Materials Science Forum
Vols. 534-536
Vols. 534-536
Materials Science Forum
Vols. 532-533
Vols. 532-533
Materials Science Forum
Vols. 530-531
Vols. 530-531
Materials Science Forum
Vols. 527-529
Vols. 527-529
Materials Science Forum
Vol. 526
Vol. 526
Materials Science Forum
Vols. 524-525
Vols. 524-525
Materials Science Forum
Vols. 522-523
Vols. 522-523
Materials Science Forum
Vols. 519-521
Vols. 519-521
Materials Science Forum
Vol. 518
Vol. 518
Materials Science Forum
Vol. 517
Vol. 517
Materials Science Forum
Vols. 514-516
Vols. 514-516
Materials Science Forum
Vol. 513
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Materials Science Forum
Vol. 512
Vol. 512
Materials Science Forum Vols. 522-523
Paper Title Page
Abstract: In situ observation of the mechanical failure behavior was conducted for different kinds of
the plasma sprayed thermal barrier coating (TBC) systems by means of an optical microscopy under
the static loadings at room and elevated temperatures; as the fundamental aspect, in order to clarify the
thermomechanical failure mechanism of TBC system in connection with various coating
characteristics. Mechanical tensile or compressive loading was applied progressively to the TBC
specimen by an axial loading mode.
It was found that the failure behavior of TBC system depends strongly on the testing temperature
under both the tensile and compressive loadings. At the elevated temperature which is higher than the
ductile-brittle transition temperature (DBTT) of metallic bond-coat (BC), in particular, the ceramic
top-coat (TC) spallation can be prevented by virtue of the stress relief induced by the enhanced plastic
flow in the BC layer. At the room temperature which is lower than the DBTT of BC, on the contrary,
the TC spalling was inevitably induced, but the initiation site of TC spalling is closely related with the
magnitude of local plastic deformation in the alloy substrate. Furthermore, an influence of thermally
grown oxides (TGO) layer developed at the TC / BC interface on the crack initiation and propagation
behavior was investigated in some detail.
345
Abstract: In order to clarify the failure behavior of plasma sprayed thermal barrier coating (TBC)
systems under the complicated modes of thermal-mechanical-chemical loadings, the stress rupture
property evaluation and failure analysis were conducted for Y2O3-ZrO2 (YSZ) and CaO-SiO2-ZrO2
(C2S-CZ) TBC systems in air and two kinds of high-temperature corrosive environments.
Static creep loading was found to bring about the typical creep failure for TBC systems even in the
aggressive environment so called hot corrosion almost in similar manner to the case in air. On the
contrary, it was revealed that the dynamic fatigue loading tends to cause a significant failure life
reduction of TBC systems both in air and in corrosive environments. For YSZ TBC system, the
penetration crack preexisting through the top-coat layer tends to provide a nucleation site for the
fatigue crack even in air, and more significantly a short circuit path for the corrosive species in hot
corrosive environment. For C2S-CZ system, on the contrary, the top-coat / bond-coat interface tends
to provide easily the nucleation site for a main crack to propagate thereafter toward both the alloy
interior and outer surface. Under lower stress level at 950°C, however, the oxide-induced crack
closure together with crack tip blunting attributed mainly to the high reactivity of Ca compounds as a
major constituent of the TC is effective to suppress substantially the crack propagation, so as to cause
the prolonged failure life as compared to YSZ system even in aggressive gaseous environment.
353
Abstract: Ni-base single crystal (SC) superalloys containing high concentrations of refractory
elements are prone to generate a diffusion layer called Secondary Reaction Zone (SRZ) beneath their
bond coating during exposure at high temperatures. SRZ causes a reduction of the load bearing cross
section and is detrimental to the creep properties of thin-wall turbine airfoils. In this study, a new
coating system – “EQ coating”, which is in thermodynamic equilibrium with the substrate, has been
proposed and the formation behavior of SRZ beneath bond coat materials was investigated on the 5th
generation Ni-base SC superalloy developed by NIMS. Diffusion couples of several alloys were made
and were heat treated at 1100°C for 300 h, 1000 h. The concentration profiles were analyzed by
EPMA. Also, cyclic oxidation tests were carried out at 1100°C in air.
361
Abstract: A coating with duplex structure of a outer β-NiAl and an inner α-Cr layer, was formed
on a Ni-40Cr-3Re (in at%) alloy with or without Zr addition, and the coated alloys were
oxidized under thermal cycling in air for up to 2300ks. The coated alloys containing Zr
showed a two-step parabolic oxidation, the kp1st in the early stage of oxidation was
2.6~5.4×10-11 kg2
m-4
s-1 for four alloys tested, and kp 2nd for the longer oxidation increased
with increasing Zr content from 2.6~5.4×10-11 for the alloy with 0.1at%Zr to 9.6×10-11 kg2
m-4
s-1 for the alloy with 1.0at%Zr. The rapid oxidation for the alloy with 1.0at%Zr is due to
the formation of ZrO2 as an internal oxide. The oxide scale in the 1st stage consisted of both
α- and θ- Al2O3 with whiskers, and with further oxidation the α-Al2O3 became the major
product in the 2nd stage. After the oxidation for 2300ks the as-prepared, outer β-NiAl was
changed into a mixture of β-NiAl and γ’-Ni3Al for the Ni-40Cr-3Re alloy containing Zr, while
in the coated Ni-40Cr-3Re alloy the outer layer became a mixture of γ’-Ni3Al and γ-Ni(Al,Cr).
It was concluded that the addition of Zr into the coated Ni-40Cr-3Re alloy helps maintain
high Al contents in the outer Ni-aluminide layer by forming a protective Al2O3 layer.
