inter diffusion involved in shs welding
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Interdiusion involved in SHS welding of SiC ceramic to itself and toNi-based superalloy
Shujie Li a,*, Huiping Duan a, Shen Liu a, Yonggang Zhang a, Zijiu Dang b,Yan Zhang b, Chengang Wu a
a Department of Materials Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100083, People's Republic of Chinab State Key Laboratory for Advanced Metals and Materials, University of Science and Technology Beijing, Beijing 100083, People's Republic of China
Received 26 October 1999; accepted 24 January 2000
Abstract
In order to reach a better understanding of the mechanism of joining of SiC ceramic to itself and to Ni-based superalloy by
pressure-aided self-propagating high-temperature synthesis (SHS) welding process, microstructural study and energy dispersive X-
ray microanalysis (EDX) were carried out with the welded samples. The wettability between SiC ceramic and the liquid reaction
products of the ller is very good. A composition transition layer forms at the SiC/ller interface mainly due to the diusion of Ti
from the ller to the ceramic. The anity between Ti and SiC is better than that between Ni and SiC. The components of the Ni-
based superalloy remarkably diuse into the reaction products of the ller. The microstructure shows an excellent bonding at the
interfaces. 2000 Published by Elsevier Science Ltd.
Keywords: Diusion; Multilayer structure; Powder technology
1. Introduction
Ni-based superalloys are widely used to manufacture
the parts of aeronautical turbine serving at elevated
temperatures. The working temperature of these mate-
rials can reach 950C (type GH128) or higher. But, it is
still not high enough for the next new turbines. In order
to further increase the working temperature and de-
crease the weight of the turbines, new high temperature
structure materials are being expected and investigated.
Among them, SiC ceramic and SiC matrix composite are
promising ones. However, one problem arising with the
application of SiC is joining of the ceramic to metals,
particularly Ni-based superalloys. As indicated by
Ref. [1], the application of ceramic materials normally
depends on the joining of ceramics to metallic structures,
as we are living in a technological world based on the
application of metals.
Self-propagating high-temperature synthesis (SHS) of
powder compacts is a novel processing technique being
developed as a route for the production of engineering
ceramics and other advanced materials [2]. This process
seems to oer just the sort of innovative new method for
welding of ceramics and intermetallics. SHS oers many
attractive features such as energy eciency, limitation of
thermal disruption of heat-sensitive substrate micro-
structures, due to rapid and highly localized heat gen-
eration, easy availability of chemical compatibility
between the reaction products and substrates, as the
process being used to produce the joint is often the same
as the process that was or could have been used to
produce the substrates, the possibility to form a com-
posite ller incorporating reinforcing phases such as
particles, chopped bres or whiskers, and the possibility
to form functionally gradient material (FGM) joints
promising for overcoming mismatches between the
chemical composition, physical and mechanical prop-
erties of dissimilar materials [3,4]. Although SHS weld-
ing of ceramics to metals is currently being in the stage
of laboratory investigation, it has shown broad pros-
pects from both technical and economical points of
view. This paper will deal with the interdiusion and
microstructures relevant to SHS welding of SiC ceramic
to itself and to Ni-based superalloy.
International Journal of Refractory Metals & Hard Materials 18 (2000) 3337
* Corresponding author. Tel.: +86-10-82314972; fax: +86-10-
82316100.
E-mail address: [email protected] (S. Li).
0263-4368/00/$ - see front matter 2000 Published by Elsevier Science Ltd.
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2. Experimental
The commercial recrystallized SiC ceramic with the
density of 2.65 gacm3, the porosity of 1516% and the
purity ofb 99 wt% was used as the starting ceramic tobe welded. The forged Ni-based superalloy (type
GH128) was used as the starting metallic material to be
welded. This alloy contains Cr(19.022.0 wt%), W(7.5
9.0 wt%), Mo(7.59.0 wt%), Ti(0.40.8 wt%), Al(0.40.8
wt%) and other elements with low content. The utilized
welding materials (llers) and their purities are as fol-
lows: Ti powder (99.23 wt%), Ni powder (99.7 wt%) and
Al powder (99.6 wt%). The particle size of the metallic
powders is 200 mesh. C powder was also used as acomponent of the welding materials. Its particle size is
0.11 lm.
The SiC ceramic and the Ni-based superalloy were
machined to cylindrical billets with the size /10 mm
5 mm. The surface for welding was polished. The SiCbillets were washed in NaOH solution with an ultrasonic
bath for 15 min, then washed in pure water. The Ni-
based superalloy billets were washed in acetone with the
same ultrasonic bath for 15 min too. Then the cleaned
billets were put in a desiccator.
