Difference between revisions of "Precipitation Hardening Copper Alloys"

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The cause for precipitation hardening of CuBe materials is the rapidly diminishing solubility of beryllium in copper as temperature decrease. As the
 
The cause for precipitation hardening of CuBe materials is the rapidly diminishing solubility of beryllium in copper as temperature decrease. As the
phase diagram for CuBe shows, 2.4 wt% of Be are soluble in Cu at 780°C ''(Fig. 5.28)''. In this temperature range annealed CuBe alloys are homogeneous(solution annealing). The homogeneous state can be frozen through rapid cooling to room temperature (quenching). Through a subsequent annealing at 325°C the desired precipitation hardening is achieved which results in a significant increase in mechanical strength and electrical conductivity of CuBe ''(Table 5.17)''. The final strength and hardness values depend on the annealing temperature and time as well as on the initial degree of cold working ''(Table 5.18)'' and ''(Figs. 5.29 - 5.31)''.
+
phase diagram for CuBe shows, 2.4 wt% of Be are soluble in Cu at 780°C <xr id="fig:Phase diagram of copperberyllium with temperature ranges for brazing and annealing treatments"/> (Fig. 5.28). In this temperature range annealed CuBe alloys are homogeneous(solution annealing). The homogeneous state can be frozen through rapid cooling to room temperature (quenching). Through a subsequent annealing at 325°C the desired precipitation hardening is achieved which results in a significant increase in mechanical strength and electrical conductivity of CuBe ''(Table 5.17)''. The final strength and hardness values depend on the annealing temperature and time as well as on the initial degree of cold working ''(Table 5.18)'' and [[#figures7|(Figs. 43 – 75)]](Figs. 5.29 - 5.31).
  
Fig. 5.28:
+
<figure id="fig:Phase diagram of copperberyllium with temperature ranges for brazing and annealing treatments">
Phase diagram of copperberyllium
+
Fig. 5.28: Phase diagram of copperberyllium with temperature ranges for brazing and annealing treatments
with temperature ranges for
+
[[File:Phase diagram of copper beryllium with temperature ranges.jpg|right|thumb|Phase diagram of copper- beryllium with temperature ranges for brazing and annealing treatments]]
brazing and annealing treatments
+
</figure>
  
 
As precipitation hardening alloys CuBe materials, mainly CuBe2 and CuBe1.7 have gained broad usage as current carrying contact springs because of their outstanding mechanical properties. Besides these CuCo2Be and CuNi2Be, which have medium mechanical strength and a relatively high electrical
 
As precipitation hardening alloys CuBe materials, mainly CuBe2 and CuBe1.7 have gained broad usage as current carrying contact springs because of their outstanding mechanical properties. Besides these CuCo2Be and CuNi2Be, which have medium mechanical strength and a relatively high electrical
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Since Beryllium is rated as a carcinogen by the European regulation EU-67/548, it has been tried to reach the application properties of the well established CuBe1.7 and CuBe2 alloys with a lower Be content. The development efforts for alternate precipitation hardening materials without toxic and declaration requiring additive materials, for example CuNiCoSi, are aimed at the replacement of CuBe.
 
Since Beryllium is rated as a carcinogen by the European regulation EU-67/548, it has been tried to reach the application properties of the well established CuBe1.7 and CuBe2 alloys with a lower Be content. The development efforts for alternate precipitation hardening materials without toxic and declaration requiring additive materials, for example CuNiCoSi, are aimed at the replacement of CuBe.
  
Fig. 5.29:
+
<div id="figures7">
Precipitation hardening
+
<xr id="fig:Precipitation hardening of CuBe2 at 325°C after different cold working"/> Fig. 5.29: Precipitation hardening of CuBe2 at 325°C after different cold working
of CuBe2 at 325°C after
 
different cold working
 
  
Fig. 5.30:
+
<xr id="fig:Precipitation hardening of CuBe2 (soft) at 325°C"/> Fig. 5.30: Precipitation hardening of CuBe2 (soft) at 325°C
Precipitation
 
hardening of CuBe2
 
(soft) at 325°C
 
  
Fig. 5.31:
+
<xr id="fig:Precipitation hardening of CuBe2 (half hard) at different annealing temperatures"/> Fig. 5.31: Precipitation hardening of CuBe2 (half hard) at different annealing temperatures
Precipitation
+
</div>
hardening of CuBe2
 
(half hard) at different
 
annealing temperatures
 
  
Table 5.17: Physical Properties of Selected Copper-Beryllium Alloys (2 Teile!)
+
<div class="multiple-images">
 +
<figure id="fig:Precipitation hardening of CuBe2 at 325°C after different cold working">
 +
[[File:Precipitation hardening of CuBe2 at 325C.jpg|right|thumb|Precipitation hardening of CuBe2 at 325°C after different cold working]]
 +
</figure>
  
