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《热喷涂技术》2016,(3)
低压等离子喷涂纳米氧化锆热障涂层,具有独特的组织结构。纳米团聚颗粒在高温等离子射流中部分熔化后沉积到基体上,团聚颗粒能够保留部分纳米结构,形成一种以纳米晶为主的纳米-微米二元结构涂层,为热障涂层的制备提供了一种新的技术方案。YSZ涂层高温服役中,纳米晶粒容易烧结长大。本文通过向YSZ粉体中加入少量的纳米α-Al_2O_3,探讨其抑制YSZ热生长的机制。首先制备了YSZ-Al_2O_3纳米混合物团聚粉末,并借助低压等离子喷涂技术制备涂层。结果表明纳米晶区占主导地位,纳米晶区嵌有少量的微米晶粒。涂层经1400℃,10h热处理,微观组织结构分析表明,α-Al_2O_3的加入对YSZ晶粒热生长具有部分抑制作用。 相似文献
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热障涂层(thermal barrier coatings,TBCs)能有效的提高航空发动机热端部件的工作温度和使用寿命。目前应用最为广泛的热障涂层材料为氧化钇部分稳定氧化锆(yttria-stabilized zirconia,YSZ),该热障涂层材料在服役温度高于1200℃下会发生相变,严重影响航空发动机的使用寿命和服役安全,难以满足新一代航空发动机的服役要求。本文综述了新型热障涂层材料的研究现状,重点介绍了掺杂改性氧化钇部分稳定氧化锆、烧绿石或萤石结构材料、钙钛矿结构化合物、磁铅石矿结构化合物以及新型黏结层材料的研究进展和发展方向,并论述了热障涂层制备技术的方法原理和优缺点,最后对热障涂层材料和制备方法的发展趋势进行了展望。 相似文献
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重型发电燃气轮机低排放、高效率的发展目标,要求燃气轮机透平的进气温度不断提高。热障涂层作为保护金属热端部件的重要手段,是实现这一目标的关键技术之一。目前世界上最先进的J级燃气轮机的透平进口温度已经达到1600℃,热端部件表面温度超过1250℃,传统的YSZ热障涂层已经不能满足这一发展需求,因此迫切需要开发温度更高、热导率更低的新型热障涂层。本文对La_2(Zr_(0.7)Ce_(0.3))_2O_7(以下简称LZ7C3)热障涂层在重型发电燃气轮机中的应用进行了初步验证。结果表明,LZ7C3涂层具有比常规YSZ热障涂层更低的热导率(0.79~0.48Wm~(-1)K~(-1),相对传统YSZ涂层下降30%以上),且在1250℃的高温火焰台架试验中表现出优良的热循环寿命( 7370次),具有良好的应用前景。 相似文献
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为了研究YSZ粉末特性对热障涂层性能的影响,选择三种通过造粒烧结工艺制备的商用YSZ粉末,测试对比了粉末颗粒的各项性能,发现三种粉末仅致密度存在显著差异。在两种不同功率条件下采用等离子喷涂工艺利用三种YSZ粉末制备了热障涂层,观察了涂层的金相组织和断口形貌,测试了涂层孔隙率和结合强度,并采用电弧风洞考核了涂层的服役性能。研究结果表明,粉末致密度对涂层性能有显著影响,致密度高的YSZ粉末喷涂过程中熔融状态更好,涂层的孔隙率更低,结合强度更高;针对致密度低的粉末,增大喷涂功率可改善粉末的熔融状态,从而改善涂层的性能。经工艺调控制备的孔隙率和结合强度相近的涂层具有相当的隔热防护效果。 相似文献
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采用大气等离子喷涂(APS)技术制备了稀土元素掺杂量为19 mol.%的HfO2涂层,即Hf0.81Y0.19O1.905 (YSH19)/YSZ与Hf0.81Yb0.0475Y0.1425O1.905(YbYSH19)/YSZ双陶瓷层热障涂层,研究了其在1300℃下耐高温燃气热冲击性能。结果表明,两种热障涂层的隔热能力约为200℃,YbYSH19/YSZ体系热障涂层经280次燃气热冲击循环后涂层结构依然较为完整,性能显著优于YSH19/YSZ及YSZ热障涂层体系。涂层的失效模式为因中心区域处较大冲击载荷造成的涂层逐层剥落,以及边缘位置处轴向应力和剪切应力导致的涂层剥落。 相似文献
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等离子喷涂热障涂层技术广泛应用于航空发动机热端部件的高温防护。应用大气等离子喷涂法成功制备了纳米氧化铈氧化钇稳定的氧化锆(CYSZ)涂层,并与常规氧化钇稳定氧化锆(YSZ)涂层在1300℃下热处理10小时,研究高温对两种涂层性能的影响,与常规的YSZ涂层相比,CeO2的掺杂使涂层具有更高的稳定性。经过高温处理,CYSZ涂层的相结构没有发生明显变化。显微形貌结果表明,CYSZ涂层没有产生裂纹缺陷,涂层中纳米区域晶粒度随着温度的升高略有增大,这表明了纳米结构的CYSZ涂层具有更优异的高温稳定性。热循环氧化实验结果证明,CYSZ涂层具有更长的热循环寿命以及优异的高温抗氧化性能。 相似文献
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Al_2O_3等氧化物对YSZ热障涂层的高温使用性能有一定的影响。本文用HVOF喷涂Ni Co Cr Al Y合金粘结层,APS喷涂YSZ陶瓷面层,制备了Al_2O_3含量为0.01~0.64wt%的YSZ涂层。比较了不同Al_2O_3含量的YSZ涂层在1100℃下的热震性能和抗烧结性能,并探讨Al_2O_3对涂层的影响机理。结果表明相较于高纯YSZ涂层,随着涂层中Al_2O_3含量升高,涂层的抗热震性能降低,且Al_2O_3促进YSZ涂层的烧结。Al_2O_3含量在小于0.01wt%-0.12wt%区间内时,对涂层抗热震和抗烧结性能有显著影响,含量继续增加至0.64%时,对性能影响减缓。显微组织观察与EDS检测结果表明涂层中Al_2O_3并未在熔融颗粒界面处偏聚,但在颗粒内部有局部偏析。由此推测,含Al_2O_3的YSZ涂层热震失效的原因可能是Al_2O_3在YSZ颗粒内部偏析,并影响涂层的烧结性能,导致裂纹容易萌生和扩展。 相似文献
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Mohammadreza Daroonparvar Muhamad Azizi Mat Yajid Noordin Mohd Yusof Hamid Reza BakhsheshiRad Esah Hamzah Mohsen Nazoktabar 《中国稀土学报(英文版)》2014,32(10):989-1002
Phase transformation of tetragonal ZrO2 to monoclinic phase and also increment of bond coat oxidation kinetic(TGO thickening) can substantially restrict the life time of thermal barrier coating systems(TBCs). So, nanostructured and conventional Y2O3 stabilized ZrO2 coatings were evaluated in fused V2O5-Na2SO4 salts during thermal exposure in air. Microstructural characterization showed lower hot corrosion products(monoclinic zirconia, YVO4 crystals) formation and reduction of TGO thickness in thermal barrier coating system consisting of nanostructured Y2O3 stabilized ZrO2(YSZ) top coat. It was found that inhomogeneities, pores and micro-cracks played a principal role in the molten salts infiltration into the YSZ coating during three steps of hot corrosion process. In the nanostructured YSZ coating with tri-model structure, nano zones which surrounded by fully molten parts could fill the aforementioned defects and could act as barrier for the oxygen and corrosive molten salts penetration into the TBC. 相似文献
