燃气轮机高压涡轮盘超速预应力试验研究  

Experimental Study on Overspeed Prestressing of High Pressure Turbine Disk of Gas Turbine

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作  者:孙彦博 田强[3] 何建元 秦鹤勇[3] SUN Yanbo;TIAN Qiang;HE Jianyuan;QIN Heyong(No.703 Research Institute of CSSC,Harbin,China,150078;National Engineering Research Center of Special Equipment and Power System for Ship and Marine EngineeringGas Turbine R&D and Testing Laboratory,Harbin,China,150078;Central Iron and Steel Research Institute,Beijing,China,100081)

机构地区:[1]中国船舶集团有限公司第七○三研究所,黑龙江哈尔滨150078 [2]船舶与海洋工程特种装备和动力系统国家工程研究中心-燃气轮机研发与检测试验室,黑龙江哈尔滨150078 [3]钢铁研究总院有限公司,北京100081

出  处:《热能动力工程》2024年第5期50-56,共7页Journal of Engineering for Thermal Energy and Power

基  金:中船集团自立科技项目(202109Z);黑龙江省自然科学基金(TD2021E001)。

摘  要:为了降低涡轮盘的服役应力、提高涡轮盘的寿命和可靠性,对加工过程中未去应力的涡轮盘试验件进行超速预应力试验,并对试验前后的轮盘试验件进行残余应力测试。研究表明:超速预应力试验可以对轮盘的关键部位(盘心)预制残余压应力,残余周向应力计算值与测量值相比误差为9.2%;超速预应力试验可以降低轮盘表面的残余应力,与试验前相比残余周向应力最大降幅达58%;超速预应力试验可以提高轮盘的服役寿命,与试验前相比寿命预测提升1倍。In order to reduce the service stress of the turbine disk,and improve the service life and relia-bility of the turbine disk,the overspeed prestressing test was carried out on a turbine disk test piece with-out removing the stress in machining process,and the residual stress was tested on the disk test piece be-fore and after the test.The results show that overspeed prestressing test can prefabricate the residual com-pressive stress of the key part of the disk(disk core),and the error of the calculated residual circumfer-ential stress is 9.2%compared with the measured value;the overspeed prestressing test can reduce the residual stress on the surface of the disk,and the residual circumferential stress decreases by the maxi-mum of 58%compared with that before the test;the overspeed prestressing test can improve the service life of the disk,and the life prediction can be doubled compared with that before the test.

关 键 词:燃气轮机 涡轮盘 超速预应力 试验 

分 类 号:TK47[动力工程及工程热物理—动力机械及工程]

 

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