The powders with designed composition were mixed
homogeneously and then cold compacted to form
compacts with the size /10 mm (11.5) mm, whichwere used as welding materials. The SiC ceramic billet,
the powder compact and the Ni-based superalloy billet
were loaded into a graphite die. Then, pressure-aided
SHS welding test was carried out by a thermo-me-chanical testing machine, type Gleeble 1500, as sche-
matically shown in Fig. 1. This is a completely
computer-controlled apparatus. The samples were
heated up by passing an electrical current, and the at-
tainable maximum temperature is 1500C. As SiC ce-
ramic is an electrical insulator, the electrical current was
transferred by the graphite die. The temperature of the
sample was measured by the thermocouple as shown in
Fig. 1 and controlled automatically.
In order to facilitate the interfacial reactions between
the SiC ceramic and the powder compact, it was de-
signed that the compact includes a reaction layer
neighboring with the ceramic, which contains sucient
active element. This layer should be as thin as possible
for preventing the welded samples from reducing of the
properties. As the Gleeble 1500 is not equipped with
ignition facilities, it is necessary that the compact also
includes an ignition layer, of which the ignition tem-
perature is lower than the attainable maximum tem-
perature of the machine. It should be noticed that the
presence of the reaction products of the ignition layer
should not cause the decrease of the properties of the
welded samples.
As indicated in Ref. [4], the degree of mismatch be-
tween the coecients of thermal expansion of the joint
materials and the ller should be smaller than about 15
25% in order to avoid joint failure. This should be fol-
lowed in designing the FGM llers. However, for the
sake of convenience to investigate the interfacial diu-
sion, interfacial reaction and microstructure, a simpliedFGM ller was studied in this paper, of which the
composition is listed in Table 1.
The temperature system tested is as follows:
Room temperature 35KaS
1273 Kkeep for 5 min
32KaS
673 K 3cooling in furnace
473 KX
The SHS welding test was conducted at constant pres-
sure 10 MPa in vacuum 35103 Torr. The micro-structure and composition of the welded area were
analyzed by scanning electron microscope (SEM) and
energy dispersive X-ray microanalysis system (EDX).The same process was utilized in welding SiC ceramic
to itself. The composition of the llers tested is presented
in Table 2. SEM and EDX analyses were also carried
out to investigate the microstructure and composition of
the welded interfaces.
3. Results and discussion
3.1. SHS welding of SiC ceramic to itself
3.1.1. Experimental results
The experimental results of SHS welding of SiC ce-
ramic to itself are presented in Table 2. (The sign `0'
denotes success of welding, `x' denotes failure.) This
table also shows the composition of the llers and the C
percentage of each combination. One can see that every
ller can reach a successful welding except ller No. SS-
6. It is noticed that the C content of this ller is quite
high. C may react precedently with the active compo-
nent Ti to form stable TiC, which consumes the active
component. Besides, the presence of TiC may decrease
the mobility of the remaining active components leading
to reducing the opportunity of contact between SiCFig. 1. Sketch map of SHS welding of SiC ceramic to Ni-based
superalloy.
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ceramic and the active components. This may be the
reason for the failure of welding.
3.1.2. Wettability
The SHS welding materials as shown in Table 2 will
form a great quantity of liquid phase during the thermal
explosive reaction. The wettability between the liquidand SiC ceramic is very important with regard to eec-
tive interfacial reactions, interdiusion and even a suc-
cessful welding.
Fig. 2 shows the microstructure at the interface be-
tween SiC ceramic and the reaction products of ller
No. SS-2. The black phase on the right is SiC ceramic. It
can be seen that the wettability between the liquid
formed during the thermal explosive reaction and SiC
ceramic is very good, which provides the possibility of
full contact, interdiusion, interfacial reactions and
formation of chemical bonding. Also, one can see that
many open pores exist at the surface of the ceramic. The
liquid can penetrate into the pores under the capillary
and external pressures, forming mechanical bonding
between the ceramic and the reaction products aftersolidication. This enhances the strength of joining at
the interface.
The experimental results indicate that for all the llers
except No. SS-6 listed in Table 2 the liquid formed
during SHS reaction can wet SiC ceramic and result in
mechanical bonding with SiC ceramic after solidica-
tion.
3.1.3. Interdiusion and interfacial reaction
The strength of joining at the interface between SiC
ceramic and the reaction products of the llers is
strongly aected by the interdiusion, the interfacial
reactions and the chemical bonding. As reported in Ref.
[5], all the active elements such as Ti, Ni and Al can
react with SiC ceramic.
The microstructure and the distribution of Si, Ti and
Ni at the interface and its neighboring areas between
SiC ceramic and the reaction products of ller No. SS-
3(Ni:Ti:C 3:2:0.5) are presented in Fig. 3. The blackphase on the left is SiC ceramic. There are no open pores
at the local surface of the ceramic. The reaction prod-
ucts are mainly composed of the grey Ti-rich phase and
the white Ni-rich phase. The distribution of Si, Ti and
Ni along the white line in the photograph shows gradualFig. 2. SEM micrograph of the interface of SiC ceramic/reaction
products of ller No. SS-2.
