The dissolution behavior of CaO-MgO-SiO2 glass fiber was investigated by scanning electron microscopy （SEM）, Fourier-transform infrared spectrometer （FTIR） and inductively coupled plasma atomic emission spectrosco...The dissolution behavior of CaO-MgO-SiO2 glass fiber was investigated by scanning electron microscopy （SEM）, Fourier-transform infrared spectrometer （FTIR） and inductively coupled plasma atomic emission spectroscopy （ICP-AES） using in-vitro tests. The results show that the soaked fiber is surrounded by an outer calcium-magnesium silicate hydrated layer, and there exists a balancing fimction between the formation and abscission of the hydrated layer during the dissolution process. The concentrations of leached ions increase constantly, and the mass loss of the fibers and pH changes of the solution are found to rise rapidly during the initial dissolution process, then their increasing rates are controlled by the balancing function of the hydrated layer at the subsequent dissolution stages. The dissolution rate constant and time for complete dissolution are estimated to be 274 ng/（cm2.h） and 15.2 d, respectively, presenting preferable biosolubilities.展开更多
Calcium-magnesium-alumina-silicate (CMAS) corrosion is an important cause for thermal barrier coating (TBC) failure,which has attracted increased attentions.In this study,some thermal barrier coating (TBC) materials i...Calcium-magnesium-alumina-silicate (CMAS) corrosion is an important cause for thermal barrier coating (TBC) failure,which has attracted increased attentions.In this study,some thermal barrier coating (TBC) materials including YSZ (yttria partially stabilized zirconia),GdPO_(4),and LaPO_(4) were prepared into bulks,and the effects of their surface roughness on wettability and spreading characteristics of molten CMAS were investigated.As-fabricated and polished bulks with different surface roughness were exposed to CMAS corrosion at 1250 ℃ for 1 and 4 h,following by macro and micro observations.Results revealed that compared with the as-fabricated bulks,molten CMAS on the polished samples had lower wettability and a smaller spreading area,mainly attributable to the reduced capillary force to drive the melt spreading.Meanwhile,GdPO_(4) and LaPO_(4) bulks exhibited lower CMAS wettability than YSZ bulk.It is thus considered that reducing the surface roughness is beneficial to CMAS corrosion resistance of TBCs.展开更多
Calcium-magnesium-alumino-silicate(CMAS)corrosion is a critical factor which causes the failure of thermal barrier coating(TBC).CMAS attack significantly alters the temperature and stress fields in TBC,resulting in th...Calcium-magnesium-alumino-silicate(CMAS)corrosion is a critical factor which causes the failure of thermal barrier coating(TBC).CMAS attack significantly alters the temperature and stress fields in TBC,resulting in their delamination or spallation.In this work,the evolution process of TBC prepared by suspension plasma spraying(SPS)under CMAS attack is investigated.The CMAS corrosion leads to the formation of the reaction layer and subsequent bending of TBC.Based on the observations,a corrosion model is proposed to describe the generation and evolution of the reaction layer and bending of TBC.Then,numerical simulations are performed to investigate the corrosion process of free-standing TBC and the complete TBC system under CMAS attack.The corrosion model constructs a bridge for connecting two numerical models.The results show that the CMAS corrosion has a significant influence on the stress field,such as the peak stress,whereas it has little influence on the steady-state temperature field.The peak of stress increases with holding time,which increases the risk of the rupture of TBC.The Mises stress increases nonlinearly along the thick direction of the reaction layer.Furthermore,in the traditional failure zone,such as the interface of the top coat and bond coat,the stress obviously changes during CMAS corrosion.展开更多
During flight,many silicates(sand,dust,debris,fly ash,etc.)are ingested by an engine.They melt at high operating temperatures on the surface of thermal barrier coatings(TBCs)to form calcium-magnesium-aluminum-silicate...During flight,many silicates(sand,dust,debris,fly ash,etc.)are ingested by an engine.They melt at high operating temperatures on the surface of thermal barrier coatings(TBCs)to form calcium-magnesium-aluminum-silicate(CMAS)amorphous settling.CMAS corrodes TBCs and causes many problems,such as composition segregation,degradation,cracking,and disbanding.As a new generation of TBC candidate materials,rare-earth zirconates(such as Sm_(2)Zr_(2)O_(7))have good CMAS resistance properties.The reaction products of Sm_(2)Zr_(2)O_(7) and CMAS and their subsequent changes were studied by the reaction of Sm_(2)Zr_(2)O_(7) and excess CMAS at 1350℃.After 1 h of reaction,Sm_(2)Zr_(2)O_(7) powders were not completely corroded.The reaction products were Sm-apatite and c-Zr0_(2) solid solution.After 4h of reaction,all Sm_(2)Zr_(2)O_(7) powders were completely corroded.After 24 h of reaction,Sm-apatite disappeared,and the c-Zr02 solid solution remained.展开更多
基金Projects(50872098, 51004080) supported by the National Natural Science Foundation of ChinaProject(B0903) supported by the Opening Fund of Research Center of Green Manufacturing and Energy-saving & Emission Reduction Technology of Wuhan University of Science and Technology, China
文摘The dissolution behavior of CaO-MgO-SiO2 glass fiber was investigated by scanning electron microscopy （SEM）, Fourier-transform infrared spectrometer （FTIR） and inductively coupled plasma atomic emission spectroscopy （ICP-AES） using in-vitro tests. The results show that the soaked fiber is surrounded by an outer calcium-magnesium silicate hydrated layer, and there exists a balancing fimction between the formation and abscission of the hydrated layer during the dissolution process. The concentrations of leached ions increase constantly, and the mass loss of the fibers and pH changes of the solution are found to rise rapidly during the initial dissolution process, then their increasing rates are controlled by the balancing function of the hydrated layer at the subsequent dissolution stages. The dissolution rate constant and time for complete dissolution are estimated to be 274 ng/（cm2.h） and 15.2 d, respectively, presenting preferable biosolubilities.