Table 5.18: Mechanical Properties of Selected Copper-Beryllium Alloys (2 Teile!)
+
<figure id="fig:Precipitation hardening of CuBe2 (soft) at 325°C">
 +
[[File:Precipitation hardening of CuBe2 (soft) at 325C.jpg|right|thumb|Precipitation hardening of CuBe2 (soft) at 325°C]]
 +
</figure>
 +
 
 +
<figure id="fig:Precipitation hardening of CuBe2 (half hard) at different annealing temperatures">
 +
[[File:Precipitation hardening of CuBe2 half hard.jpg|right|thumb|Precipitation hardening of CuBe2 (half hard) at different annealing temperatures]]
 +
</figure>
 +
</div>
 +
<div class="clear"></div>
 +
 
 +
'''Table 5.17: Physical Properties of Selected Copper-Beryllium Alloys''' (2 Teile!)
 +
 
 +
'''Table 5.18: Mechanical Properties of Selected Copper-Beryllium Alloys''' (2 Teile!)
  
 
====5.1.6.2 Other Precipitation Hardening Copper Alloys====
 
====5.1.6.2 Other Precipitation Hardening Copper Alloys====
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=====5.1.6.2.1 Copper-Chromium Alloys=====
 
=====5.1.6.2.1 Copper-Chromium Alloys=====
  
As the phase diagram shows, copper-chromium has a similar hardening profile compared to CuBe ''(Fig. 5.32)''. In the hardened stage CuCr has limitations to work hardening. Compared to copper it has a better temperature stability with good electrical conductivity. Hardness and electrical conductivity as a function of cold working and precipitation hardening conditions are illustrated in Figs. 5.33-5.35 ''(Tables 5.19 and 5.20)''.
+
As the phase diagram shows, copper-chromium has a similar hardening profile compared to CuBe <xr id="fig:Copper corner of the copper-chromium phase diagram for up to 0.8 wt% chromium"/>(Fig. 5.32). In the hardened stage CuCr has limitations to work hardening. Compared to copper it has a better temperature stability with good electrical conductivity. Hardness and electrical conductivity as a function of cold working and precipitation hardening conditions are illustrated in Figs. 5.33-5.35 ''(Tables 5.19 and 5.20)''.
  
 
Copper-chromium materials are especially suitable for use as electrodes for resistance welding. During brazing the loss in hardness is limited if low melting brazing alloys and reasonably short heating times are used.
 
Copper-chromium materials are especially suitable for use as electrodes for resistance welding. During brazing the loss in hardness is limited if low melting brazing alloys and reasonably short heating times are used.
  
Fig. 5.32:
+
<figure id="fig:Copper corner of the copper-chromium phase diagram for up to 0.8 wt% chromium">
Copper corner of the copper-chromium
+
Fig. 5.32: Copper corner of the copper-chromium phase diagram for up to 0.8 wt% chromium
phase diagram for up to 0.8 wt% chromium
+
[[File:Copper corner of the copper chromium phase diagram.jpg|right|thumb|Copper corner of the copper-chromium phase diagram for up to 0.8 wt% chromium]]
 +
</figure>
  
Fig. 5.33:
+
Fig. 5.33: Softening of precipitation-hardened and subsequently cold worked CuCr1 after 4hrs annealing
Softening of precipitation-hardened
+
[[File:Softening of precipitation hardened and subsequently cold worked CuCr1.jpg|right|thumb|Softening of precipitation-hardened and subsequently cold worked CuCr1 after 4hrs annealing]]
and subsequently cold
 
worked CuCr1 after
 
4hrs annealing
 
  
Fig. 5.34 a:
+
Fig. 5.34 a: Electrical conductivity of precipitation hardened CuCr 0.6 as a function of annealing conditions
Electrical conductivity of
+
[[File:Electrical conductivity of precipitation hardened CuCr 0.6.jpg|right|thumb|Electrical conductivity of precipitation hardened CuCr 0.6 as a function of annealing conditions]]
precipitation hardened
 
CuCr 0.6 as a function of
 
annealing conditions
 
  
Fig. 5.34 b:
+
Fig. 5.34 b: Hardness of precipitation hardened CuCr 0.6 as a function of annealing conditions
Hardness of
+
[[File:Hardness of precipitation hardened CuCr 0.6.jpg|right|thumb|Hardness of precipitation hardened CuCr 0.6 as a function of annealing conditions]]
precipitation hardened
 
