Key Engineering Materials
Vol. 383
Vol. 383
Key Engineering Materials
Vols. 381-382
Vols. 381-382
Key Engineering Materials
Vol. 380
Vol. 380
Key Engineering Materials
Vols. 378-379
Vols. 378-379
Key Engineering Materials
Vol. 377
Vol. 377
Key Engineering Materials
Vols. 375-376
Vols. 375-376
Key Engineering Materials
Vols. 373-374
Vols. 373-374
Key Engineering Materials
Vols. 368-372
Vols. 368-372
Key Engineering Materials
Vol. 367
Vol. 367
Key Engineering Materials
Vols. 364-366
Vols. 364-366
Key Engineering Materials
Vols. 361-363
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Key Engineering Materials
Vols. 359-360
Vols. 359-360
Key Engineering Materials
Vols. 353-358
Vols. 353-358
Key Engineering Materials Vols. 373-374
Paper Title Page
Abstract: The high-energy laser melts the cladding materials which coagulate onto the surface of
the base materials. The laser cladding coatings are produced mainly in two methods: powder
feeding and prefabricating. The grain-strengthening composite coatings could be formed more
easily by prefabricating method than by powder feeding method. In this paper, Ni/SiC ceramic
composite coating on carbon steel (45 steel) was made by prefabricating method. The
microstructure and wear-resistance of Ni/SiC cladding coating on the 45 steel were studied using
scanning electronic microscope (SEM) and wear test. The results showed that the microstructure of
cladding coatings included bonding layer, thermo-affected layer and heat-affected layer after laser
cladding. The microstructure of cladding coating was mainly of dendrite and cell-like crystals. The
resultant multilayered coating had excellent adherence with the base steel. The addition of SiC
particles into cladding coatings significantly reinforced the microhardness of laser cladding coating.
Compared with Ni60A cladding coating, Ni60A/SiC cladding coating had high microhardness,
which was attributed to not only the dispersion intensification effect of the SiC particle, but also by
the new complicated phases. During laser cladding process, SiC particles may decompose and
dissolve into the coating and result in solid solution strengthening effect which increases the
microhardness of the composite coatings. The base material and Ni-based laser cladding coatings
with and without SiC were tested to assess the wear-resistance property. The test results
demonstrated that the laser cladding coatings had better wear resistance than the base material.
Furthermore, the laser cladding coating with SiC particles had higher wear-resistance than the
coating without SiC.
375
Abstract: This paper presents some results of plasma oxidizing of Al alloys. The oxidation of
aluminium alloys was carried out in the mid-frequency pulsed excited plasma. The processing
temperature was 450~500°Cand the processing time was 4 hours. The modified layer was
characterized by X-ray photoelectron spectroscopy (XPS), atomic force microscopy (AFM) and
scanning electron microscopy (SEM). AFM and SEM observations indicated that there were no
evident defects appeared in the modified layer. The immersion experiments in 3.5% NaCl solutions
were carried out to test the effect of plasma oxidation on the corrosion resistance of Al alloys. After
immersion for 200 hours, the severe pit-corrosion was occurred on the untreated sample surface
while for the treated sample no evident corrosion was observed.
379
Abstract: A numerical simulation is proposed to study the dynamics expansion characteristics
during the material irradiated by a high-intensity laser beam.The ionization effect and the local mass
and momentum conservations for plasma expansion are considered in this model. As an example of
carbon target, the plasma flow dynamics into a vacuum, like ionization degree, plasma number
density and space pressure are studied in detail. The results show the plasma temperature strongly
affects the ionization fraction and the ionization effect evidently influences the plasma dynamic
expansion behavior. The space pressure of plasma decreases along with the plasma expansion.
