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Permanent Weld Repair of GE F Type IP Outer Shell With Incorporated Design Improvements

机译:GE F型IP外壳永久焊接修复,具有掺入的设计改进

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Recently an internal inspection was performed on a 30-year old 219 MW General Electric F9 design steam turbine that was forced out of service due to high vibration. During the inspection two significant cracks were discovered on the IP upper outer shell. The cracking was located in the reheat inlet bowl area on the left and right hand side. The cracking initiated at the horizontal joint bolt hole locations and propagated upwards towards the intercept valve flange. The left side crack was approximately 26"in length and had propagated all the way through the shell wall from the ID to the OD. The right side crack was 30" in length and had propagated approximately halfway through the shell wall thickness in this area. This type of cracking has been observed on other General Electric turbine shells of similar design in the past. The repeatability of this cracking mode is indicative of a design weakness in this particular design. A repair vendor to determine the best geometry of the shell in the reheat bowl area performed an extensive engineering analysis utilizing finite element modeling. This was necessary since it was the owner's intent to perform a permanent weld repair because of their desire to obtain another 20 plus years of service for this unit. If design improvement could be achieved to advance this objective then the owner wanted them to incorporated into the repair. It was felt that if the geometric design issue was not addressed then the potential for future cracking in this area remained very high. This paper will detail the results obtained from the finite element modeling and analysis study. The resulting repair recommendations and procedures will be discussed with an overview of the actual permanent weld repair process that was performed on this unit. The unit was stress relieved weld repaired in the fall of 1998 and has been successfully returned to service.
机译:最近,在30岁的219 MW通用电气F9设计汽轮机上进行了内部检查,由于高振动而被迫退出服务。在检查期间,在IP上外壳上发现了两个显着的裂缝。裂缝位于左侧和右侧的再热入口碗区域中。在水平接头螺栓孔位置发起的裂缝,并向上朝向拦截阀法兰传播。左侧裂缝的长度约为26英寸,并从ID到OD中一直通过壳壁传播。右侧裂缝的长度为30英寸,并且通过该区域的壳体厚度大约半途地传播。在过去的类似设计的其他通用电动涡轮机壳上已经观察到这种类型的裂缝。该开裂模式的可重复性指示该特定设计中的设计弱点。修复供应商以确定再热碗区域中壳体的最佳几何形状进行了广泛的工程分析,利用有限元建模进行了广泛的工程分析。这是必要的,因为主人的目的是因为他们想要为本机获得另外20多年的服务而进行永久焊接修复。如果可以实现设计改进以推进此目标,那么所有者希望他们纳入维修。有人认为,如果没有解决几何设计问题,那么该地区未来破裂的可能性仍然很高。本文将详述从有限元建模和分析研究中获得的结果。由此产生的修复建议和程序将概述本机上执行的实际永久焊接修复过程。该单位是1998年秋季修复的压力缓解焊缝,已成功返回服务。

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