Damage analysis of aluminium--steel bimetals.
Maronek, Milan ; Caplovic, Lubomir
1. INTRODUCTION
Aluminium steel bimetals are often used in metal production
industry due to their good mechanical properties and very low transient
resistance between aluminium and steel. They can be made by several
technologies among which belongs also an explosion welding. However, the
combination of aluminium and steel is difficult to weld due to possible
formation of intermetallic compounds between aluminium and iron which
are hard and brittle. There is why the some bimetal manufactures uses
titanium as an interlayer between aluminium and steel.
An explosion welding process uses high speed impact and despite of
extremely short welding time (typically milliseconds) there is generated
enough heat in the joint interface to produce melted areas and to form
intermetallic compounds if the welded metals are prone to their
creation. That is why there is necessary to control the heat input by
explosion welding parameters, e. g. detonation velocity, dynamic
collision angle, set-up distance etc. (Hudak, 1995), (Kwang-Jin, 2007).
The bimetals subjected to the analysis in this paper were damaged
after a very short time of their work. Having known some of the process
variables, there could have been calculated other variables allowing to
estimate whether welding parameters had not been set too high with a
risk of intermetallic coumpound formation (Maronek. 1995). The proof of
their presence in the weld joint interface was carried out by
examination methods described below.
2. INVESTIGATION PROCEDURE
The first part of analysis was to determine the detonation velocity
of an explosive charge. In order to get the straight propagation of
detonation wave, the detonator initiates the primary charge with high
detonation velocity at first and this charge consequently initiates the
main charge having detonation velocity significantly lower. The front of
detonation wave forms an angle y with an edge of primary charge (Fig.
1). Detonation velocity of the main charge is described by formula:
[v.sub.d2] = [v.sub.d1] x sin [gamma] (1)
where [v.sub.d2] is the detonation velocity of main charge and
[v.sub.d1] is the detonation velocity of primary charge. Having known
the angle [gamma] and detonation velocity of primary charge [v.sub.d1],
there is possible to estimate the main charge detonation velocity and to
compare it with the recommended detonation velocity.
[FIGURE 1 OMITTED]
The next step used light microscopy, microhardness measurements in
the joint interface and electron probe microanalysis (EPMA).
3. RESULTS
A surface of damaged bimetals had wavy pattern typical for
explosion welding joints (Fig. 2).
[FIGURE 2 OMITTED]
The value of [gamma] angle measured on damaged bimetal (Fig. 3) was
24[degrees].
Detonation velocity of plastic explosive used as the primary charge
(Tvarex 4A) was 7300 [m.s.sup.-1]. Hence the detonation velocity of the
main charge (Sypex 14A, loose consistency) was determined according to
formula (1) to 2969 [m.s.sup.-1].
[FIGURE 3 OMITTED]
The recommended detonation welocity according to welding procedure
specification was 2200 to 2300 [m.s.sup.-1].
It was obvious the detonation velocity used was 29 to 35 % higher
than recommended and the occurrence of intermetallic compounds could
have been predicted.
Predicted presence of intermetallic compound was proved by light
and electron microscopy analysis. There was observed continual layer of
approximately 50 [micro]m thick brittle phase (Fig. 4) with. This layer
included cracks and there had been observed significantly plastically
deformed islands of metal matter.
[FIGURE 4 OMITTED]
The microhardness measurements showed, that the hardness of brittle
phase was 400 to 700 HV 0,1. This microhardness values significantly
exceeded the hardness of both basic materials (Fig. 5).
[FIGURE 5 OMITTED]
A test sample for the impact test had been prepared from the weld
joint. Having broken the test sample, the fractographic analysis of
revealed fracture surface as well as the the chemical composition of the
fracture surface by EDS analysis had been carried out. The morphology of
fracture surface (Fig. 6) was transcrystallic with brittle splitting.
The chemical analysis detected that the element composition corresponded
to intermetallic phase FeAl (Brundle, 1992), (Westbrook, 2000).
[FIGURE 6 OMITTED]
4. DICSUSSION
Detailed analysis of thin intermetallic phase showed, that a fine
microcrystalline metal compound was squashed into the crack area. That
means the created layer cracked immediately after its formation due to
intensive deformation. Consecutively small volumes of welded materials
were pressed into the cracks and aterwards in the process of impact load
they represented only a small barrier during the crack propagation. That
is why the fracture surface had such a heterogenous character. From the
chemical composition point of view the layer was unambiguously
identified as the intermetallic phase FeAl, which has low mechanical
properties.
5. CONCLUSION
The obtained results prooved, that the main cause of continuous
highly brittle phase FeAl formation having significant influence on
mechanical properties degradation of weld joint fabricated by explosion
welding with parameters mentioned and revealed above was the high
kinetic energy of used explosive charge. This energy caused the local
overheat of weld interface with temerature exceeding the aluminium
melting point. Due to this fact there came up appropriate cicrcumstances
for brittle phase formation.
The reason of high energy input during explosion welding could have
been in using explosive charge with higher detonation velocity, thicker
explosive charge or higher charge density. This finally led to higher
flyer plate impact velocity and thus higher kinetic energy transforming
after collision with parent plate to heat.
This paper was realised with the support of KEGA 3/4157/06 and APVV
0057-07 grants.
6. REFERENCES
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