382
Abstract: Ultrasonic phase spectrum of reflection coefficient has been used to nondestructively
characterize the density, porosity, and microcracks of plasma sprayed Cr2O3 coatings irradiated by
high-intensity pulsed ion beam (HIPIB). The ultrasonic measurement was investigated using
immersion focusing pulse echo method with a 25 MHz transducer and the phase spectrum of
reflection coefficient has been experimentally obtained. The relationship among velocity, density,
attenuation coefficient and the phase spectrum was analyzed based on an acoustic transmission model
in a multi-layered structure. The velocity relates to the harmonic frequency of the phase spectrum, and
the density and attenuation coefficient play roles on the amplitude of the maximum and the shape of
the spectrum. The effects of the three parameters (velocity, density and attenuation coefficient) on the
amplitude of the maximum of the phase are similar. Some critical value exists which change the
relationship between the individual parameter and the maximum of the phase spectrum. When one of
the three parameters exceeds the corresponded critical value, the amplitude of the maximum
decreases in the form of exp( ) n y = A Bx . For the as-sprayed and irradiated coatings with the thickness of
50 0m, the velocity calculated from the phase spectrum is 2522 and 2772 m/s, harmonic frequency
corresponding to 12.61 and 13.86 MHz, respectively. These ultrasonic determinations demonstrated
that the coating becomes more densified after irradiation by HIPIB, in agreement with SEM
observations. Ultrasonic phase spectrum itself is a good indicator to reveal differences between
density and microstructures of coating prepared with various conditions as well as to follow their
evolution after HIPIB irradiation.
386
Abstract: In order to improve the wear resistance of the surface of thick copperplate, a coating of
alloy powder is produced on the surface of the thick copperplate with the method of laser remelting
plasma sprayed coating. The value simulation of temperature and the experimental results show that,
it is difficult to produce ferronickel coating with large area and crackfree on thick copperplate for
laser cladding technique. Using transsonic plasma heat spraying method to fix the alloy powder on the
surface of thick copperplate, a sprayed coating can be produced, which has certain adhesion strength
to the copperplate. In order to prevent crack produced in large area laser remelting coating, a method
with band-like and point-like remilting area at intervals of same distance has been taken. The surface
appearance and roughness of the coating produced by plasma spraying are compared with that of the
coating produced by plasma spraying and remelted by laser, micro organization analysis and wear
resistance comparison experiments are taken to the specimen. The microstructure photos show that
the coating of the plasma heat sprayed is mainly made up by grains, with a great deal of pores existing.
After laser remelting, microstructure of the coating is more compact, and the most of pores
disappeared, so the strength of the boundary between the remelted coating and the copperplate is build
up and the coating with large area and crackfree on thick copperplate is performed by the method of
laser remelting plasma spraying coating in large amount of point-like remilting areas
The experiment result shows that the wear resistance of laser remelting plasma heat sprayed coating
enhances 3 times more than That of the unremelt coating, and about 14 times compared with the
copperplate, and the wear resistance of the surface with point-like laser remelting area is between that
of plasma heat sprayed coating and that of the laser remelting coating, it depends on the ratio of the
remelted part to the whole in area, however, the wear resistance increases with the value of the ratio
392
Abstract: In this paper, boron films were deposited on W6Mo5Cr4V2 high speed steel (HSS) via ion beam
sputtering of boron target and implanted with polyenergetic(50 keV, 30 keV, 10 keV) nitrogen ions.
The mechanical properties of the implanted layer were tested by Vicker`s hardness and SKODA wear
tester. The microstructure of the implanted layer was analysed by X-ray Photoelectron Spectroscopy
(XPS) and Fourier Infrared (IR) spectroscopy. Experimental results showed that the HSS substrate
was intensified obviously after the implantation of boron and nitrogen ion. When the nitrogen dose
equals to 12.8×1017 ions/cm2, the hardness reaches its highest value, HV1982 and the relative
wearability was increased for about ten times under the load of 30N. XPS depth concentration profiles
show an interfacial mixing between film and substrate, and compared with monoenergetic ion
implantation, polyenergetic ion implanted layer have an even N/B distribution. Combined with XPS
and IR analysis results, It can conclude that boron exists in the form of boron nitride and first as a-BN
or h-BN, with the depth decreasing, it has a tendency to transform to c-BN.
