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增压器叶片K17合金失效分析
引用本文:董建新.增压器叶片K17合金失效分析[J].兵器材料科学与工程,1996,19(6):54-58.
作者姓名:董建新
作者单位:北京科技大学
摘    要:通过显微分析手段,如SEM、TEM、成分分析及X-射线分析等,对经6000h实际运行的机车用增压器叶片(K17合金)进行解剖分析。结果表明,K17合金叶片产生较为严重的热腐蚀,并伴随有强化相γ'的聚集长大。

关 键 词:K17合金,增压器叶片,热腐蚀

INACTIVATION ANALYSIS ON ROOSTER BLADE OF K17 ALLOY
Dong Jianxin.INACTIVATION ANALYSIS ON ROOSTER BLADE OF K17 ALLOY[J].Ordnance Material Science and Engineering,1996,19(6):54-58.
Authors:Dong Jianxin
Abstract:The booster blade with 6,000 hours service was investigated with scan electron microscope(SEM), transmission electron microscope(TEM), micro-chemical composition and x-ray analysis. The experimental results show that the inactivation of K17 alloy blade is led by hotcorrosion, and with the coarsening behavior of the strengthening phase of γ'.
Keywords:s: K17  blade  hot-corrosion
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