 kg./mm. and heating at 110 C. for 100 hours.
It is clear from the above table that the aluminum alloy conductor of the invention has a higher conductivity Electric and a better anti-softening characteristic after heating for 5 Tensile conducand delong time, and more excellent creep characteristics at high Name 01 figfggg g 253 temperatures than conventional aluminum conductor. (stren th) EXAMPLE 4 Quaternary alloys consisting of Fe-Re-Zr-Al in the r Aluminum conductor the proportion shown in Table 7 were made into wires of 2.9 inventivm (23) 21. 8 00. 3 +4. 8 mm. dra. by ordinary working methods to measure their 220 m8 +9.3 conductivity and tensile strength, and the results are or (ig) ?3-2 $2 shown in Table 7. The rates of increase and decrease of 5005 'i i 0 5: 'Igfg tensile strength after heating at the predetermined temp Aldrey alloy conductor 5&2 perature for 2 hours are shown in Table 8.
Table 7 Electric Fe Re Zr conduc- Tensile (per- (pcr- (per- Al (percent) tivity strength cent) cent) cent) (I.A.C.S., (kg/mm?) percent) Table 8 It is apparent from the above tables that the conductivity and heat resistance of the quaternary Fe-Re-Zr-Al 100C C, 4 C. C. l 220C- alloy are greatly improved compared with conventional 70 heat resisting aluminum alloys (5005 alloy and Aldrey Percent Pefielntz Page? P35321251 Percent3 ll 5. 17.2 +123 16 9a EXAMPLE 6 77 +151 .70 .5 its +104 +8.11 1.1 -1e.9 The aluminum alloy conductors of the invention conga: 3 313;; 75 sisting of Mg-Fe-Re-Al in the proportion shown in Table 1 1 were compared with the conventional 5005 alloy con- 7 ductor (both in 2.9 mm. dia. wire form) with respect to tensile strength and electric conductivity. The results are shown in Table 11.
It is apparent from the the above table that the aluminum alloy of the invention maintains substantially the same tensile strength at 150 C. as at room temperature.
It is clearly shown in the above tables that the tensile strengths of the 5005 alloy and the alloys of the invention are substantially the same but that the electric conductivity of the latter alloys is far better than that of the former.
The rates of tensile strength decrease for the above aluminum alloy conductor of the invention, Aldrey alloy EXAMPLE 7 The alloys having composition shown in Table 14 were cast into 4" x 4.5" wire bars which were hot rolled by a rod mill into bars and then redrawn into 2.9 mm. dia. wires to measure their tensile strength and electric conductivity at room temperature. The results are shown in Table 14.
Table 14 Mg Re Fe Tensile Electric (per- (per- (per- Al (percent) strength conduccent) cent) cent) (kg/mm?) tivity (percent) 0. 2 0. 15 Remainder 24. 4 60. 7 0.2 0.6 0.15 .do 25.8 59.3 0. 2 1. 26. 8 58. 8 0. 2 2. 0 28. 7 57. 3 0. 4 25. 8 57. 8 0. 4 0. 6 28. 2 56. 7 0. 4 1. U 29. 56. 2 0. 4 2. 0 31. 7 55. 0 0. 6 l 27. 4 54. 0 0. 6 0 6 20. 4 54. 4 0.6 1. 0 30. 5 54. 1 0.6 2. 0 32. 5 52. 5
conductor, and 5005 alloy conductor were measured after heating them at 120 C. The results are shown in Table Besides, the above aluminum alloy conductor of the invention consisting of said quaternary elements having diameter of 2.9 mm. was compared with a conventional heat resistant aluminum conductor by measuring their tensile strength after heating at 150 C. for minutes. The results are shown in Table 13.
It is apparent from the above table that the Work hardening effect of Al-Mg alloys increases as Re content increases and the tensile strength increases 3-3.5 kg./rnrn. per Re 1% independent of the Mg content in the alloy prior to the addition. The electric conductivity decreases in direct proportion to Re content in the alloy, but the rate of decrease is as small as l.11.4% I.A.C.S. In other words, in Al-Re-Fe-Mg alloy, the tensile strength can be improved by 2.2 kg./mm. at the loss of conductivity of 0.8%, while, in Al-Mg alloy, tensile strength improvement of 1.4-1.6 kg/mm. is accompanied with the loss of conductivity by 24-29%. Thus, the alloy of the invention improves mechanical strength and electric conductivity greatly.
