摘要
针对材料级试验件在高温环境、低周离心载荷和高周振动载荷共同作用下的疲劳寿命,开展高温高低周复合载荷疲劳试验技术研究,突破电磁感应加热试验技术、高低周复合载荷加载控制技术,并在试验中得到了充分验证。
For the fatigue life of turbine rotor blades under the combined action of high temperature,low cycle centrifugal load and high cycle vibration load,the technology of high-low cycle composite load fatigue test with high temperature is carried out,and break through electromagnetic induction heating technology,coordinated loading control technology of high-low cycle composite loads,orthogonal load decoupling technique.And based on the turbine blade simulation test,the above technology is fully verified,the correctness and feasibility of the test technology are proved.
作者
张伟
由于
黄太誉
燕群
徐健
Zhang Wei;You Yu;Huang Taiyu;Yan Qun;Xu Jian(Aircraft Strength Research Institute of China,Xi’an 710065,China)
出处
《飞行器强度研究》
2021年第3期49-53,共5页
Aircraft Strength Research
关键词
涡轮转子叶片
电磁感应加热
高低周复合载荷
协调加载
turbine rotor blade
electromagnetic induction heating
high-low cycle combined loads
synchronous coordinated loading