Thermal Conductivity Measurement of an Electron-Beam Physical-Vapor-Deposition Coating

An industrial ceramic thermal-barrier coating designated PWA 266, processed by electron-beam physical-vapor deposition, was measured using a steady-state thermal conductivity technique. The thermal conductivity of the mass fraction 7 % yttria-stabilized zirconia coating was measured from 100 °C to 900 °C. Measurements on three thicknesses of coatings, 170 μm, 350 μm, and 510 μm resulted in thermal conductivity in the range from 1.5 W/(m·K) to 1.7 W/(m·K) with a combined relative standard uncertainty of 20 %. The thermal conductivity is not significantly dependent on temperature.     

用EB-PVD法制备Ti-AI／Nb层板复合材料的研究

采用电子束物理气相沉积（EB-PVD）技术，成功制备了0．2mm厚由24层Ti．Al和23层Nb交替叠加而成的Ti—AI／Nb层板复合材料，并采用扫描电子显微镜（SEM）等测试手段，对其物相组成和断口形貌等与Ti-Al单层材料进行了对比分析。结果表明，Ti—AI／Nb层板复合材料的界面明晰，层间距约为8gm；Ti-AI层由γ相和τ相组成，其成分呈梯度变化，且平均成分与原始铸锭的成分偏差较大，但未发现Ti-Al单层材料中看到的分层现象；Ti-AI／Nb层板复合材料具有比Ti-Al单层材料更好的韧性。     

Oxidation and lifetime of PYSZ and CeSZ coated Ni-base substrates with MCrAlY bond layers

Abstract

IN100 blades and CMSX-4 samples with NiCoCrAlY bond coats manufactured via LPPS and EB-PVD were cyclically tested in a burner rig at 1120°C and a furnace at 1100°C. Two different TBC chemistries were deposited by EB-PVD techniques: PYSZ and CeSZ. In all cases the performance of the CeSZ coated variances was superior to the PYSZ coated counterparts. TGO growth kinetics were slightly slower for the CeSZ coated samples. The benefits in lifetime are mainly attributed to the mixed zone oxides that tolerate spinel phase formation due to their ability to “wet” each other. Pore formation in the mixed zone is hereby suppressed favoring crack blunting mechanisms.     

基板温度对EB-PVD ZrO2涂层微观组织及残余应力的影响

采用电子束物理气相沉积(EB-PVD)技术在不锈钢基板上沉积ZrO2涂层.研究基板温度对涂层微观组织和残余应力的影响.结果表明:沉积的涂层均为t-ZrO2结构,涂层表面平整致密;随着基板温度的升高,涂层表面颗粒逐渐长大,表面粗糙度增大;涂层残余应力也随着基板温度的升高而增加,当基板温度为1000 ℃时,涂层残余应力的增量最大,ZrO2涂层的残余应力主要是由于涂层与基板热膨胀系数差别而产生的热应力引起.     

熔盐环境下热障涂层的等温热腐蚀行为研究

采用电子束物理气相沉积（EB-PVD）在镍基高温合金表面制备了YSZ/NiCoCrAlY双层结构热障涂层,研究了其在熔盐环境下的等温热腐蚀行为。结果表明,涂层在加热过程中发生相变引起体积收缩,导致涂层内部产生微裂纹。熔盐填充涂层内微裂纹和柱状晶间隙,降低了涂层的应变容限,引起涂层内应力升高。同时,熔盐促使热生长氧化层（TGO）碱性溶解,产生疏松多孔的氧化物层,导致TGO层加速增厚。在热应力作用下,疏松层氧化物破碎,最终导致涂层剥落。     

EB-PVD梯度热障涂层的制备及其热疲劳性能

采用ＥＢ－ＰＶＤ的方法,连续蒸发按一一分比混合的Ａｌ＋Ａ１２Ｏ３＋ＺｒＯ２混合源,在Ｎｉ基高温合金基体上制备了一种新型结构的热障涂层,ＳＥＭ和ＥＤＳ的观察、分析表明,这作层实现了由金属粘结层向陶资顶层的微观结构的梯度过渡和化学成分的连续变化。涂层的基本结构为ＮｉＣｏＣｒＡ１Ｙ／Ｎｉ３Ａｌ＋Ａ１２Ｏ３／Ａ１２Ｏ３ＺｒＯ２／ＺｒＯ２。这北度热障涂层在１０５０℃的抗高温氧化性能优于传统的二层结构的热障涂     

EB-PVD制备钛合金薄板渗铝相结构转变研究

对电子束物理气相沉积（EB-PVD）技术制备的钛合金薄板进行粉末包埋法渗铝，研究不同温度渗铝后的相结构转变规律。结果表明：制备态合金薄板相结构为Ti和Ti3Al，材料组织致密均匀，X射线衍射峰发生宽化，具有不对称性。在较低温度（600℃和620℃）渗铝后薄板两边的相结构变为Al3Ti相，但薄板的中心部位仍然为制备态的Ti3Al相，两边的Al3Ti组织和中心部位的Ti3Al组织都很均匀致密。在两相之间，存在清晰、平整的界面。在较高温度（700℃）渗铝后薄板的相结构为A13Ti，此时整个板材都被渗穿，组织均匀致密，并在局部小区域内出现铝元素的富集。     

复合喷丸强化对EB-PVD制备的CoCrAlY涂层的高温氧化性能的影响

为了研究复合型的高能喷丸工艺对EB-PVD制备的CoCrAlY涂层的高温氧化性能,采用0.3N、0.3N+0.1N和0.3N+0.2N的喷丸强度对CoCrAlY涂层进行了表面强化。观察了喷丸强化前后涂层的表面形貌;测量了喷丸前后涂层的表面粗糙度、表面残余应力、涂层的厚度和截面硬度;对比分析了喷丸前后涂层物相变化以及涂层高温氧化性能。研究结果表明：复合喷丸强化比普通高能喷丸强化对EB-PVD制备的CoCrAlY涂层的抗高温氧化性能提升更加明显,0.3N+0.1N的复合喷丸工艺对提升涂层的高温抗氧化性能最好。相较普通喷丸工艺,复合喷丸工艺更能明显降低EB-PVD制备的CoCrAlY涂层表面粗糙度,提高涂层的致密度,改善物相结构,进而提升涂层的抗高温氧化性能。喷丸强度大于等于0.3N时,CoCrAlY涂层表面出现鳞状突出物,导致氧化物在此处择优生长,生成的氧化膜中的应力在此处集中而发生破裂,降低涂层的使用寿命,但复合喷丸能消除该鳞状突出物。     

Failure mechanism of a (Ni,Pt)Al/EB-PVD 8YSZ deposited on substrate with different curvature signs in thermal shock test

A thermal shock test was conducted on an 8 wt% Y₂O₃ stabilized ZrO₂ electron beam-physical vapor deposited (EB-PVD 8YSZ) thermal barrier coating with a (Ni, Pt)Al bond coating on the substrate with different curvature signs. The microstructural evolution and durability have been characterized. The microstructure of the top ceramic layer is strongly dependent on the substrate geometry. The results of the thermal shock test indicated that the sample with a positive curvature exhibits mixed mode spalling by the linking of cracks at TBC/TGO interface and TGO/BC interface. Spallation occurs primarily at the TGO/BC interface and inside the bond coats near to the surface of bond coats in planar samples. The spalling occurs principally at the TGO/BC interface in specimens with a negative curvature. The failure mechanism is elucidated integrate with stress analysis.