CuCr 0.6 as a function
 
of annealing conditions
 
  
Fig. 5.35:
+
Fig. 5.35: Electrical conductivity and hardness of precipitation hardened CuCr 0.6 after cold working
Electrical conductivity
+
[[File:Electrical conductivity and hardness of precipitation hardened CuCr 0.6.jpg|right|thumb|Electrical conductivity and hardness of precipitation hardened CuCr 0.6 after cold working]]
and hardness of precipitation
 
hardened CuCr 0.6 after
 
cold working
 
  
Table 5.19: Physical Properties of Other Precipitation Hardening Copper Alloys (2 Teile!)
+
'''Table 5.19: Physical Properties of Other Precipitation Hardening Copper Alloys''' (2 Teile!)
  
Table 5.20: Mechanical Properties of Other Precipitation Hardening Copper Alloys
+
'''Table 5.20: Mechanical Properties of Other Precipitation Hardening Copper Alloys'''
  
 +
<table border="1" cellspacing="0" style="border-collapse:collapse"><tr><td><p class="s16">Material</p></td><td><p class="s16">Hardness</p><p class="s16">Condi- tion</p></td><td><p class="s16">Tensile</p><p class="s16">Strength R<span class="s18">m</span></p><p class="s16">[MPa]</p></td><td><p class="s16">0,2% Yield</p><p class="s16">Strength R<span class="s18">p02</span></p><p class="s16">[MPa]</p></td><td><p class="s16">Elongation</p><p class="s16">A50</p><p class="s16">[%]</p></td><td><p class="s16">Vickers</p><p class="s16">Hardness</p><p class="s16">HV</p></td><td><p class="s16">Spring Bending</p><p class="s16">Limit <span class="s19">F</span><span class="s18">FB </span>[MPa]</p></td></tr><tr><td><p class="s16">CuCr</p></td><td><p class="s16">R 230<span class="s18">a</span></p><p class="s16">R 400<span class="s18">a </span>R 450<span class="s18">b </span>R 550<span class="s18">b</span></p></td><td><p class="s33">&gt;<span class="s16"> 230</span></p><p class="s33">&gt;<span class="s16"> 400</span></p><p class="s33">&gt;<span class="s16"> 450</span></p><p class="s33">&gt;<span class="s16"> 550</span></p></td><td><p class="s33">&gt;<span class="s16"> 80</span></p><p class="s33">&gt;<span class="s16"> 295</span></p><p class="s33">&gt;<span class="s16"> 325</span></p><p class="s33">&gt;<span class="s16"> 440</span></p></td><td><p class="s16">30</p><p class="s16">10</p><p class="s16">10</p><p class="s16">8</p></td><td><p class="s33">&gt;<span class="s16"> 55</span></p><p class="s33">&gt;<span class="s16"> 120</span></p><p class="s33">&gt;<span class="s16"> 130</span></p><p class="s33">&gt;<span class="s16"> 150</span></p></td><td><p class="s16">350</p></td></tr><tr><td><p class="s16">CuZr</p></td><td><p class="s16">R 260<span class="s18">a</span></p><p class="s16">R 370<span class="s18">a </span>R 400<span class="s18">b </span>R 420<span class="s18">b</span></p></td><td><p class="s33">&gt;<span class="s16"> 260</span></p><p class="s33">&gt;<span class="s16"> 370</span></p><p class="s33">&gt;<span class="s16"> 400</span></p><p class="s33">&gt;<span class="s16"> 420</span></p></td><td><p class="s33">&gt;<span class="s16"> 100</span></p><p class="s33">&gt;<span class="s16"> 270</span></p><p class="s33">&gt;<span class="s16"> 280</span></p><p class="s33">&gt;<span class="s16"> 400</span></p></td><td><p class="s16">35</p><p class="s16">12</p><p class="s16">12</p><p class="s16">10</p></td><td><p class="s33">&gt;<span class="s16"> 55</span></p><p class="s33">&gt;<span class="s16"> 100</span></p><p class="s33">&gt;<span class="s16"> 105</span></p><p class="s33">&gt;<span class="s16"> 115</span></p></td><td><p class="s16">280</p></td></tr><tr><td><p class="s16">CuCr1Zr</p></td><td><p class="s16">R 200<span class="s18">a</span></p><p class="s16">R 400<span class="s18">b</span></p><p class="s16">R 450<span class="s18">b</span></p></td><td><p class="s33">&gt;<span class="s16"> 200</span></p><p class="s33">&gt;<span class="s16"> 400</span></p><p class="s33">&gt;<span class="s16"> 450</span></p></td><td><p class="s33">&gt;<span class="s16"> 60</span></p><p class="s33">&gt;<span class="s16"> 210</span></p><p class="s33">&gt;<span class="s16"> 360</span></p></td><td><p class="s16">30</p><p class="s16">12</p><p class="s16">10</p></td><td><p class="s33">&gt;<span class="s16"> 70</span></p><p class="s33">&gt;<span class="s16"> 140</span></p><p class="s33">&gt;<span class="s16"> 155</span></p></td><td><p class="s16">420</p></td></tr></table>
  
