Process of manufacturing solid bodies of copper-zinc-aluminium alloys

Claim 2

A process of preparing solid bodies of copper-zinc-aluminum alloys having a β-crystal structure and a fatigue resistance of at least 100,000 cycles for a psuedo-elastic elongation of 0.8 to 1% under a maximum bending load of 250 MN/m 2 , which comprises the steps of providing a pulverulent material which consists essentially of unavoidable impurities, 10-40% by weight of Zn, 1-12% by weight of Al and the balance of Cu, cold compacting this pulverulent material and subsequently hot extruding it to form a solid body.

Claim 3

The process of claim 1 wherein said pulverulent material consists essentially of a minor portion of unavoidable impurities, 24-32% by weight of Zn, 1-6% by weight of Al and the balance of Cu.

Claim 4

The process of claim 1 wherein said pulverulent material consists essentially of a minor portion of impurities, 18-24% by weight of Zn, 4-8% by weight of Al and the balance of Cu.

Claim 5

The process of claim 1 wherein said pulverulent material consists essentially of a minor portion of unavoidable impurities, 10-18% by weight of Zn, 7-12% by weight of Al and the balance of Cu.

Claim 6

The process of any one of claims 1-4, characterised in that said pulverulent starting material has been obtained by melting the elements Zn, Al and Cu together in a desired ratio, followed by atomization of the resulting molten alloy with the aid of a fluid jet.

Claim 7

The process of claim 1, characterised in that the cold compacting step is followed by a hot compacting step prior to extrusion.

Claim 8

The process of claim 6, characterised by effecting the hot compacting step at 500°-600° C.

Claim 9

The process of claim 1, characterised by effecting the extrusion at 700°-800° C.

Claim 10

The process of claim 1, characterised in that the extruded body is cooled to room temperature by quenching with a cold liquid.

Claim 11

The process of claim 1, characterised in that the extruded body, is converted to an end product of desired shape and dimensions by means of a mechanical deformation step.

Claim 12

A product of any one of claims 1 to 4 having β-crystal structure.

Claim 13

A product according to claim 11, characterised by having a grain structure with grain sizes between 20-30 μm.

Claim 14

A copper-zinc-aluminum alloy article having a predominantly β-crystal structure, an average grain size of down to about 20-30 μm and a fatigue resistance of at least 100,000 cycles for a psuedo-elastic elongation of 0.8 to 1% under a maximum bending load of 250 MN/m 2 , and which is suitable for direct use and as an intermediate for further mechanical deformation to an end product having an average grain size not exceeding about 200 μm; said article being made by a process which comprises: (a) mixing pulverulent material selected from the group consisting of elemental powders and/or alloy powders, said alloy article consisting essentially of 10-40% by weight of Zn, 1-12% by weight of Al, less than 0.2% by weight of oxygen and the balance of Cu, (b) cold compacting said mixture to form a self supporting mass, (c) heating said mass to a temperature of at least 700° C. and (d) hot extruding said mass at an extrusion ratio of at least about 32 to yield said alloy article.

Claim 15

A copper-zinc-aluminum alloy article having a predominantly β-crystal structure, an average grain size of down to about 20-30 μm and a fatigue resistance of at least 100,000 cycles for a psuedo-elastic elongation of 0.8 to 1% under a maximum bending load of 250 MN/m 2 , and which is suitable for direct use and as an intermediate for further mechanical deformation to an end product having an average grain size not exceeding about 200 μm; said article being made by a process which comprises: (a) mixing pulverulent material selected from the group consisting of elemental powders and/or alloy powders, said alloy article consisting essentially of 10-40% by weight of Zn, 1-12% by weight of Al, less than 0.2% by weight of oxygen and the balance of Cu, (b) cold compacting said mixture to form a self supporting mass, (c) heating said mass to a temperature of at least 700° C. and (d) hot extruding said mass at an extrusion ratio of at least about 32 to yield said alloy article.

Claim 16

Alloy article according to claim 13, consisting essentially of 24-32% by weight of Zn, 1-6% by weight of Al, less than 0.2% by weight of oxygen and the balance of Cu.

Claim 17

Alloy article according to claim 13, consisting essentially of 18-24% by weight of Zn, 4-8% by weight of Al, less than 0.2% by weight of oxygen and the balance of Cu.

Claim 18

Alloy article according to claim 13, consisting essentially of 10-18% by weight of Zn, 7-12% by weight of Al, less than 0.2% by weight of oxygen and the balance of Cu.

Claim 19

Alloy article according to claim 13, wherein the alloy powders have been obtained by melting the elements Zn, Al and Cu in a desired ratio, followed by atomization of the resulting molten alloy with the aid of a fluid jet.

Claim 20

Alloy article according to claim 13, wherein the cold compacting step is followed by a hot compacting step prior to extrusion.

Claim 21

Alloy article according to claim 18, wherein the hot compacting step is effected at a temperature of at least 500° C.

Claim 22

Alloy article according to claim 13, wherein the extruded mass is cooled to room temperature by quenching with a cold liquid.

Claim 23

The alloy article of claim 13 having an average grain size not exceeding about 200 μm obtained by mechanical deformation treatment.

Claim 26

The method as defined in claim 22 including, subsequent to step (b) and prior to step (c), the step of heating said coherent mass and compacting the same while so heated.

Claim 27

The method as defined in claim 22 wherein the compaction of step (b) is effected at a pressure of about 1000 MN/m 2 .

Claim 28

The method as defined in claim 23 wherein the compaction of step (b) is effected at a pressure of about 430 MN/m 2 .

Claim 29

The method as defined in claim 24 wherein the extrusion ratio is about 71.5.

Claim 30

The method as defined in claim 25 wherein the extrusion ratio of step (c) is about 32.2.