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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.

    PII: S 0 2 6 3 - 4 3 6 8 ( 0 0 ) 0 0 0 0 8 - 1

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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.

    34 S. Li et al. / International Journal of Refractory Metals & Hard Materials 18 (2000) 3337

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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.

    S. Li et al. / International Journal of Refractory Metals & Hard Materials 18 (2000) 3337 35

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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

    [1] Nicholas, MG. Joining Structural Ceramics, In: Peteves SD,

    editors, Designing Interfaces for Technological Applications:

    CeramicCeramic, CeramicMetal Joining. Amsterdam: Elsevier,

    1991, p. 49.

    [2] Yi HC, Moore JJ. Review self-propagating high-temperature

    (combustion) synthesis(SHS) of powder-compacted materials.

    Journal of Materials Science 1990;25:115968.

    [3] Orling TT, Messler RW, Jr., Fundamentals of the SHS joining

    process. In: Carim AH, Schwartz DS, Silberglitt RS. editors,

    Proceedings of the 1993 MRS Symposium on Joining and

    Adhesion of Advanced Inorganic Materials, MRS, Pittsburgh,

    1993;314:17783.

    [4] Messler RW, Jr., Zurbuchen MA, Orling TT, Welding with self-

    propagating high-temperature synthesis. Welding Journal Oct.

    1995, 3741.

    [5] Rabin BH. A Review of Silicon Carbide/Metal Interactions with

    Relevance to Silicon Carbide Joining, EGG-MS-9633, DE91

    012768, EG&G Idaho Falls, ID 83415, 1991.

    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

    S. Li et al. / International Journal of Refractory Metals & Hard Materials 18 (2000) 3337 37