Background of the invention
[0001] At the present time, aerosol cans are manufactured either from pure aluminium or
from aluminium alloys. In the former case, 1000-series aluminium according to the
European standard EN 573-3 is mostly used. The most common aluminium grades are EN
AW 1050A having the minimum Al content of Al 99.5% and EN AW 1070A having the minimum
Al content of 99.7%.
[0002] In the latter case, aerosol cans are mostly made of 3000-series aluminium alloys
according to the European standard EN 573-3. The most common aluminium alloy grades
are EN AW 3102 having the Mn content of approximately 0.3% and EN AW 3207 having the
Mn content of approximately 0.6%.
[0003] For the manufacture of aerosol cans, aluminium and its alloys are mostly supplied
in the form of slugs.
[0004] Such slugs are manufactured in a continuous two-phase process comprising the following
steps.
a.) Phase 1 - Manufacture of strips
[0005]
- Melting down ingots in melting furnaces.
- Transfer of molten aluminium into a holding furnace.
- Continuous casting of a strip.
- Hot rolling of the cast strip.
- Cold rolling of the cast strip.
- Coiling the rolled strip.
b.) Phase 2 - Manufacture of slugs
[0006]
- Uncoiling the rolled strip.
- Punching the slugs in a blanking press.
- Annealing of the slugs.
- Cooling down of the slugs.
- Surface finishing of the slugs (tumbling, sand blasting, vibration).
- Packaging of the slugs.
[0007] The method of manufacturing aerosol cans can be described as follows:
- Applying a lubricant to the slugs.
- Backward impact extrusion.
- Wall ironing of the can.
- Brushing of the can.
- Degreasing of the can.
- Application of the inner varnish layer + curing in a polymerization oven
- Application of the basecoat + curing in oven.
- Application of the decorative inks + curing in oven.
- Application of the overcoat + curing in oven.
- Shaping the cans on the necking press.
[0008] The above described materials according to the standards EN AW 1050A and EN AW 1070A
respectively exhibit significant levels of formability and work hardening which make
them ideal for the manufacture of aerosol cans in a backward impact extrusion process.
Aluminium alloys EN AW 3102 and EN AW 3207 offer enhanced mechanical properties (strength)
and hence better rigidity and pressure resistance of finished aerosol cans. Nevertheless,
the mechanical properties of these materials are changed when the cans pass through
a curing oven in which polymerization of the inner varnish layer takes place. The
curing (polymerization) temperatures of the inner varnish layers range between 210
and 255°C, the respective curing process lasting about 10 minutes. Under such temperatures,
partial annealing of the can bodies occurs causing the mechanical strength of the
same to decrease.
[0009] In order to eliminate the above undesirable effect, thicker walls of the aerosol
cans must be selected which are necessary for achieving the required safety and technological
specifications, particularly a sufficient pressure resistance, of the cans. This leads
to an significant increase of the consumption of input materials.
Summary of the invention
[0010] The above drawbacks are eliminated by the heat-resistant alloy for the production
of aerosol cans having the features defined in the characterizing part of claim 1.
Brief description of the drawings
[0011] The invention will be further explained with reference to the accompanying drawings
in which Fig. 1 shows the temperature dependences of the strengths of the new alloys
in comparison with those of standard alloys by means of a graphical representation.
[0012] The subject matter of the present invention is a new, modified heat resistant aluminium
based alloy provided for eliminating the effect of weakening the material of the cans
passing through a curing oven. Thereby, the desired enhancement of the mechanical
properties of aerosol cans is achieved in comparison with standard (conventionally
used) materials, along with the reduction of the wall thickness and increase of the
pressure resistance of the same. Particularly, the above favourable effect is achieved
by adding an anti-recrystallization admixture formed by Zr (zirconium) for the purpose
of modifying the compositions of aluminium and its alloys: EN AW 1050A, EN AW 3102,
EN AW 3207.
[0013] The chemical compositions of the commonly used, non-modified alloys have the following
limit values in accordance with EN 573-3 in percent by weight:
EN AW 1050A
Si ≤ 0.25; Fe ≤ 0.40; Cu ≤ 0.05; Mn ≤ 0.05; Mg ≤ 0.05; Zn ≤ 0.07; Ti ≤ 0.05; Al 99.5
min.
