机译:用铝化涂层的Ni基超合金涡轮机叶片的维修损伤机理及界面开裂行为
Department of Aeronautics and Astronautics Fudan University Shanghai 200433 PR China;
AECC CHENGDU ENGINE CO. LTD. Chengdu 610503 PR China;
Xiangyang Hangtai Power Machinery Factory Xiangyang 441002 PR China;
Department of Aeronautics and Astronautics Fudan University Shanghai 200433 PR China;
Commercial Aircraft Engine Co. Ltd AECC Shanghai 200241 PR China;
Commercial Aircraft Engine Co. Ltd AECC Shanghai 200241 PR China;
Commercial Aircraft Engine Co. Ltd AECC Shanghai 200241 PR China;
Turbine blade; Aluminized coating; Ni-based superalloy; Service damage mechanism; Fatigue failure;
机译:基于Ni的高温合金叶片的竞争性开裂行为和微观机理,各自加速CCF衰竭
机译:单晶镍基高温合金PWA1480的#gamma#'相形貌,适用于第一高压涡轮叶片
机译:单晶NI基超合金,PWA1480的#Gamma#'相的形态,在第一高压涡轮叶片服务
机译:镍基高温合金第一阶段低压透平叶片简单老化后的形貌
机译:镍基高温合金晶间裂纹扩展中的晶界变形和损伤机理。
机译:镍基高温合金单晶涡轮叶片根部缺陷的产生
机译:基于分形分析的镍基高温燃气轮机叶片微结构损伤评估
机译:用小冲头法表征先进燃气轮机叶片中渗铝膜的力学性能