Thermal barrier coating ( TBC) consisting of a NiCoCrAlY bond coat ( BC) and a ZrO2-8 wt. % Y2O3 topcoat ( TC) was fabricated on the nickel-base superalloy by air plasma spray ( APS) . The BC was treated by supersonic...Thermal barrier coating ( TBC) consisting of a NiCoCrAlY bond coat ( BC) and a ZrO2-8 wt. % Y2O3 topcoat ( TC) was fabricated on the nickel-base superalloy by air plasma spray ( APS) . The BC was treated by supersonic fine particle bombarding ( SFPB) . Thermal cyclic failure and residual stress in thermally grown oxide ( TGO) scale were studied by SEM with EDS and ruby fluorescence spectroscopy ( RFS) . As shown in the results,after treated by SFPB,thickening of TGO was relatively slow,which reduced the level of growth stress. The TBC with SFPB treatment was still remained well undergoing 350 times of thermal cycle. However,after thermal cycle with the same times,the separation of TC was observed in TBC without SFPB treatment. The residual stress analysis by RFS showed that the residual stress of SFPB-treated TBC increased with the increasing number of thermal cycle. The residual stress of conventional TBC reached a value of 650 MPa at 350 times of cycle and that of SFPB-treated TBC only reached 532 MPa at 400 times of cycle. The BC with SFPB treatment after 400 times of cycle was analyzed by RFS,the high stress value was not observed in local thickened region of TGO. Thermal cycling resistance of TBC can be improved by the SFPB technology.展开更多
Thermally Grown Oxide（TGO） is a dominating component in controlling the effectiveness of thermal barrier coating.During the growth of TGO,whether we could homogeneously distribute Al atom on the TGO and the intermed...Thermally Grown Oxide（TGO） is a dominating component in controlling the effectiveness of thermal barrier coating.During the growth of TGO,whether we could homogeneously distribute Al atom on the TGO and the intermediate metal layer will be the key factor in forming TGO with continuous,uniform and single-ingredient（Al2O3）.In this experiment,we bombarded particles on to the metallic bound layer.We studied the influence of supersonic particle bombardment on the diffusion of Al.We hope to control the growth of TGO by monitoring the diffusion of Al.Thermal barrier coating（TBC）,which consists of a NiCoCrAlY bond coat and a ZrO2-8Y2O3（wt.%） topcoat（TC）,is fabricated on the nickel-base superalloy by air plasma spray（APS）.NiCoCrAlY bond coat is treated by supersonic fine particles bombarding（SFPB）.The morphology,oxidation behavior of TBC and phase are characterized by scanning electron microscope（SEM） equipped with an energy dispersive spectromrter（EDS） and X-ray diffractometer（XRD）.The influence of supersonic fine particles bombarding technique on the service life of thermal barrier coating is studied.The results show that SFPB technique improves the flaw of excessive surface undulation in the as-sprayed bond coat.A continuous,uniform and single-ingredient（Al2O3） TGO can quickly form in the SFPB TBC during high temperature oxidation process.The thickening of TGO is relatively slow.These will effectively suppress the formation of other non-protective oxides.Therefore,SFPB technique reduces the growth stress level generated by the continuous growth of TGO,and also avoids the stress concentration induced by formation of the large particle spinal oxide.Thermal barrier coating still remains well after 350 thermal cycles.The service life of TBC is improved.The proposed research provides theoretical basis and technical references to further improve and enhance the SFPB technique.展开更多
采用超音速微粒轰击技术（Supersonic Fine Particles Bombarding，SFPB）对调质态合金钢38CrSi进行表面纳米化处理；利用X射线衍射、扫描电镜、透射电镜等分析技术研究不同工艺条件下表面纳米化层的微观组织结构特征。结果表明：经SFP...采用超音速微粒轰击技术（Supersonic Fine Particles Bombarding，SFPB）对调质态合金钢38CrSi进行表面纳米化处理；利用X射线衍射、扫描电镜、透射电镜等分析技术研究不同工艺条件下表面纳米化层的微观组织结构特征。结果表明：经SFPB处理后，材料表层组织严重细化，并形成了纳米结构层（晶粒尺寸〈100nm），随处理时间的延长，最表面纳米晶的尺寸变化不大，纳米结构层的厚度有所增加；当处理时间为240s时，在最表面层形成了平均晶粒尺寸约为16nm的具有随机取向的等轴纳米晶。纳米结构层的晶粒尺寸随着距表面距离的增加而增大。在距表面约25μm处，存在着大量的由位错线和高密度的位错缠结分割的胞块，尺寸为80～100nm；分析表明位错运动是表面纳米化的主要原因。展开更多