EN AW 3102
Si ≤ 0.40; Fe ≤ 0.70; Cu ≤ 0.10; Mn 0.05-0.40; Zn ≤ 0.30; Ti ≤ 0.10; Al remainder
EN AW 3207
Si ≤ 0.30; Fe ≤ 0.45; Cu ≤ 0.10; Mn 0.40-0.80; Mg ≤ 0.10; Zn ≤ 0.10; Al remainder
[0014] The alloys according to the invention have new chemical compositions with added Zr,
the proportion of the new constituent ranging between 0.05 and 0.20% by weight. The
addition of Zr gives rise to completely new alloys which cannot be categorized in
the existing classes according to the standard EN 573-3. Therefore, the new alloys
will be referred to as MC alloys hereinafter, namely MC1 (EN AW 1050A + Zr), MC3 (EN
AW 3102 + Zr) and MC4 (EN AW 3207 + Zr). The compositions of the new alloys (in percent
by weight) are as follows:
Alloy MC1
Si ≤ 0.25; Fe ≤ 0.40; Cu ≤ 0.05; Mn ≤ 0.05; Mg ≤ 0.05; Zn ≤ 0.07; Ti ≤ 0.05; Zr =
0.05÷0.20; Al remainder; (sum of all secondary elements ≤ 0.10)
Alloy MC3
Si ≤ 0.40; Fe ≤ 0.70; Cu ≤ 0.10; Mn 0.05÷0.40; Zn ≤ 0.30; Ti ≤ 0.10; Zr = 0.05÷0.20;
Al remainder; (sum of all secondary elements ≤ 0.10)
Alloy MC4
Si ≤ 0.30; Fe ≤ 0.45; Cu ≤ 0.10; Mn 0.40÷0.80; Mg ≤ 0.10; Zn ≤ 0.10; Zr = 0.05÷0.20;
Al remainder; (sum of all secondary elements ≤ 0.10)
[0015] Preferably, the new alloys have the following chemical compositions (in percent by
weight) which are optimized for the technology of production aerosol cans:
Alloy MC1
Si = 0.05÷0.09; Fe = 0.15÷0.27; Cu ≤ 0.005; Mn ≤ 0.005; Mg ≤ 0.005; Zn ≤ 0.015; Ti
= 0.01÷0.03; Zr = 0.05÷0.20; Al remainder; (sum of all secondary elements ≤ 0.10)
Alloy MC3
Si = 0.05÷0.09; Fe = 0.23÷0.27; Cu ≤ 0.005; Mn = 0.28÷0.32; Mg ≤ 0.005; Zn ≤ 0.015;
Ti = 0.01÷0.03; Zr = 0.05÷0.20; Al remainder; (sum of all secondary elements ≤ 0.10)
Alloy MC4
Si = 0.05÷0.09; Fe = 0.23÷0.27; Cu ≤ 0.005; Mn = 0.58÷0.62; Mg ≤ 0.005; Zn ≤ 0.015;
Ti = 0.01÷0.03; Zr = 0.05÷0.20; Al remainder; (sum of all secondary elements ≤ 0.10)
[0016] In order to verify the anti-recrystallization effect during the aerosol can production
process, the new alloys were compared with the known, commonly used materials. The
outcome is graphically represented in Fig. 1 where the first standard material according
to EN AW 1050A, herein specifically referred to as alloy A5, is compared with the
new alloy MC1_A and the second standard material according to EN AW 3102, herein specifically
referred to as alloy A3Mn, is compared with the new alloy MC3_A containing the added
anti-recrystallization constituent Zr. The cans, which were made of the above materials
under the same technological conditions, had identical wall specifications.
[0017] The standard alloys used for comparison purposes of anti-recrystallization effect
are designated as follows:
Alloy A5 (aluminium according to EN AW 1050A) having the following chemical composition
in percent by weight:
Si = 0.08; Fe = 0.24; Cu ≤ 0.005; Mn ≤ 0.005; Mg ≤ 0.005; Zn = 0.01; Ti = 0,02; Al
remainder
Alloy A3Mn (aluminium alloy according to EN AW 3102) having the following chemical
composition in percent by weight:
Si = 0.07; Fe = 0.25; Cu ≤ 0.005; Mn = 0.29; Mg ≤ 0.005; Zn = 0.01; Ti = 0.02; Al
remainder
[0018] The newly developed alloys used for comparison purposes of anti-recrystallization
effect are designated as follows:
Alloy MC1_A having the following chemical composition in percent by weight:
Si = 0.08; Fe = 0.24; Cu ≤ 0.005; Mn ≤ 0.005; Mg ≤ 0.005; Zn = 0.01; Ti = 0.02; Zr
= 0.11; Al remainder
Alloy MC3_A having the following chemical composition in percent by weight:
Si = 0.06; Fe = 0.23; Cu ≤ 0.005; Mn = 0.30; Mg ≤ 0.005; Zn = 0.01; Ti = 0.03; Zr
= 0.12; Al remainder
[0019] Table 1 shows the mechanical properties of the cans made of the above materials.
