Ni3Al基合金IC6的NiCrA1Y（Si）包覆型涂层研究

研究了磁控溅射NiCrA1Y(Si)包覆型涂层对Ni3A1基合金IC6的抗氧化性能及力学性能的影响，同时也研究了该涂层的微观组织及其稳定性。结果表明，研制的NiCrA1Y(Si)物理沉积包覆型涂层是适合于IC6合金及其使用条件的防护涂层。     

适用于Ni3Al基合金IC6的NiCoCrAlY涂层研究

为了研制适用于IC6合金的NiCoCrAlY包覆涂层，采用离子电弧镀方法在Ni3Al基合金IC6上涂覆了NiCoCrAlY 5元包覆涂层，测试了涂覆涂层后IC6合金的主要力学性能和抗氧化抗腐蚀性能．结果表明，NiCoCrAlY涂层主要由γ(Ni)、γ′(Ni3Al)、β(NiAl)和α-Cr组成，可使IC6合金的抗氧化抗腐蚀性能得到明显改善，而且对IC6合金的主要力学性能无明显影响，是IC6合金一种较为理想的防护涂层。     

电弧离子镀制备NiCrAlY涂层及其抗高温氧化性能

为提高高温合金材料抗高温氧化性能,利用真空阴极电弧离子镀在DZ22B高温合金上沉积Ni Cr Al Y涂层,研究涂层的抗高温氧化性能。采用扫描电镜观察膜层表面和截面形貌,化学容量法测试膜层成分,X射线衍射仪分析涂层的物相组成,万能试验机检测涂层结合力。结果表明:所制备的Ni Cr Al Y涂层厚度约50μm,涂层致密且与基体结合良好;涂层成份除Al元素有所损失外基本与靶材一致。Ni Cr Al Y涂层主要相为γ′-Ni3Al/γ-Ni,同时含有少量的β-Ni Al相。在1050℃高温下,Ni Cr Al Y涂层表面形成致密的氧化铝层有助于减缓氧化速度,对基材起到良好的保护作用;涂层失效的主要方式是随着氧化的进展,氧化层产生裂纹并剥落,新的表面被氧化,剥落和被氧化往复进行,直至涂层失效。     

地面燃机涡轮叶片和导向叶片涂层的应用EI

介绍了国外燃用低质柴油的地面燃机一级涡轮叶片及导向叶片防护涂层的抗腐蚀性能 ,肯定了高 Cr- MCr Al X (M=Ni、 Co、 Ni Co,X=Y、 Si、 Hf)涂层防护效果。     

高速电弧喷涂FeNiCr/Ni包覆Cr3C2涂层组织和性能的研究

通过常温超声波辅助化学镀方法制备Ni包覆Cr3C2陶瓷粉体,以其作为增强相的粉芯材料通过高速电弧喷涂制备FeNiCr/Ni包覆Cr3C2涂层.采用光学显微分析、场发射扫描电镜分析(FE-SEM)、能谱分析(EDS)以及显微硬度测试方法,研究Ni包覆Cr3C2陶瓷粉体对涂层组织结构及性能的影响.试验结果表明:Ni包覆Cr3C2陶瓷粉体能改善涂层中各相之间的结合状态,显著减少涂层的氧化物和孔隙率,并提高涂层与基体的结合强度、抗热震性和抗高温冲蚀性能.     

溅射Ni11Co26Cr6Al0.5Y涂层对镍基合金在1000 ℃氧化行为的影响

通过对有/无Ni11Co26Cr6Al0.5Y涂层镍基合金在1000℃进行氧化动力学曲线测定,及组织结构观察,研究了Ni11Co26Cr6Al0.5Y涂层对镍基合金高温氧化行为的影响。结果表明:高温氧化期间,合金发生外氧化和内氧化,外氧化层由NiO、NiCrO_4、CoWO_4构成,中间氧化物由TiO_2、Al_2O_3、NiWO_4构成,中间层氧化物层抑制了基体中Al元素向外扩散,形成平直连续的Al_2O_3内氧化物层;合金氧化动力学曲线呈现起伏波动的特征。镍基合金经溅射Ni11Co26Cr6Al0.5Y涂层,可有效改善合金的抗氧化性能;涂层的氧化动力学曲线仅在氧化初期有轻微增重而后趋于平稳,遵循抛物线规律,其形成的Al_2O_3氧化膜未发生明显剥落,仅在涂层内及近涂层/基体界面区域存在少量Al_2O_3内氧化物。     