基金Sponsored by the National Natural Science Foundation of China ( Grant No 60879018)
文摘Thermal barrier coating ( TBC) consisting of a NiCoCrAlY bond coat ( BC) and a ZrO2-8 wt. % Y2O3 topcoat ( TC) was fabricated on the nickel-base superalloy by air plasma spray ( APS) . The BC was treated by supersonic fine particle bombarding ( SFPB) . Thermal cyclic failure and residual stress in thermally grown oxide ( TGO) scale were studied by SEM with EDS and ruby fluorescence spectroscopy ( RFS) . As shown in the results,after treated by SFPB,thickening of TGO was relatively slow,which reduced the level of growth stress. The TBC with SFPB treatment was still remained well undergoing 350 times of thermal cycle. However,after thermal cycle with the same times,the separation of TC was observed in TBC without SFPB treatment. The residual stress analysis by RFS showed that the residual stress of SFPB-treated TBC increased with the increasing number of thermal cycle. The residual stress of conventional TBC reached a value of 650 MPa at 350 times of cycle and that of SFPB-treated TBC only reached 532 MPa at 400 times of cycle. The BC with SFPB treatment after 400 times of cycle was analyzed by RFS,the high stress value was not observed in local thickened region of TGO. Thermal cycling resistance of TBC can be improved by the SFPB technology.
基金supported by National Natural Science Foundation of China (Grant No. 50575220)
文摘Thermally Grown Oxide（TGO） is a dominating component in controlling the effectiveness of thermal barrier coating.During the growth of TGO,whether we could homogeneously distribute Al atom on the TGO and the intermediate metal layer will be the key factor in forming TGO with continuous,uniform and single-ingredient（Al2O3）.In this experiment,we bombarded particles on to the metallic bound layer.We studied the influence of supersonic particle bombardment on the diffusion of Al.We hope to control the growth of TGO by monitoring the diffusion of Al.Thermal barrier coating（TBC）,which consists of a NiCoCrAlY bond coat and a ZrO2-8Y2O3（wt.%） topcoat（TC）,is fabricated on the nickel-base superalloy by air plasma spray（APS）.NiCoCrAlY bond coat is treated by supersonic fine particles bombarding（SFPB）.The morphology,oxidation behavior of TBC and phase are characterized by scanning electron microscope（SEM） equipped with an energy dispersive spectromrter（EDS） and X-ray diffractometer（XRD）.The influence of supersonic fine particles bombarding technique on the service life of thermal barrier coating is studied.The results show that SFPB technique improves the flaw of excessive surface undulation in the as-sprayed bond coat.A continuous,uniform and single-ingredient（Al2O3） TGO can quickly form in the SFPB TBC during high temperature oxidation process.The thickening of TGO is relatively slow.These will effectively suppress the formation of other non-protective oxides.Therefore,SFPB technique reduces the growth stress level generated by the continuous growth of TGO,and also avoids the stress concentration induced by formation of the large particle spinal oxide.Thermal barrier coating still remains well after 350 thermal cycles.The service life of TBC is improved.The proposed research provides theoretical basis and technical references to further improve and enhance the SFPB technique.
基金supported by the National Natural Science Foundation of China(Nos.U1804146,51801054,52111530068)the Program for Science and Technology Innovation Talents in Universities of Henan Province,China(No.17HASTIT026)+2 种基金the Foreign Experts Introduction Project of Henan Province,China(No.HNGD2020009)the Science and Technology Innovation Team of Henan University of Science and Technology,China(No.2015XTD006)the Academy of Finland(No.311934)。
文摘采用超音速微粒轰击技术（Supersonic Fine Particles Bombarding，SFPB）对调质态合金钢38CrSi进行表面纳米化处理；利用X射线衍射、扫描电镜、透射电镜等分析技术研究不同工艺条件下表面纳米化层的微观组织结构特征。结果表明：经SFPB处理后，材料表层组织严重细化，并形成了纳米结构层（晶粒尺寸〈100nm），随处理时间的延长，最表面纳米晶的尺寸变化不大，纳米结构层的厚度有所增加；当处理时间为240s时，在最表面层形成了平均晶粒尺寸约为16nm的具有随机取向的等轴纳米晶。纳米结构层的晶粒尺寸随着距表面距离的增加而增大。在距表面约25μm处，存在着大量的由位错线和高密度的位错缠结分割的胞块，尺寸为80～100nm；分析表明位错运动是表面纳米化的主要原因。