396
Abstract: A remanufacturing system based on robot MAG surfacing has been developed recently. In
this paper, the work principle, functions and composition of this system are introduced. A worn metal
part to be remanufactured should be preprocessed firstly, and the defective model of the part gained
by reversing engineering technology is compared with normal model of the metal part, then the
prototyping path layout is carried out combined with MAG welding process, finally the
remanufacturing prototyping is implemented. The remanufacturing system is composed of robotic
system (as executing machine), 3D laser scanner (as reversing scanning device), digital pulse MAG
welding power source (as prototyping equipment), desk computer (as central control unit) and
software modules that support various functions. The functions of the remanufacturing system
comprise calibration of system, part reversing measurement, data processing, defective model
reconstruction, welding remanufacturing prototyping path layout and etc. It is indicated that the
exploitation of the remanufacturing system will provide an effective way for the remanufacturing of
metal defective parts.
400
Abstract: Compressor rotor blade is one of the critical parts of aero-engine. Because of the
complex structure and bad work environment, it often went wrong. More over, the trouble of blade
can result in serious accident of engine even the aircraft. But the conventional shot peening
strengthen method couldn’t take ideal effect, so a new method, laser shock peening on aero-engine
compressor rotor blade was studied in this paper. The principle of laser shock peening strengthening
was presented first, and the appropriate shock parameters of a certain type blade are fixed on by
modeling. The parameters were as follows: laser pulse width is 20ns, output energy is 25J, the spot
diameter is 8mm, and peak value is at GW level, and the laser peak value power is bigger than
material dynamic yield intensity. Based on these parameters, an experiment was performed by
shocking the blade through a repeated Nd: glass LASER supplied by Jiangsu University. Through
contrastive performance test, an analysis on the high frequency fatigue life and surface rigidity of
the blade fore and after laser shock was performed. The result was concluded that laser shock
peening can significantly increase the high frequency fatigue life of aero-engine compressor rotor
blade, and enhance the surface rigidity to increase the performance of contuse resistance. At last the
reasons were analyzed from two aspects: laser shock can impart compressive residual stress on
blade and reduce the size of crystal grain. Surface compressive residual stress can change the blade
distribution of load when working; and reduce the size of crystal grain can bring in more crystal
interface, for the more interface the crystal has the higher dislocation moving resistance and yield
stress is produced.
404
Abstract: According to analyzing the principle of atmospheric pressure plasma arc (APPA) cleaning
metal surface, a model of heat and mass transfer is put forward with using transient-state heat transfer
equation about interior heat source and Arrhenius equation of chemical reaction kinetics theory. With
finite volume method, the one dimensional control differential equation is transformed into discrete
control equation, which is calculated numerically and analyzed with the using of implicit scheme.
Taken cleaning lubricant film as an example and analyzed temperature distribution of cleaning film
on metal surface, the result indicates that the temperature of film has a strong effect on its removal rate
which improves with increasing temperature. In order to both avoid damaging the workpiece surface
owing to higher temperature and ensure removal rate of the film, there exists an appropriate
temperature under given calculation conditions.
408
Abstract: The preparation and characterization of a nickel-based composite coating reinforced by
TiB2 particles produced in situ and WC particles on stainless steel by laser cladding have been
investigated. The experiment results show that the coating obtained at suitable parameters
epitaxially grows from the substrate. The coating is mainly composed of γ-Ni dendrite and
dispersed TiB2 and WC particles. In the upper part of the coating, the white phase dispersed in the
coatings is mainly fine batt-shaped TiB2 particles. In the middle and bottom parts of the coating, the
white phase is mainly composed of comparatively coarse equiaxial WC particles, only an small
amount of fine TiB2 particles are present. The different distribution of TiB2 and WC should be
attributed to the density difference of TiB2, WC and Ni-based alloys and the comparatively slow
scanning rate. No cracks were observed throughout the whole coating, especially in the interface,
after the coating was deal with by the thermal shock experiment, which shows that the coating
processes a good metallurgical bond with the substrate and the high cracking resistance.
412