 
=====5.1.6.2.2 Copper-Zirconium Alloys=====
 
=====5.1.6.2.2 Copper-Zirconium Alloys=====
Line 83: Line 80:
 
The earlier used CuCr and CuZr materials have been partially replaced over the years by the capitation hardening three materials alloy CuCr1Zr. This material exhibits high mechanical strength at elevated temperatures and good oxidation resistance as well as high softening temperatures. In its hardened condition CuCr1Zr has also a high electrical conductivity (Bild 5.37). Their usage extends from mechanically and thermally highly stressed parts such as contact tulips in high voltage switchgear to electrodes for resistance welding.
 
The earlier used CuCr and CuZr materials have been partially replaced over the years by the capitation hardening three materials alloy CuCr1Zr. This material exhibits high mechanical strength at elevated temperatures and good oxidation resistance as well as high softening temperatures. In its hardened condition CuCr1Zr has also a high electrical conductivity (Bild 5.37). Their usage extends from mechanically and thermally highly stressed parts such as contact tulips in high voltage switchgear to electrodes for resistance welding.
  
Fig. 5.36:
+
Fig. 5.36: Copper corner of the copperzirconium for up to 0.5 wt% zirconium
Copper corner of the copperzirconium
+
[[File:Copper corner of the copper zirconium for up to 0.5-wt zirconium.jpg|right|thumb|Copper corner of the copper- zirconium for up to 0.5 wt% zirconium]]
for up to 0.5 wt%
 
zirconium
 
  
Fig. 5.37:
+
Fig. 5.37: Softening of CuCr1Zr after 1 hr annealing and after 90% cold working
Softening of CuCr1Zr after
+
[[File:Softening of CuCr1Zr after 1hr annealing.jpg|right|thumb|Softening of CuCr1Zr after 1 hr annealing and after 90% cold working]]
1 hr annealing and after 90%
 
cold working
 
  
 
==References==
 
==References==
 
[[Contact Carrier Materials#References|References]]
 
[[Contact Carrier Materials#References|References]]

Revision as of 18:14, 10 March 2014

5.1.6.1 Copper-Beryllium Alloys (Beryllium Bronze)

The cause for precipitation hardening of CuBe materials is the rapidly diminishing solubility of beryllium in copper as temperature decrease. As the phase diagram for CuBe shows, 2.4 wt% of Be are soluble in Cu at 780°C Figure 1 (Fig. 5.28). In this temperature range annealed CuBe alloys are homogeneous(solution annealing). The homogeneous state can be frozen through rapid cooling to room temperature (quenching). Through a subsequent annealing at 325°C the desired precipitation hardening is achieved which results in a significant increase in mechanical strength and electrical conductivity of CuBe (Table 5.17). The final strength and hardness values depend on the annealing temperature and time as well as on the initial degree of cold working (Table 5.18) and (Figs. 43 – 75)(Figs. 5.29 - 5.31).

Fig. 5.28: Phase diagram of copperberyllium with temperature ranges for brazing and annealing treatments
Phase diagram of copper- beryllium with temperature ranges for brazing and annealing treatments

As precipitation hardening alloys CuBe materials, mainly CuBe2 and CuBe1.7 have gained broad usage as current carrying contact springs because of their outstanding mechanical properties. Besides these CuCo2Be and CuNi2Be, which have medium mechanical strength and a relatively high electrical conductivity, are also used as contact carrier materials. After stamping and forming into desired contact configurations these CuBe materials are then precipitation hardened. CuBe alloys are available as semi-finished materials in a variety of cold work conditions. They can also be supplied and used in the already precipitation hardened condition without significant strength losses. In this case the hardening was already performed at the alloy producer.

Since Beryllium is rated as a carcinogen by the European regulation EU-67/548, it has been tried to reach the application properties of the well established CuBe1.7 and CuBe2 alloys with a lower Be content. The development efforts for alternate precipitation hardening materials without toxic and declaration requiring additive materials, for example CuNiCoSi, are aimed at the replacement of CuBe.

