Till König, Sebastian P. Hagen, Sannakaisa Virtanen, Mathias C. Galetz
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引用次数: 0
Abstract
Co-based γ/γ′ superalloys are in development as candidates to replace Ni-based superalloys in turbine engines, where they will be exposed to hot corrosion. The present study investigates the resistance to high temperature Type I hot corrosion of four alloys of the Co–Ni–Al–W system, which differed in their Co to Ni ratio and their W content. In addition, the alloys are tested not only uncoated but also with an Al and a Cr diffusion coating. The exposures were performed at 950°C with a Na2SO4 deposit of 2.5 mg/cm2 in air containing 0.1% SO2 for 100 and 300 h. The degradation was investigated by material loss measurements. Both coatings proved mostly protective for 100 h, while the uncoated samples were severely degraded. After the longer exposure time, only the Cr-coating remained partially protective and outmatched the Al-coating. Further, a positive influence was attributed to a higher Co to Ni ratio (1.4 vs. 0.7) and a higher W content (5 vs. 3 at%).
co基γ/γ′高温合金正在开发中,作为涡轮发动机中ni基高温合金的候选材料,它们将暴露在热腐蚀中。本文研究了Co - Ni比和W含量不同的4种Co - Ni - al - W系合金的耐高温I型热腐蚀性能。此外,合金不仅进行了无涂层测试,还进行了Al和Cr扩散涂层测试。在950°C下,在含有0.1% SO2的空气中以2.5 mg/cm2的Na2SO4沉积100和300小时进行暴露。通过材料损耗测量来研究其降解。两种涂层在100小时内都具有良好的保护作用,而未涂层的样品降解严重。在较长的曝光时间后,只有cr涂层保留了部分保护作用,并超过了al涂层。此外,较高的Co / Ni比(1.4 vs. 0.7)和较高的W含量(5% vs. 3%)也具有积极的影响。
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