Table 2
Composition of llers (atomic ratio) and results of SHS welding of SiC ceramic to itself
No. of ller Ni Ti Al C Percentage of C (at.%) Result of welding
SS-1 7 2 0.5 5.26 0
SS-2 2 5 0.5 6.67 0
SS-3 3 2 0.5 9.09 0
SS-4 2 3 0.5 9.09 0
SS-5 7 2 0.5 5.26 0SS-6 0.5 2 1 28.57 SS-7 3 2 0.5 9.09 0
SS-8 2 3 0.5 9.09 0
Table 1
Composition of FGM welding materialsa
Reaction layer Second layer Ignition layer
Composition Ti Ti1C1 20Ni Ti1C1 40Ti1Ni1Weight of powders (g) 0.03 0.5 0.5
a Note: Ti1C1 20Ni denotes that the atomic ratio Ti X C 1 X 1, the weight of Ti powder plus C powder is 80 wt% of the total mixed powders, theweight of Ni powder is 20 wt% of the total.
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changes at the interface, which indicates the presence of
a composition transition area (i.e., reacted layer) at the
interface. From the gure, one can also see that the
position of the composition transition area shifts to SiC
ceramic. The results show that the composition transi-
tion area forms mainly due to the diusion of Ti from
the ller to the ceramic. This is in accordance with the
fact that the diusion coecient of SiC is very small as
this chemical compound is dominated by covalent bond.
In addition, it can be seen that the grey Ti-rich phase
forms at the interface, indicating the precedent concen-
tration of Ti at the interface during welding. Therefore,
it can be concluded that the anity between Ti and SiC
is better than that between Ni and SiC.
For all the llers except No. SS-6 listed in Table 2, the
interdiusion takes place during SHS welding as the
llers contain sucient active elements.
3.2. SHS welding of SiC ceramic to Ni-based superalloy
3.2.1. Microstructure of interface
The microstructure of interfaces including the in-
terface of Ni-based superalloy/reaction products, the
interfaces between the dierent layers of the reaction
products and the interface of reaction products/SiC
ceramic is presented in Fig. 4. The microstructure
shows that the bonding at the interfaces is excellent,
especially at the interface of Ni-based superalloy/re-
action products and the interface of reaction products/
SiC ceramic.
The chemical composition of the 4 points a,b,c,d as
shown in Fig. 4(a) was analyzed by EDX, and the results
are listed in Table 3. The results clearly prove that the
components of the Ni-based superalloy, Cr, W and Mo,
remarkably diuse into the reaction products of the
ller.
Fig. 4. SEM micrographs of the interfaces (a) Ni-based superalloy/
FGM ller; (b) between dierent layers of FGM ller; (c) FGM ller/
SiC ceramic.
Fig. 3. SEM micrographs of the interface of SiC ceramic/reaction
products of ller No. SS-3 and the distribution of element (a) Si, (b) Ti,
(c) Ni.
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3.2.2. Result of SHS welding
As shown in Fig. 4, excellent bonding exists at the
interfaces within the total welded area. This result in-
dicates that the joining of SiC ceramic to Ni-based su-
peralloy has been realized by SHS welding. However, as
stated in Section 2, for the sake of convenience to in-
vestigate the interdiusion, interfacial reaction and mi-
crostructure, a simplied FGM ller was utilized, which
is not sucient for overcoming the thermal stress caused
by the mismatch between the thermal expansion coe-
cients of the welded dissimilar materials, leading to the
generation of microcracks in the ceramic near the in-
terface of SiC ceramic/reaction products of the ller.
The experiments to overcome the thermal stress using
FGM ller consisting of multi-layer together with other
measures are well under way.
4. Conclusions
1. The liquid phase formed in SHS reaction of theNi+Ti+C (less than 9 at.%) series llers can wet
SiC ceramic. The liquid can penetrate into the open
pores of the ceramic, forming mechanical bonding
between the ceramic and the reaction products after
solidication.
2. The liquid phase formed in SHS reaction of the series
llers reacts with SiC ceramic at the interface. This
interfacial reaction is realized mainly by the diusion
of Ti from the ller to the ceramic. Successful SHS
welding of SiC ceramic to itself has been achieved uti-
lizing this series llers.
3. The anity between Ti and SiC ceramic is better than
that between Ni and SiC ceramic.
4. SiC ceramic has been joined to Ni-based superalloy
by SHS welding with the simplied FGM ller. The
bonding at the interfaces is excellent. Interdiusion
takes place between the ller and the welded materi-
als.
Acknowledgements
The authors gratefully acknowledge the nancial
support of the project by the Aeronautical Science
Foundation of China and the National Natural Science
Foundation of China (Grant No. 59881001).
References
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Table 3
Composition at the interface of Ni-based superalloy/reaction products
of the ller (at%)
Position Ti Cr Ni Mo W
a 0.48 19.00 62.51 9.01 9.00
b 51.86 10.89 5.02 17.12 15.12c 72.92 12.94 5.34 4.43 4.37
d 90.70 2.13 2.77 2.43 1.97
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