基金This research is sponsored by the National Natural Science Foundation of China(Grant No.51971156).
文摘Calcium-magnesium-alumina-silicate (CMAS) corrosion is an important cause for thermal barrier coating (TBC) failure,which has attracted increased attentions.In this study,some thermal barrier coating (TBC) materials including YSZ (yttria partially stabilized zirconia),GdPO_(4),and LaPO_(4) were prepared into bulks,and the effects of their surface roughness on wettability and spreading characteristics of molten CMAS were investigated.As-fabricated and polished bulks with different surface roughness were exposed to CMAS corrosion at 1250 ℃ for 1 and 4 h,following by macro and micro observations.Results revealed that compared with the as-fabricated bulks,molten CMAS on the polished samples had lower wettability and a smaller spreading area,mainly attributable to the reduced capillary force to drive the melt spreading.Meanwhile,GdPO_(4) and LaPO_(4) bulks exhibited lower CMAS wettability than YSZ bulk.It is thus considered that reducing the surface roughness is beneficial to CMAS corrosion resistance of TBCs.
基金This study is supported by the National Natural Science Foundation of China(Nos.1171101165 and 11902240).
文摘Calcium-magnesium-alumino-silicate(CMAS)corrosion is a critical factor which causes the failure of thermal barrier coating(TBC).CMAS attack significantly alters the temperature and stress fields in TBC,resulting in their delamination or spallation.In this work,the evolution process of TBC prepared by suspension plasma spraying(SPS)under CMAS attack is investigated.The CMAS corrosion leads to the formation of the reaction layer and subsequent bending of TBC.Based on the observations,a corrosion model is proposed to describe the generation and evolution of the reaction layer and bending of TBC.Then,numerical simulations are performed to investigate the corrosion process of free-standing TBC and the complete TBC system under CMAS attack.The corrosion model constructs a bridge for connecting two numerical models.The results show that the CMAS corrosion has a significant influence on the stress field,such as the peak stress,whereas it has little influence on the steady-state temperature field.The peak of stress increases with holding time,which increases the risk of the rupture of TBC.The Mises stress increases nonlinearly along the thick direction of the reaction layer.Furthermore,in the traditional failure zone,such as the interface of the top coat and bond coat,the stress obviously changes during CMAS corrosion.
基金supported by the National Natural Science Foundation of China(No.5177020526).
文摘During flight,many silicates(sand,dust,debris,fly ash,etc.)are ingested by an engine.They melt at high operating temperatures on the surface of thermal barrier coatings(TBCs)to form calcium-magnesium-aluminum-silicate(CMAS)amorphous settling.CMAS corrodes TBCs and causes many problems,such as composition segregation,degradation,cracking,and disbanding.As a new generation of TBC candidate materials,rare-earth zirconates(such as Sm_(2)Zr_(2)O_(7))have good CMAS resistance properties.The reaction products of Sm_(2)Zr_(2)O_(7) and CMAS and their subsequent changes were studied by the reaction of Sm_(2)Zr_(2)O_(7) and excess CMAS at 1350℃.After 1 h of reaction,Sm_(2)Zr_(2)O_(7) powders were not completely corroded.The reaction products were Sm-apatite and c-Zr0_(2) solid solution.After 4h of reaction,all Sm_(2)Zr_(2)O_(7) powders were completely corroded.After 24 h of reaction,Sm-apatite disappeared,and the c-Zr02 solid solution remained.