EXAMPLE 8 The alloys having composition shown in Table 15 were made into wires of 2.9 mm. dia. It is clearly shown in Table 15 that the workability for wire drawing and bendability decrease as Mg content and Re content increase.
Table 13 Tensile Rate of Mg Re Fe Zr strength increase Name of alloy (per- (per- (per- (per- A1 (percent) at room and decent) cent) cent) cent) temp. crease (kg/mm?) (percent) Hgat resistant aluminum eon- 0.15 0. 1 Remainder 18 21 uctor. Aluminum conductor of the in- 0.05 0. 6 0.25 do 23 +1.
vention (28). 8
9 10 Table 15 Besides, by adding 0.02-0.1% of magnesium to the Fe-Re-Al alloys, the mechanical strength, heat resistance Mg Re Fe Bending and electric conductivity thereof are greatly improved. w s g g ga A1 (p g g Besides, the addition of 0.1-0. 6% of magnesium to the n Fe-Re-Al alloys has great effect of considerably increasing the mechanical strength of the original alloys without 8% g 8; Remainder": i B affecting the electric conductivity.
g g What I claim is: 3 3 D 1. Heat resistant aluminum alloy for electric conducg; i 8. 1 3g tor consisting of 0.1-0.5%, preferably 0.15-0.2570, of 4 20 D iron, 06-30%, preferably 06-15%, of Misch metal, 0.8 4 0. 25 50 D and the remainder of aluminum.
2. Heat resistant aluminum alloy for electric conduc- Here, D Stands for the diameter of the wire, and the tor conslsting of 0.1-0.5%, preferably 0.15 O.25%, of l iron, (LG-3.0%, preferably 0.6-1.5%, of Misch metal, larger the rnultlple is, the smaller the bendabihty.
-0.0l-0.1%, preferably 0.040.06%, of zirconium, and Accordingly, the additions of Mg and Re are limited the remainder of aluminum 3 i g g m g i the angle of Wire 3. High strength heat resistant aluminum alloy for rawmg Wor a an en a electric conductor consisting of (ll-0.5%, preferably 0.15-0.25% of iron 0.6-3.0% preferably 0.61.5% of s EXAMPLE 9 Misch metal, 0.02-0.1%, preferably 0.04 0.os%, of The quaternary alloys of Mg-Re-Fe-Al having commagnesium, and the remainder of aluminum. position shown in Table 16 were compared with the 4. High strength aluminum alloy for electric conducconventional Aldrey alloy with regard to tensile strength, tor consisting of 0.1O.5%, preferably 0.150.25%, of electric conductivity and the rate of decrease in tensile iron, 06-30%, preferably 06-15%, of Misch metal, strength after heating at 120 C. for 1,000 hours. The (ll-0.6% of magnesium, and the remainder of alumiresults are shown in Table 16. num.
Table 16 Mg Re Fe Si Tensile Electric Rate of Name of alloy (per (per- (per- (perstrength conducdecrease cent) cent) cent) cent) (kg/mm?) tivity (percent) (percent) Aldrey alloy T 0.5 0.15 0.5 33 52 23 It will be apparent from the above table that the alu- References Cited by the Examiner minum alloy of the invention has very high electric conductivity and anti-softening characteristic compared with UNITED STATES PATENTS the publicly known heat resistant aluminum alloy. 3,063,832 11/1962 Snyder 75-138 Of the aluminum alloys of the invention s expl ln 3,113,991 12/1963 Kleber 75-147 above in detail, the ternary Fe-Re-Al all ys hav better 3,199,979 8/1965 Martin 75 147 electric conductivity, tensile strength, anti-softening char- 3,241,953 3 /1966 Pryor et aL 75 138 acteristic and creep characteristic than the ordinary aluminum conductor, while the quaternary Fe-Re-Zr-Al al- D AVID L RECK, Primary Examiner.
loys have better heat resistance and electric conductivity than the conventional heat resistant aluminum alloys.
R. O. DEAN, Assistant Examiner.