铬(Cr)添加量对真空粉末熔覆镍铬-碳化铬(NiCr-Cr_3C_2)复合涂层微观组织的影响

采用高温真空粉末熔覆工艺在镍基高温合金表面制备了Cr改善的Ni Cr-Cr_3C_2复合涂层,涂层与基体形成冶金结合。通过添加不同含量(0%,10%,20%,30%(质量分数))的Cr粉末,研究了Cr含量对涂层微观组织,相组成及界面扩散的影响。结果表明,Cr的添加促进了涂层中硅(Si)元素的消耗并形成Cr3Si,同时抑制了界面处脆性相Ni3Si的产生。随着Cr添加量的增多,二次反应区厚度及界面处的Ni3Si含量均相应减少。     

Al(Ni)含量对钛合金激光熔覆AlNiMoSi复合涂层摩擦学性能的影响

研究含Al、Si元素涂层的摩擦学性能可为其应用提供重要的理论参考。以Al、Ni、Mo、Si粉末为原料,采用激光熔覆技术在Ti6Al4V合金表面制备了Al质量分数分别为20%(Ni的为40%),30%(Ni的为30%),40%(Ni的为20%)的AlNiMoSi复合涂层,分别命名为20Al、30Al、40Al复合涂层。采用XRD、SEM和EDS分析了涂层的物相和显微组织,并测试了复合涂层的干滑动磨损性能。结果表明:20Al、30Al和40Al复合涂层的平均摩擦系数和磨损率分别为0.380,0.258,0.325和9.36×10~(-5),8.43×10~(-5),1.05×10~(-4)mm~3/(N·m),30Al复合涂层的磨损性能最好,主要是因为该涂层中TiC和Ti3Al含量较高;20Al和40Al复合涂层的磨损机理主要为黏着磨损和磨粒磨损,30Al复合涂层的磨损机理主要为轻微的磨粒磨损。     

NiCoCrAIY（Si）梯度涂层对Ni3Al基单晶合金IC6SX抗氧化性能的影响

采用超音速火焰喷涂的方法在Ni3Al基单晶合金IC6SX上涂覆了NiCoCrAlYSi／NiCoCrAlY梯度涂层,研究了涂层对IC6SX合金1100℃抗氧化性能的影响。利用扫描电镜、X射线衍射等手段观察了氧化试样的微观结构,分析了氧化产物的成分及涂层氧化前后的相组成变化。结果表明：涂层表面形成了致密的氧化膜,氧化膜由内外两层组成,内层主要由Al2O3组成,外层主要由NiAl2O4及少量的Cr2O3组成;涂层有效地控制了Mo元素的扩散氧化,对IC6SX合金的抗氧化性能有明显改善。     

NiCoCrAlY(Si)梯度涂层对Ni3Al基单晶合金IC6SX抗氧化性能的影响

采用超音速火焰喷涂的方法在Ni3Al基单晶合金IC6SX上涂覆了NiCoCrAlYSi/NiCoCrAlY梯度涂层,研究了涂层对IC6SX合金1100℃抗氧化性能的影响.利用扫描电镜、X射线衍射等手段观察了氧化试样的微观结构,分析了氧化产物的成分及涂层氧化前后的相组成变化.结果表明:涂层表面形成了致密的氧化膜,氧化膜由内外两层组成,内层主要由Al2O3组成,外层主要由NiAl2O4及少量的Cr2O3组成;涂层有效地控制了Mo元素的扩散氧化,对IC6SX合金的抗氧化性能有明显改善.     

