为提升涡轮叶片缘板阻尼器设计水平,对比B-G(blade to ground)型阻尼器和切向无约束B-B(blade to blade)型阻尼器结构,提出了一种基于刚度设计的B-B型缘板阻尼器结构。在动力学建模中重点分析了相邻叶片缘板和阻尼器之间总的正压力随阻...为提升涡轮叶片缘板阻尼器设计水平,对比B-G(blade to ground)型阻尼器和切向无约束B-B(blade to blade)型阻尼器结构,提出了一种基于刚度设计的B-B型缘板阻尼器结构。在动力学建模中重点分析了相邻叶片缘板和阻尼器之间总的正压力随阻尼器与左、右叶片缘板间相对运动在左、右缘板间的分配,给出了基于阻尼器运动的正压力分配方法;通过数值仿真分析了正压力分配对系统振动响应的影响,并重点讨论了阻尼器刚度、外激励相位差、正压力以及外激励幅值对系统减振特性的影响。仿真结果表明,在左、右叶片缘板与阻尼器完全粘滞和左、右叶片相对阻尼器对称同步振动的工况下可以将正压力按照平均分配处理;相比于切向无约束的B-B型阻尼器和刚性的B-G型阻尼器,所提出的基于刚度设计的缘板阻尼结构具有更优的减振性能。因此,研究结果提升了涡轮叶片缘板阻尼器接触正压力计算的准确性,拓展了阻尼器设计思路,可为同类阻尼器设计提供理论和工程参考。展开更多
The high temperature oxidation resistance of RE Ni W B B 4C MoS 2 composite coating, the effects of electrodeposition conditions on the morphologies of the coating and the effect of heat treatment temperature on its h...The high temperature oxidation resistance of RE Ni W B B 4C MoS 2 composite coating, the effects of electrodeposition conditions on the morphologies of the coating and the effect of heat treatment temperature on its hardness, abrasion resistance and phase structure were investigated by using scanning electron microscope(SEM), X ray diffractometer, microhardness tester and abrasion machine. The results show that the oxidation degree of RE Ni W B B 4C MoS 2 composite coating is small when the temperature is lower than 700 ℃, but it increases sharply when the temperature is higher than 700 ℃. The hardness of RE Ni W B B 4C MoS 2 composite coating increases with increasing heat treatment temperature, it comes up to the maximum value at 400 ℃,but it decreases gradually if the temperature rises continuously. The most favourable abrasion resistance was attained after RE Ni W B B 4C MoS 2 composite coating being heat treated at 400 ℃. Without heat treating, it is mainly amorphous and partially crystallized, but wholly crystallized after being heat treated at 500 ℃. RE in the composite coating is in the form of CeO 2 and additions of CeO 2 and B 4C can enhance the thermostability of RE Ni W B B 4C MoS 2 composite coating.展开更多
文摘为提升涡轮叶片缘板阻尼器设计水平,对比B-G(blade to ground)型阻尼器和切向无约束B-B(blade to blade)型阻尼器结构,提出了一种基于刚度设计的B-B型缘板阻尼器结构。在动力学建模中重点分析了相邻叶片缘板和阻尼器之间总的正压力随阻尼器与左、右叶片缘板间相对运动在左、右缘板间的分配,给出了基于阻尼器运动的正压力分配方法;通过数值仿真分析了正压力分配对系统振动响应的影响,并重点讨论了阻尼器刚度、外激励相位差、正压力以及外激励幅值对系统减振特性的影响。仿真结果表明,在左、右叶片缘板与阻尼器完全粘滞和左、右叶片相对阻尼器对称同步振动的工况下可以将正压力按照平均分配处理;相比于切向无约束的B-B型阻尼器和刚性的B-G型阻尼器,所提出的基于刚度设计的缘板阻尼结构具有更优的减振性能。因此,研究结果提升了涡轮叶片缘板阻尼器接触正压力计算的准确性,拓展了阻尼器设计思路,可为同类阻尼器设计提供理论和工程参考。
文摘The high temperature oxidation resistance of RE Ni W B B 4C MoS 2 composite coating, the effects of electrodeposition conditions on the morphologies of the coating and the effect of heat treatment temperature on its hardness, abrasion resistance and phase structure were investigated by using scanning electron microscope(SEM), X ray diffractometer, microhardness tester and abrasion machine. The results show that the oxidation degree of RE Ni W B B 4C MoS 2 composite coating is small when the temperature is lower than 700 ℃, but it increases sharply when the temperature is higher than 700 ℃. The hardness of RE Ni W B B 4C MoS 2 composite coating increases with increasing heat treatment temperature, it comes up to the maximum value at 400 ℃,but it decreases gradually if the temperature rises continuously. The most favourable abrasion resistance was attained after RE Ni W B B 4C MoS 2 composite coating being heat treated at 400 ℃. Without heat treating, it is mainly amorphous and partially crystallized, but wholly crystallized after being heat treated at 500 ℃. RE in the composite coating is in the form of CeO 2 and additions of CeO 2 and B 4C can enhance the thermostability of RE Ni W B B 4C MoS 2 composite coating.
