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after 4 thermal cycles: micro-cracks parallel to sample length due to compression stresses after 100 thermal cycles: cracks perpendicular to sample length due to tensile loading shortly before failure: further growth and accumulation of cracks preferentially perpendicular to
sample length failure: main crack propagates along pre-existing damage and rigid phases
High volume fractions of highly interconnected rigid phases can lead to a high tensile strength of the alloy at elevated temperatures, however the consequentially low ductility limits the TMF-resistance
Closely packed primary Si and intermetallic phases facilitate crack formation and propagation more refined structures have a positive effect on the TMF resistance
Damage mechanisms and evolution during thermomechanical fatigue of cast near eutectic Al-Si piston alloys
K. Bugelnig1, H. Germann2, T. Steffens2, F. Wilde3, E. Boller4, G. Requena5,6
1Institute of Materials Science and Technology, TU Vienna, Karlsplatz 13, 1040 Vienna, Austria 2KS Kolbenschmidt GmbH, Karl-Schmidt-Straße, 74172 Neckarsulm, Germany 3Institute of Materials Research, Helmholtz-Zentrum Geesthacht, D-21502 Geesthacht, Germany 4ESRF-The European Synchrotron, CS40220, Grenoble Cedex 9, France 5German Aerospace Centre, Linder Höhe, 51147 Cologne, Germany 6Metallic Structures and Materials Systems for Aerospace Engineering, RWTH Aachen University, Aachen 52062, Germany
Acknowledgements This work is part of the “K-Project for Non-Destructive Testing and Tomography Plus" supported by the COMET-Program of the Austrian Research Promotion Agency (FFG) as well as the Provinces of Upper Austria (LOÖ) and Styria, Grant No. 843540. The ESRF and DESY are acknowledged for the provision of synchrotron facilities at the beamlines ID19 and P05, respectively. Contact: [email protected]
Motivation Cast near eutectic Al-Si alloys are used in automotive pistons due to their high strength-to-weight ratio as well as excellent castability and heat conductivity. Particularly, the piston bowl rim in modern diesel engines must be able to withstand thermo-mechanical fatigue (TMF) conditions in a temperature range between 25 - 380 °C with thermal cycles of a few seconds during service. Topological and morphological changes in the microstructure owing to chemical compositions, thermal heat treatments and thermo-mechanical conditions during service can have a crucial effect on performance. Damage mechanisms and evolution during TMF of two Al-Si piston alloys have been studied with regards to the effect of 3D microstructural features.
Alloy Composition [wt.%]
Al Si Cu Ni Mg
AlSi12Cu3Ni2 bal. ~ 12 3 2 < 0.3
AlSi12Cu4Ni2Mg bal. ~ 12 4 2 1
Materials Methods
• gravity die casting • heat treatment: T5
primary Si
eutectic Si
aluminides
primary Si
eutectic Si aluminides
3D hybrid network of rigid phases
Microstructure in initial condition t [sec]
T [°C]
380
80
25 ε = 0 %
dT/dt = 15 K/sec
3 sec
10 sec
1. Gleeble 1500
piston bowl rim area
1 cm
plastic deformation [mm]
of the piston due to thermo-mechanical
loading
50 µm 50 µm
AlSi12Cu3Ni2 AlSi12Cu4Ni2Mg 2. Synchrotron tomography
Results
0 40 80 120 160 200 240 280 320 360
-200
-150
-100
-50
0
50
100
150
200 first 10 cycles
half of cycles to failure)
last 10 cycles
str
ess [
MP
a]
T [°C]
compression range
tensile range
Conclusions preferential damage initiation sites during TMF: micro-cracking through primary Si particles in Si clusters at junctions of coalesced primary Si
particles
AlSi12Cu4Ni2Mg AlSi12Cu3Ni2
Volume (primary Si) > 34500 µm³
Cu-rich alloy is prone to form large primary Si clusters during
solidification
AlSi12Cu3Ni2 AlSi12Cu4Ni2Mg
• high TMF resistance (822 ± 107 cycles) • comparatively higher ductility and lower
strength due to reduced Cu and Mg contents • comparatively small homogeneously
distributed primary Si particles (~ 8-10 µm) • nearly no primary Si clusters present
resulting in less sites for damage initiation and accumulation
• lower TMF resistance (about 40%) • lower ductility and higher strength due to
high volume fraction of intermetallic phases • larger primary Si particles (~ 10 - 15 µm)
• primary Si clusters provoke earlier formation
and higher accumulation of damage in these regions
initial condition micro-cracks through large, irregular primary Si (parallel to sample length)
after 4 cycles
micro-cracks through primary Si (parallel & perpendicular to sample length)
after 100 cycles
after 350 cycles post-mortem (504 cycles)
σ
100 µm
100 µm 100 µm
40 µm
10 µm
σ
primary Si
eutectic Si
aluminides 4 cycles 100 cycles 350 cycles post-mortem
200 µm
σ
200 µm 200 µm 200 µm
primary Si
micro-cracks
10 µm
σ
5. 3D visualization of damage evolution after selected TMF cycle numbers for AlSi12Cu4Ni2Mg
6. tomographic slices of the microstructure of AlSi12Cu4Ni2Mg after several TMF-cycles
4. Damage initiation preferentially in shape of micro-cracks parallel to sample length through large, irregular primary Si in clusters
1. cyclic stress evolution during TMF
10 µm
P05 ID19
Energy [keV] 23 19
Voxel- Size [µm³] (1.18)3 (0.33)3
Sample-to-detector distance [mm]
30 13
Exposure time [msec/proj] 1200 100
Nr. of proj. 900 5969
total scan time [h] 1.5 0.2
Beamline Parameters
Beamlines
Storage ring
Booster synchrotron Linear
accelerator
0
1.5x10-6
3.0x10-6
4.5x10-6
0 100 200 300 400 500 600 700 800 900
0
0.03
0.06
0.09
0.12
num
be
r d
en
sity
of vo
ids [µ
m-1]
AlSi12Cu3Ni2
AlSi12Cu4Ni2Mg
AlSi12Cu3Ni2
AlSi12Cu4Ni2Mg
vo
lum
e fra
ctio
n
of vo
ids [%
]
number of cycles to failure
0
200
400
600
800
1000
nu
mb
er o
f cyc
les
to f
ailu
re
AlSi12Cu3Ni2 AlSi12Cu4Ni2Mg
3. evaluation of damage during TMF
2. number of TMF-cycles to failure
Source: KS Kolbenschmidt GmbH
0.207
0.429
0.254
0.186 0.175
0.171
0.203
0.416
0.323
0.247