Ni_3Al－Mo金属间化合物的高温腐蚀与表面防护研究

研究了ＩＣ６合金的抗氧化、耐腐蚀性能。针对可能的实用背景，探讨了ＩＣ６合金的表面防护问题。溅射ＮｉＣｒＡｌＹ涂层可通过在表面形成保护性的Ａｌ＿２Ｏ＿３膜而使合金获得优异的抗高温氧化、热腐蚀性能，同时也不损害基材的力学性能。     

Phase constituents and thermal expansion behavior of a NiCrAlYRe coating alloy

Phase constituents and properties of MCrAlY coating alloys play a crucial role in determining the performance of MCrAlY stand-alone overlay coatings and thermal barrier coating systems. Recent advances in computer modeling including access to involved thermodynamic databases make it possible to predict phase stabilities in these alloy systems. This article investigates the phase stabilities of a NiCrAlY coating alloy containing Re both experimentally and thermodynamically. The addition of Re promotes the formation of the Cr-rich α-phase that owns low coefficient of thermal expansion (CTE), and thereby decreases the CTE of the NiCrAlYRe coating alloy. In addition, the martensitic transformation of the B2 β-NiAl phase is investigated. This transformation has an important influence on the microhardness of the β-NiAl phase.     

磁控溅射沉积NiCrAlY涂层中的氩及其对氧化行为的影响

用直流磁控溅射沉积NiCrAlY涂层。发现使用较高的负偏压时,涂层中掺有氩,其含量与负偏压的立方成正比。用SEM和TEM观察,发现高偏压下沉积的涂层中有微孔和微裂纹。因此,过高的负偏压导致涂层的氩含量激增,以至严重降低涂层的周期氧化性能。     

Powder Microstructure and Overlay Coating Property ofNiCrAlY Alloy

The microstructural features of NiCrAlY alloy powders with different particle size fractions and their effects on the overlay coating property have been investigated. It is shown that the finer (20~30 μm) powder particles experience rapid recalescence and heat extraction to the surroundings resulting in microcellular structure, whereas the coarser (40~50μm) powder particles exhibit a coarse cellular and dendritic mixed structure because of recalescence followed by slow cooling.In addition, it is also indicated that the finer the powder particle sizes, the higher the mechanical property and the metallurgical thermal stability of the overlay coatings deposited by as-atomized powders, which is presumably attributed to the formation of dense fine grain Structure and oxide layer for the fine size fraction of the powders.     

Application of fracture mechanics tofailure analysis and to residual life assessment of components operating at high temperatures

Abstract

MCrAlY overlay coatings have been successfully used as a means of improving the oxidation performance of gas turbine blades operating at elevated temperatures. However, depletion of aluminium can limit the ability of such coatings to form a protective oxide layer should spallation of the original α-Al₂O₃ oxide layer occur under thermal cycling conditions. It is the objective of the current research to evaluate the potential of NiAl₃ as a reservoir phase for a NiCrAlY overlay coating on a IN738LC superalloy substrate at 1,100°C in air. The morphologies and microstructures of the conventional NiCrAlY and NiAl3-modified NiCrAlY overlay coatings in the as-sprayed and oxidised conditions were characterised using SEM, EDX and XRD techniques.     

Microstructure and composition evolution of a single-crystal superalloy caused by elements interdiffusion with an overlay NiCrAlY coating on oxidation

MCrAlY(M=Ni and/or Co) overlay coating is widely used as a protective coating against high temperature oxidation and corrosion. However, due to its big difference in chemical composition with the underlying superalloy, elements interdiffusion occurs inevitably. One of the direct results is the formation of interdiffusion zone(IDZ) and secondary reaction zone(SRZ) with a high density of fine topological closed-packed phases(TCPs), weakening dramatically the mechanical properties of the alloy substrate. It is by now the main problem of modern high-temperature metallic coatings, but there are still hardly any reports studying the formation, growth and transformation of IDZ and SRZ in deep, as well as the precipitation of TCPs.In this work, a typical NiCrAlY coating is deposited by arc ion plating on a single-crystal superalloy N5.Elements interdiffusion between them and its relationship on microstructure were clarified. Cr rather than Al from the coating diffuses into the alloy at high temperatures and segregates immediately beneath their interface, contributing largely to the formation of IDZ. Simultaneously, diffusion of Ni from the deep alloy to IDZ leads to the formation and continuous expansion of SRZ.     