During the comparison, the values of the tensile strength (Rm) of the cans measured
before and after the curing oven, in which the inner varnish layer was polymerized,
were evaluated. Moreover, the hardness (HB) of the input semifinished products (slugs)
was measured.
Table 1
Alloy |
Hardness of the slug |
Tensile strength Rm [MPa] |
After the backward extrusion |
After the curing (polymerization) oven of inner varnish |
210°C/10min |
230°C/10min |
255°C/10min |
A5 |
20.8 |
164.1 |
154.8 |
150.5 |
135.1 |
A3Mn |
22 |
180.7 |
172.6 |
167.9 |
151.2 |
MC1_A |
22 |
171.0 |
171.1 |
168.3 |
167.2 |
MC3_A |
23.5 |
182.5 |
179.2 |
179.0 |
178.3 |
[0020] The results listed in Table 1 clearly show that the standard materials lose their
tensile strength when being subject to the temperature of 255°C in the oven, the strength
being decreased by 17.7% for aluminium A5 and by 16.3% for the alloy A3Mn. In contrast
to that, the loss of strength of the alloys containing Zr is significantly lower,
namely only 2.2% for the alloy MC1_A and 2.3% for the alloy MC3_A. In several cases,
even an increase of the tensile strength of the new alloys was observed after they
had passed through the curing oven.
[0021] The comparison of aluminium A5 with the alloy MC1_A shows that the value of the tensile
strength of the latter alloy was by 32.1 MPa higher after the passage through the
polymerization oven under the temperature of 255°C.
[0022] The comparison of aluminium alloys A3Mn and MC3_A shows that the value of the tensile
strength of the latter alloy was by 27.1 MPa higher after the passage through the
polymerization oven under the temperature of 255°C.
[0023] Also advantageous proves to be the fact that although the alloy MC1_A containing
the added Zr constituent has its tensile strength after the backward extrusion by
9.7 MPa lower in comparison with the alloy A3Mn, the passage of the alloy MC1_A through
the polymerization oven under temperatures over 226°C causes the strength of this
alloy to exceed the strength of the A3Mn alloy, even though the MC1_A alloy does not
contain Mn.
[0024] The main advantages of the new alloys MC1, MC3 and MC4 particularly include:
- a.) Owing to the admixture of Zr, the alloys MC1, MC3 and MC4 contain a fine dispersion
of Al3Zr.
- b.) The presence of manganese in the alloys MC3 and MC4 additionally results in an
increase of the strength of these alloys after undergoing a shaping process, this
being due to the formation of the particles of Al6Mn, Al6(FeMn) and α-Al(Mn,Fe)Si.
- c.) The above particles become caught in the subgrain boundaries, thus preventing
any recovery, formation of recrystallization nuclei or growth of recrystallized grains
from occurring (increasing the recrystallization resistance).
1. Heat-resistant alloy for production of aerosol cans from a material having the following
contents of alloying additions in percent by weight:
according to the standards EN 573-3
EN AW 1050A
Si ≤ 0.25; Fe ≤ 0.40; Cu ≤ 0.05; Mn ≤ 0.05; Mg ≤ 0.05; Zn ≤ 0.07; Ti ≤ 0,05;
EN AW 3102
Si ≤ 0.40; Fe ≤ 0.70; Cu ≤ 0.10; Mn 0.05-0.40; Zn ≤ 0.30; Ti ≤ 0.10;
EN AW 3207
Si ≤ 0.30; Fe ≤ 0.45; Cu ≤ 0.10; Mn 0.40-0.80; Mg ≤ 0.10; Zn ≤ 0.10;
or with more specific compositions
- Si = 0.05÷0.09; Fe = 0.15÷0.27; Cu ≤ 0.005; Mn ≤ 0.005; Mg ≤ 0.005; Zn ≤ 0.015;
Ti = 0.01÷0.03;
- Si = 0.05÷0.09; Fe = 0.23÷0.27; Cu ≤ 0.005; Mn = 0.28÷0.32; Mg ≤ 0.005; Zn ≤ 0.015;
Ti = 0.01÷0.03;
- Si = 0.05÷0.09; Fe = 0.23÷0.27; Cu ≤ 0.005; Mn = 0.58÷0.62; Mg ≤ 0.005; Zn ≤ 0.015;
Ti = 0.01÷0.03;
characterized in that each composition contains added Zr in the amount ranging between 0.05 and 0.20% by
weight, the sum of the contained amounts of all the secondary elements being ≤ 0,10%
by weight and Al content is remainder.
2. Modified heat resistant aluminium alloy according to claim 1, characterized in that the content of added Zr ranges between 0.10 and 0.15% by weight.