369
Abstract: In order to improve the cyclic-oxidation resistance of Ni and SUS304 steel, the coating of
a Ni aluminide containing La on both samples were carried out by the electrodeposition of Al and
La in a molten salt. The electrodepositions of Al and La were conducted using a potentiostatic
polarization method at 1023 K in an equimolar NaCl-KCl melt containing 3.5 mol%AlF3, and that
containing 4 mol%La2O3-24 mol%NH4Cl, or 3.5 mol%LaF3. Observation and analysis of the
cross-section of the specimen after polarization showed that a deposited layer consisting of a thick
inner Ni aluminide layer and a thin outer layer containing a large amount of La was formed on both
samples. The cyclic-oxidation resistance of the Ni specimen covered with the deposit layer having
the La layer as the outer layer was higher than those of the untreated Ni specimen and the Ni
specimen coated with the deposit layer without La. The stainless steel covered with the Ni
aluminide showed a high cyclic-oxidation resistance in the atmosphere containing water vapor at
1273 K in comparison with untreated stainless steel, without depending on the existence of La in
the deposited layer.
377
Abstract: The thermal sprayed coatings are widely used in waste incineration boilers and fossil fuel-fired
boilers. However, the defects, such as porosity, cracks and unmelted particles, in these coatings are
detrimental to corrosion performance. In this study, the nickel based self fluxing alloy coating was fused
by YAG laser to improve hot corrosion resistance of the coating. Under appropriate laser parameters, the
nonporous, crack-free coating was produced. Hot corrosion test, conducted in the presence of a mixed salt of
Na2SO4/NaCl/KCl at 550Гshowed that the modified coating exhibited excellent corrosion resistance
compared with the as sprayed and gas fused coatings.
385
Abstract: In the high temperature oxidation of metallic alloys oxide scale strains and in particular critical
scale strains play a key role with regard to scale adherence. Scale spallation/exfoliation is a vital
issue for not only long term alloy performance but also steel sheet production. In many cases materials
selection is based on thermodynamic considerations and short term laboratory data, not taking
into account changes in the oxidation mechanisms resulting from stresses induced by thermal cycles,
oxide growth, specimen or component geometry, or other operational factors. This paper presents
a very concise summary of the present knowledge in the form of an approach to a comprehensive
scale failure model which is based on a number of microscopic and macroscopic system parameters.
This failure model is part of an on-going work which aims at a computer-assisted assessment
of oxide scale mechanical reliability.
393
Abstract: The mechanical behavior of oxidized low alloyed steel has been studied at
temperatures between 700°C and 900°C. Such a work is carried out to obtain information
about the damages which occur in the oxide scales developed on steels during hot rolling
process. Actually the mechanical behavior is tested with a four point bending apparatus at
high temperature under controlled atmosphere. Some information about mechanical damages
have been collected during the mechanical loading thanks to recording of the sample acoustic
emission. During this study, two procedures have been used which differ in the thermal
scheme used to build the oxide scales. The results obviously show that the procedure has a
great influence on the mechanical behavior of the oxidized low alloyed steel. For instance a
marked decrease of the stress is observed at constant displacement between the 900°C and
800°C tests of one procedure, as the opposite behavior is observed with the other procedure.
Different points are considered to explain such results, as the thermal strains which are only
present in one of the two procedures, the phase transformations in the metal and in the oxide.
401
Abstract: For industrial purposes, the adhesion control of secondary scale on hot rolled steel sheet
is important. A basic study was carried out to clarify the effect of scale microstructure on the scale
adhesion of low carbon steel (0.03%C-0.2%Mn). When scale of FeO (about 8μm thickness) was
generated at 800°C and transformed by continuous cooling from 250~600°C to 200°C, the scale
transformed from 400°C showed good adhesion. The scale consisted of magnetite seam from the
steel substrate, lamellar structure of magnetite and α-Fe, and magnetite layer from the scale surface.
The orientation analysis by TEM showed the relationship {110}Fe // {100}Fe3O4, <110>Fe //
<100>Fe3O4, and the lattice strain was calculated as 4%. On the other hand, FeO/Fe substrate
showed the relationship {100}Fe // {110}FeO, <110>Fe // <110>FeO, and 25% lattice strain was
calculated. It is considered that the adhesion of scale should be affected by the lattice strain, thus
Fe3O4/Fe substrate showed better adhesion than FeO/Fe substrate. The temperature of FeO
formation also affects the scale adhesion through the extent of Fe super saturation in FeO.
409
Abstract: It is very difficult to obtain mechanical properties of oxide films formed on a
material in high temperature environments despite its importance of estimating material
degradation caused by such as thermal stress. Corrosion/oxidation tests were conducted for
pure titanium and titanium alloy in high temperature corrosive environments of wet air and
water vapor with hydrogen chloride at temperatures from 673 K to 973 K to look into basic
behavior of degradation and the growth of titanium oxide films. It was found that oxide films
were usually formed on the specimen surface and the growth was accelerated by the
corrosiveness of the environment. In order to examine mechanical properties and exfoliation of
corrosion products or oxide films formed on titanium and its alloy, tests of single particle
impact on the specimen surface with a glass bead were performed in high temperature
corrosive environments. The piling-up surfaces around impact craters were formed and
plastically strained. The oxide film formed on the metal surface was detached in a wide range
of the circumference and fractured a little far from the rim of the crater. Then fracture and
exfoliation stress of the oxide film were estimated by the calculation of impact energy and
fractured and detached areas. It was found that both the fracture and exfoliation stress of the
oxide films were different depending on the corrosive environment and chemical composition
of titanium alloy.
417