首页|K465高压涡轮叶片短时超温组织损伤研究

K465高压涡轮叶片短时超温组织损伤研究

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研究了K465 高压涡轮叶片经(1150~1310)℃×15 min超温热处理的组织退化规律.结果表明:随着超温温度的升高,K465高压涡轮叶片宏观晶粒颜色从黄色逐渐变为暗黄色+淡蓝色到深蓝色.枝晶间和枝晶干的γ'相、碳化物γ'膜、晶界γ'膜依次在 1240℃、1250~1260℃、1270℃溶解;共晶相在 1280℃时发生初溶,随着温度升高至 1310℃,共晶相溶解,空冷后重新析出花篮状形貌.碳化物组织退化主要表现为γ'膜的溶解和M6C的回溶;晶界组织退化主要表现为γ'膜的溶解和初溶的发生.随着温度升高,枝晶干和枝晶间的γ'相发生合并-球化-溶解-重新析出细小球状相的演变,γ'相面积分数降低.
Study on Microstructure Damage of K465 High-pressure Turbine Blade after Short-time Over-temperature Process
The microstructure degradation of K465 high-pressure turbine blades after(1150-1310)℃×15 min of over-temperature heat treatment was studied.The results show that the macroscopic grain color gradually changes from yellow,dark yellow+light blue to dark blue with the increase of over-temperature temperature.The interdendrite and dendrite γ'phase,the carbide γ'film,and the grain boundary γ'film are dissolved at 1240℃,1250-1260℃and 1270℃,respectively.The initial melting of eutectic occurs at 1280℃,and when the temperature increases to 1310℃,the eutectic phase is dissolved and the basket-like morphology is precipitated again after air cooling.The degeneration of carbide structure is mainly manifested by the dissolution of γ'film and the re-dissolution of M6C.The degradation of grain boundary structure is mainly manifested by the dissolution of γ'film and the occurrence of initial melting.With the increase of temperature,the evolution of the interdendrite and dendrite γ'phase from merging,spheroidization,dissolution to re-precipitation of fine globules happens,and the area fraction of γ'phase decreases.

K465 high-pressure turbine bladeover-temperaturemicrostructure degradation

王继成、邹伟、全琼蕊

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中国人民解放军 93147 部队,四川 广汉 618300

中国航发航空科技股份有限公司计量理化中心,四川 成都 610083

K465高压涡轮叶片 超温 组织退化

2024

热加工工艺
中国船舶重工集团公司热加工工艺研究所 中国造船工程学会船舶材料学术委员会

热加工工艺

CSTPCD北大核心
影响因子:0.55
ISSN:1001-3814
年,卷(期):2024.53(23)