Claims (1)

1. HEAT RESISTANT ALUMINUM ALLOY FOR ELECTRIC CONDUCTOR CONSISTING OF 0.1-0.5%, PREFERABLY 0.15-0.25%, OF IRON, 0.6-3.0% PREFERABLY 0.6-1.5%, OF MISCH METAL, AND THE REMAINDER O ALUMINUM.
US373559A 1963-06-12 1964-06-08 Aluminum alloys for electric conductors Expired - Lifetime US3278300A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP3142463 1963-06-12

Publications (1)

Publication Number Publication Date
US3278300A true US3278300A (en) 1966-10-11

Family

ID=12330847

Family Applications (1)

Application Number Title Priority Date Filing Date
US373559A Expired - Lifetime US3278300A (en) 1963-06-12 1964-06-08 Aluminum alloys for electric conductors

Country Status (1)

Country Link
US (1) US3278300A (en)

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3375102A (en) * 1965-04-09 1968-03-26 Kawecki Chemical Company Prevention of magnesium burn-out in aluminum-magnesium alloys
US3383188A (en) * 1965-09-27 1968-05-14 Olin Mathieson Aluminum conductors
US3670401A (en) * 1970-04-01 1972-06-20 Southwire Co Method of fabricating aluminum alloy rod
JPS4831449B1 (en) * 1968-04-29 1973-09-29
USRE28419E (en) * 1968-05-21 1975-05-13 Table iv
US3960606A (en) * 1975-03-12 1976-06-01 Southwire Company Aluminum silicon alloy and method of preparation thereof
US3964935A (en) * 1972-04-03 1976-06-22 Southwire Company Aluminum-cerium-iron electrical conductor and method for making same
US4121951A (en) * 1976-03-05 1978-10-24 Alcan Research And Development Limited Aluminum alloy electrical conductor and method therefor
FR2428079A1 (en) * 1978-06-05 1980-01-04 Alusuisse IMPROVEMENT OF THE ELECTRICAL CONDUCTIBILITY OF ALUMINUM ALLOYS BY THE ADDITION OF MISCHMETAL
USRE30465E (en) * 1974-09-23 1980-12-30 Southwire Company Aluminum alloy wire
US4787943A (en) * 1987-04-30 1988-11-29 The United States Of America As Represented By The Secretary Of The Air Force Dispersion strengthened aluminum-base alloy
EP0997546A1 (en) * 1998-10-30 2000-05-03 Sumitomo Electric Industries, Ltd. Aluminum alloy and method for manufacturing aluminum-alloy member
US9440272B1 (en) * 2011-02-07 2016-09-13 Southwire Company, Llc Method for producing aluminum rod and aluminum wire

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3063832A (en) * 1960-07-05 1962-11-13 Anaconda Wire & Cable Co High conductivity tin-bearing aluminum alloy
US3113991A (en) * 1959-08-18 1963-12-10 Nuclear Corp Of America Method of tagging bulk materials
US3199979A (en) * 1961-10-27 1965-08-10 William F Jobbins Inc Aluminum base casting alloys and method
US3241953A (en) * 1963-10-03 1966-03-22 Olin Mathieson Aluminum conductor and process for obtaining same

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3113991A (en) * 1959-08-18 1963-12-10 Nuclear Corp Of America Method of tagging bulk materials
US3063832A (en) * 1960-07-05 1962-11-13 Anaconda Wire & Cable Co High conductivity tin-bearing aluminum alloy
US3199979A (en) * 1961-10-27 1965-08-10 William F Jobbins Inc Aluminum base casting alloys and method
US3241953A (en) * 1963-10-03 1966-03-22 Olin Mathieson Aluminum conductor and process for obtaining same

