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Evaluation of residual stresses of thermal barrier coatings with HVOF thermally sprayed bond coats using the Modified Layer Removal Method (MLRM)

机译:使用改良层去除法(MLRM)评估HVOF热喷涂粘结涂层的热障涂层的残余应力

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The use of thermally sprayed thermal barrier coatings (TBC) has permitted the increase of combustion temperatures of gas turbines and diesel engines in the last decades. In terms of system performance, the possibility of increasing in working temperature is always welcome. It is well known that the residual stresses due to the mismatch between metallic bond coat and ceramic top coat as well as the stresses due to the oxidation of the bond coat generate debonding of the TBC, leading to a collapse of all thermal barrier system. Several attempts have been done to minimize or even to solve this kind of problems. One of the possibilities that have been tried is to apply graded or multilayered coatings, or to induce compressive stresses that can compensate the tensile residual stresses due to spraying process. In this work, two TBC systems were obtained by applying two distinct bond coats and two distinct top coats. The commercial bond coats were applied by High Velocity Oxygen Fuel (HVOF) thermal spraying. Residual stresses were measured by the Modified Layer Removal Test. Results show that the residual stresses are mainly influenced by the thermal history regarding the quenching of individual splats and the plastic deformation of ceramic deposits. (c) 2005 Elsevier B.V. All rights reserved.
机译:在过去的几十年中,热喷涂热障涂层(TBC)的使用使燃气轮机和柴油发动机的燃烧温度得以提高。在系统性能方面,始终欢迎提高工作温度的可能性。众所周知,由于金属粘结涂层和陶瓷面涂层之间的不匹配而产生的残余应力以及由于粘结涂层的氧化而产生的应力会导致TBC脱粘,从而导致所有热障系统崩溃。已经进行了几次尝试以最小化或什至解决此类问题。已尝试的一种可能性是施加渐变或多层涂层,或产生可补偿由于喷涂过程而产生的拉伸残余应力的压缩应力。在这项工作中,通过应用两个不同的粘结层和两个不同的面漆获得了两个TBC系统。通过高速氧气燃料(HVOF)热喷涂法来涂覆商用粘结层。残余应力通过改性层去除测试进行测量。结果表明,残余应力主要受单个钢板淬火和陶瓷沉积物塑性变形的热历史影响。 (c)2005 Elsevier B.V.保留所有权利。

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