Titania-carbon nanotubes nanocomposite coating on Mg alloy: microstructural characterisation and mechanical properties

Atmospheric plasma spraying was carried out to deposit a bilayered NiCrAlY/nTiO₂-CNT composite coating. Initially, NiCrAlY, as an under-layer with a thickness of around 100?µm, was deposited. Afterwards, nanostructured TiO₂ (nTiO₂), as an over-layer with a thickness of 135?μm, was deposited with and without the incorporation of carbon nanotubes (CNTs) on the Mg alloy surface. In contrast to NiCrAlY and NiCrAlY/nTiO₂, the NiCrAlY/nTiO₂-CNT nanocomposite coating displayed a higher bonding strength. The wear behaviour of the coatings was examined by the pin-on-disc test and the results revealed that the incorporation of CNTs into the nTiO₂ coating considerably enhanced the tribological behaviour of Mg alloy due to the CNT’s bridging mechanism.     

An in-situ formed ceramic/alloy/ceramic sandwich barrier to resist elements interdiffusion between NiCrAlY coating and a Ni-based superalloy

NiCrAlY coatings are widely applied on various alloy components to enhance oxidation and/or corro-sion resistance at high temperatures.However,elements interdiffusion occurs between them due to composition difference.Although various diffusion barriers(DBs)are reported,this problem is still far from completely solved as most ceramic barriers suffer from poor adherence,while the metallic barriers play a limited role.In this study,NiCrAlY coating was deposited onto a second-generation single-crystal superalloy by arc ion plating.A novel simple method is provided to address elements interdiffusion.By pre-oxidation at a moderate temperature,a thin scale of Ni(Co)O forms at the alloy surface.It transforms to be an alumina/NiCoCr alloy/alumina sandwich by an in-situ reaction with the overlaying NiCrAlY coat-ing and the alloy substrate at high service temperatures,which offers good barrier ability in conjunction with strong adhesion.In the presence of such an alumina/alloy/alumina DB,the NiCrAlY coating provides high resistance to oxidation and scale spallation for the alloy substrate.     

TiAl合金表面TiAlCrY/YSZ涂层高温长时间服役性能

TiAl合金具有低密度、高比强度的优异性能,是一种潜在的航空发动机用结构材料。TiAl合金的服役温度范围为700～900℃,在其表面制备高温热防护涂层可以进一步提高服役温度。本研究采用等离子喷涂技术在TiAl合金表面制备了新型TiAlCrY/YSZ涂层,并与传统的NiCrAlY/YSZ热障涂层进行高温长时间服役性能对比研究。结果发现, TiAlCrY/YSZ涂层在1100℃空气环境中服役300 h保持完好,表现出良好的高温性能,而NiCrAlY/YSZ涂层在1100℃的服役寿命不足100 h。显微分析结果表明, TiAlCrY黏结层表面会形成一层连续且致密的TGO,其主要成分为Al2O3,与YSZ涂层的界面兼容性良好。并且TGO在1100℃空气环境中服役300 h后,厚度仍<8μm。以上研究表明,与传统NiCrAlY/YSZ热障涂层相比, TiAlCrY/YSZ更适合作为TiAl合金表面的高温热防护涂层。     

掺杂纳米CeO2对ZrO2-Y2O3热障涂层隔热性能的影响

以纳米ZrO₂-8 wt%Y₂O₃(YSZ)和在纳米ZrO_2-8wt%Y₂O₃中分别掺杂25wt%和50wt%纳米CeO₂团聚处理后作为隔热层材料,NiCrAlY(Ni-25Cr-5Al-0.5Y,wt %)作为粘结层材料,用等离子喷涂(APS)方法在GH30高温合金表面制备三种材料体系的热障涂层(TBC) 。通过扫描电镜(SEM)和X射线衍射仪(XRD)对掺杂了25wt%纳米CeO₂涂层的微观组织结构进行分析研究,测定了三种材料涂层在室温和 300、500、700℃时的热导率,并在相同边界条件下测试了它们的隔热性能。结果表明：掺杂纳米CeO₂涂层组成相为稳定的t相(t-ZrO₂、t-Zr_0.82Y_0.18O_1.91、t-Zr_0.82Ce_0.18O₂)和c相(c-CeO₂) , 涂层中存在闭合的孔隙和微裂纹;掺杂纳米CeO₂能够降低涂层的热导率,并且隔热性能随CeO₂含量的增加而提高。对于 400μm厚的CeO₂/ZrO₂-Y₂O₃涂层(CYZ , 掺杂25wt%CeO₂)对基体产生的温降比纳米YSZ涂层提高了10.7%,当CeO₂的含量从25wt%提高到50wt%时,隔热性能也提高了7.1%。