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Cracking behaviour, failure modes and lifetime analysis of M320 abradable compressor seal coating

机译:M320耐磨压缩机密封涂层的开裂行为,失效模式和寿命分析

摘要

Metco 320 is a AlSi-hBN-polyester abradable, used in the high pressure compressorof commercial gas turbines. The material response to cyclic heating and cooling, and theresulting changes in microstructure, as well as their associated failure mechanisms wereinvestigated. It was found that the top surface layer of the abradable liner degrades overits lifetime. During thermal cycling hBN is removed from the material’s microstructure,which results in the degradation of the abradable and increased brittleness of the topsurface.Furthermore, material cracking and delamination behaviour during service was successfullyreproduced in the laboratory. The cracking and delamination observations made duringoverhaul, were replicated using cyclic water-quenching, but the spallation of abradablematerial did not occur. Investigations into material properties and their influenceupon the abradable failure mechanics revealed, that soft M320 matched the observationsmade during engine overhauls. It could also be established, that the plasma spray process,grit blasting, surface treatment after deposition and the transient of the substrateaffect the abradable’s performance and life-time, when heat cycled.Some service casings suffer from premature liner loss. These unscheduled overhaulsare costly and their number is desired to be reduced, if possible eliminated. In orderto control the material failures, the stresses introduced into the abradable seal duringmanufacturing need to be reduced, since this is one of main drivers for material crackingand delamination. Furthermore, it was established, that material at the top end ofthe hardness specification performed better in service. This is due to the fact, that moreAlSi metal matrix is present in the microstructure and the hBN loss does not affect thematerial integrity as much as in soft material. 2D and 3D modelling showed temperatureand strain profiles evolving during the quenching process. These show the areas of highstrain, which are consistent with the crack initiation areas observed during testing.It can be concluded, that M320 abradable is a very complex material system, which isinfluenced by several parameters. This research project highlighted, how sensitive thefailure modes are to changes in the material/substrate combination. Recommended isto increase the material hardness towards the upper end of the current specification (70HR15Y), reduce the stresses in the substrate and the abradable material by means ofannealing stages after grit blasting, and temperature control during plasma spraying. Furthermore,it would be beneficial to reduce the machining of the abradable’s surface afterdeposition, as well as carrying out further research into the failure modes of abradables.
机译:Metco 320是可磨损的AlSi-hBN聚酯,用于商用燃气轮机的高压压缩机。研究了材料对循环加热和冷却的反应,以及由此导致的微观结构变化及其相关的失效机理。已经发现,耐磨衬里的顶表面层降低了其使用寿命。在热循环过程中,hBN会从材料的微观结构中去除,这会导致耐磨性下降并增加顶表面的脆性。此外,在实验室中成功地再现了材料在使用过程中的开裂和分层行为。大修过程中观察到的开裂和分层现象是通过循环水淬处理重复进行的,但可磨耗材料的剥落并未发生。对材料性能及其对耐磨性失效机理的影响进行的调查显示,软M320与发动机大修期间的观察结果相符。还可以确定,当进行热循环时,等离子喷涂工艺,喷砂处理,沉积后的表面处理以及基材的瞬变会影响可磨耗性材料的性能和使用寿命。某些维修用套管会因衬套过早损坏而遭受损失。这些计划外的大修费用昂贵,并且如果可能的话,希望减少它们的数量。为了控制材料失效,需要减少制造过程中引入耐磨密封件的应力,因为这是材料破裂和分层的主要驱动力之一。此外,可以确定的是,硬度规格最高的材料在使用中表现更好。这是由于以下事实:在显微组织中存在更多的AlSi金属基体,而hBN损失对材料完整性的影响不如软质材料大。 2D和3D建模显示了淬火过程中温度和应变曲线的演变。这些显示出高应变区域,与测试期间观察到的裂纹萌生区域一致。可以得出结论,M320耐磨材料是非常复杂的材料系统,受多个参数的影响。该研究项目强调了失效模式对材料/基材组合变化的敏感程度。推荐的方法是在当前规范(70HR15Y)的上限范围内提高材料硬度,通过喷砂后的退火阶段以及等离子喷涂期间的温度控制来降低基材和耐磨材料中的应力。此外,减少可磨耗材料表面沉积后的机械加工以及对可磨耗材料的失效模式进行进一步研究将是有益的。

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    Goergen Sandra;

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  • 年度 2012
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