Figure 2 Fig. 5.29: Precipitation hardening of CuBe2 at 325°C after different cold working

Figure 3 Fig. 5.30: Precipitation hardening of CuBe2 (soft) at 325°C

Figure 4 Fig. 5.31: Precipitation hardening of CuBe2 (half hard) at different annealing temperatures

Precipitation hardening of CuBe2 at 325°C after different cold working
Precipitation hardening of CuBe2 (soft) at 325°C
Precipitation hardening of CuBe2 (half hard) at different annealing temperatures

Table 5.17: Physical Properties of Selected Copper-Beryllium Alloys (2 Teile!)

Table 5.18: Mechanical Properties of Selected Copper-Beryllium Alloys (2 Teile!)

5.1.6.2 Other Precipitation Hardening Copper Alloys

5.1.6.2.1 Copper-Chromium Alloys

As the phase diagram shows, copper-chromium has a similar hardening profile compared to CuBe Figure 5(Fig. 5.32). In the hardened stage CuCr has limitations to work hardening. Compared to copper it has a better temperature stability with good electrical conductivity. Hardness and electrical conductivity as a function of cold working and precipitation hardening conditions are illustrated in Figs. 5.33-5.35 (Tables 5.19 and 5.20).

Copper-chromium materials are especially suitable for use as electrodes for resistance welding. During brazing the loss in hardness is limited if low melting brazing alloys and reasonably short heating times are used.

Fig. 5.32: Copper corner of the copper-chromium phase diagram for up to 0.8 wt% chromium
Copper corner of the copper-chromium phase diagram for up to 0.8 wt% chromium

Fig. 5.33: Softening of precipitation-hardened and subsequently cold worked CuCr1 after 4hrs annealing

Softening of precipitation-hardened and subsequently cold worked CuCr1 after 4hrs annealing

Fig. 5.34 a: Electrical conductivity of precipitation hardened CuCr 0.6 as a function of annealing conditions

Electrical conductivity of precipitation hardened CuCr 0.6 as a function of annealing conditions

Fig. 5.34 b: Hardness of precipitation hardened CuCr 0.6 as a function of annealing conditions

Hardness of precipitation hardened CuCr 0.6 as a function of annealing conditions

Fig. 5.35: Electrical conductivity and hardness of precipitation hardened CuCr 0.6 after cold working

Electrical conductivity and hardness of precipitation hardened CuCr 0.6 after cold working

Table 5.19: Physical Properties of Other Precipitation Hardening Copper Alloys (2 Teile!)

Table 5.20: Mechanical Properties of Other Precipitation Hardening Copper Alloys

Material

Hardness

Condi- tion

Tensile

Strength Rm

[MPa]

0,2% Yield

Strength Rp02

[MPa]

Elongation

A50

[%]

Vickers

Hardness

HV

Spring Bending

Limit FFB [MPa]

CuCr

R 230a

R 400a R 450b R 550b

> 230

> 400

> 450

> 550

> 80

> 295

> 325

> 440

30

10

10

8

> 55

> 120

> 130

> 150

350

CuZr

R 260a

R 370a R 400b R 420b

> 260

> 370

> 400

> 420

> 100

> 270

> 280

> 400

35

12

12

10

> 55

> 100

> 105

> 115

280

CuCr1Zr

R 200a

R 400b

R 450b

> 200

> 400

> 450

> 60

> 210

> 360

30

12

10

> 70

> 140

> 155

420

5.1.6.2.2 Copper-Zirconium Alloys

The solubility of Zirconium in copper is 0.15 wt% Zr at the eutectic temperature of 980°C (Fig. 5.36). Copper-zirconium materials have a similar properties spectrum compared to the one for copper-chromium materials. At room temperature the mechanical properties of copper-zirconium are less suitable than those of copper chromium, its temperature stability is however at least the same.

5.1.6.2.3 Copper-Chromium-Zirconium Alloys

The earlier used CuCr and CuZr materials have been partially replaced over the years by the capitation hardening three materials alloy CuCr1Zr. This material exhibits high mechanical strength at elevated temperatures and good oxidation resistance as well as high softening temperatures. In its hardened condition CuCr1Zr has also a high electrical conductivity (Bild 5.37). Their usage extends from mechanically and thermally highly stressed parts such as contact tulips in high voltage switchgear to electrodes for resistance welding.

Fig. 5.36: Copper corner of the copperzirconium for up to 0.5 wt% zirconium

Copper corner of the copper- zirconium for up to 0.5 wt% zirconium

Fig. 5.37: Softening of CuCr1Zr after 1 hr annealing and after 90% cold working

Softening of CuCr1Zr after 1 hr annealing and after 90% cold working

References

References