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3375102A (en) * 1965-04-09 1968-03-26 Kawecki Chemical Company Prevention of magnesium burn-out in aluminum-magnesium alloys
US3383188A (en) * 1965-09-27 1968-05-14 Olin Mathieson Aluminum conductors
JPS4831449B1 (en) * 1968-04-29 1973-09-29
USRE28419E (en) * 1968-05-21 1975-05-13 Table iv
US3670401A (en) * 1970-04-01 1972-06-20 Southwire Co Method of fabricating aluminum alloy rod
US3964935A (en) * 1972-04-03 1976-06-22 Southwire Company Aluminum-cerium-iron electrical conductor and method for making same
USRE30465E (en) * 1974-09-23 1980-12-30 Southwire Company Aluminum alloy wire
US3960606A (en) * 1975-03-12 1976-06-01 Southwire Company Aluminum silicon alloy and method of preparation thereof
US4121951A (en) * 1976-03-05 1978-10-24 Alcan Research And Development Limited Aluminum alloy electrical conductor and method therefor
FR2428079A1 (en) * 1978-06-05 1980-01-04 Alusuisse IMPROVEMENT OF THE ELECTRICAL CONDUCTIBILITY OF ALUMINUM ALLOYS BY THE ADDITION OF MISCHMETAL
US4213799A (en) * 1978-06-05 1980-07-22 Swiss Aluminium Ltd. Improving the electrical conductivity of aluminum alloys through the addition of mischmetal
US4787943A (en) * 1987-04-30 1988-11-29 The United States Of America As Represented By The Secretary Of The Air Force Dispersion strengthened aluminum-base alloy
EP0997546A1 (en) * 1998-10-30 2000-05-03 Sumitomo Electric Industries, Ltd. Aluminum alloy and method for manufacturing aluminum-alloy member
US6402860B2 (en) 1998-10-30 2002-06-11 Sumitomo Electric Industries, Ltd. Aluminum alloy and method for manufacturing aluminum-alloy member
US9440272B1 (en) * 2011-02-07 2016-09-13 Southwire Company, Llc Method for producing aluminum rod and aluminum wire
US10518304B2 (en) 2011-02-07 2019-12-31 Southwire Company, Llc Method for producing aluminum rod and aluminum wire

Similar Documents

Publication Publication Date Title
US3063832A (en) High conductivity tin-bearing aluminum alloy
US3278300A (en) Aluminum alloys for electric conductors
US4182640A (en) Aluminum alloy electric conductor wire
JPS633936B2 (en)
GB1076685A (en) Improvements in or relating to electric power conductors
US5045131A (en) Contact conductor for electric vehicles
US2572562A (en) Aluminum alloy
US4233066A (en) Electrical conductor of aluminium
JPS6216269B2 (en)
US3694195A (en) Heat-resistant aluminum alloys for electric conductors
US3763686A (en) Process for obtaining aluminum alloy conductor
US4213800A (en) Electrical conductivity of aluminum alloys through the addition of yttrium
JPS6328971B2 (en)
US4213799A (en) Improving the electrical conductivity of aluminum alloys through the addition of mischmetal
US3359141A (en) Electrical conductors of aluminum and methods for production of same
US3711339A (en) Aluminum alloy conductor
US2286734A (en) Copper-cobalt-tin alloy
US1991162A (en) Process for improving coppertitanium alloys
US3959027A (en) Method of manufacturing aluminum alloy electric conductors
JPS5828340B2 (en) Aluminum alloy for conductive use
US3823041A (en) Treatment of aluminum alloys
CA1041797A (en) Aluminum alloy for electric conductors and its method of manufacture
JPH0432146B2 (en)
JPS634893B2 (en)
JPS5828339B2 (en) Conductive aluminum alloy