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采用等离子喷涂物理气相沉积 ( PS-PVD ) 技术开展了热障涂层梯度结构调控研究,通过调整喷涂送粉速率,
在底部、中间和顶部沉积阶段制备了五种不同的热障涂层,对热障涂层的显微组织、粗糙度、孔隙率、耐熔盐腐
蚀和耐粒子冲蚀性能进行表征,阐明了显微结构变化对热障涂层耐侵蚀性能的影响。研究表明:送粉速率的变化
对PS-PVD热障涂层羽柱状结构的沉积有显著的影响,低送粉速率下,涂层底部结构比较致密,当送粉速率增大时,
由于粉末颗粒在喷涂过程气化不充分,未熔粒子增加,羽柱状顶部结构趋向致密结构转变,涂层顶部孔隙率下降,
表面粗糙度降低。送粉速率由底至顶梯度递增制备的涂层表现出较高的耐熔盐腐蚀性能和耐粒子冲蚀性能。 相似文献
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Nanostructured yttria partially stabilized zirconia(YSZ) coatings were prepared by atmospheric plasma spraying(APS) using the conglomeration made by zirconia nanoparticle as the raw materials.The measurement methods,which consisted of scanning electron microscopy(SEM),transmission electron microscopy(TEM) and thermal cycling behavior,were used to character the morphology,composition and thermal oxidation behavior of the powder and the coatings.From the results,it was shown that the YSZ coating was the laminar structure,and the elements distribution in the bond and top coat were well-proportioned.The YSZ coatings were composed of fine grains with size ranging from 30 to 110 nm.The laminar layers with columnar grains were surrounded with unmelted parts of the nanostructured powder and some equiaxed grains.In the as-sprayed nanostructured zirconia coatings,there existed pores that were less than 1 μm.The cracks were observed on some of the crystal border.The cyclic oxidation experiment showed that the nanostructured coating had longer thermal cycling lifetime to exhibit the promising thermal cyclic oxidation resistance.The failure of the nanostructured TBC was similar to the failure of conventional APS TBC. 相似文献
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Thermal conductivity of (Sm1-xLax)2Zr2O7 (x=0, 0.25, 0.5, 0.75 and 1) oxides for advanced thermal barrier coatings 总被引:1,自引:0,他引:1
Pyrochlore oxides of general compositions, A2Zr2O7, where A is a 3+ cation (La to Lu), are promising candidate materials for ap-plications as high temperature thermal barrier coatings because of their high melting points, high thermal expansion coefficients, and low thermal conductivities. In this study, oxides of Sm2Zr2O7, (Sm0.75La0.25)2Zr2O7, (Sm0.5 La0.5)2Zr2O7, (Sm0.25La0.75)2Zr2O7 and La2Zr2O7 were prepared by solid reactions at 1600 ℃ for 10 h using Sm2O3, La2O3 and ZrO2 as the reactants. The phase compositions of these ceramic ma-terials were analyzed by X-ray diffractometer (XRD) and fourier transform infrared spectroscopy (FT-IR) methods, respectively. The micro-structure was observed by scanning electronl microscope (SEM). The thermal conductivities of these ceramic materials were measured using laser-flash method. XRD and FT-IR results showed that pure ceramic materials with pyrochlore structure were prepared successfully. SEM results indicated that microstructures of these ceramic materials were dense and grain boundaries were very clean. The La2O3 doped Sm2Zr2O7 pyrochlores (Sm0.75 La0.25)2Zr2O7 and (Sm0.5 La0.5)2Zr2O7 had lower thermal conductivity than the undoped Sm2Zr2O7. The thermal conductivity of (Sm0.25La0.75)2Zr2O7 was found to be lower than that of La2Zr2O7. The results showed that these ceramic materials had the poten-tial to be used as candidate materials for TBCs. 相似文献