-
公开(公告)号:US20130081269A1
公开(公告)日:2013-04-04
申请号:US13249440
申请日:2011-09-30
CPC分类号: B23K20/12 , B23K2101/001 , B23P6/00 , B23P6/005 , F01D5/005 , F05D2230/232 , Y10T29/49229 , Y10T29/5182
摘要: A system for repairing holes in a turbine engine component is provided. The system includes a turbine engine component including a front surface, a back surface, and a tapered surface extending from the front surface to the back surface, the tapered surface circumscribing the hole. The system further includes a plug configured to be welded to the turbine engine component, the plug including at least one tapered portion configured to contact the tapered surface when the plug is welded to the turbine engine component, and a die plate positioned on the back surface of the turbine engine component and including an aperture defined therethrough that is configured to collect flash generated when the plug is welded to the turbine engine component.
摘要翻译: 提供一种用于修理涡轮发动机部件中的孔的系统。 该系统包括涡轮发动机部件,其包括前表面,后表面和从前表面延伸到后表面的锥形表面,该锥形表面限定孔。 所述系统还包括被配置为焊接到所述涡轮发动机部件的塞子,所述塞子包括构造成当所述塞子被焊接到所述涡轮发动机部件时与所述锥形表面接触的至少一个锥形部分,以及定位在所述背面 并且包括限定在其中的孔,其被构造成收集当所述塞被焊接到所述涡轮发动机部件时产生的闪电。