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    火箭发动机液压身部电铸镍与锆铜基材连接异常分析

    Analysis on Abnormal Connection of Electroformed Nickel and Zirconium Copper Substrate of Hydraulic Body in a Rocket Engine

    • 摘要: 某型火箭发动机液压身部锆铜内壁与电铸镍外壁成型后,经激光全息检测发现凸耳与电铸镍焊接位置背面存在约φ20 mm的连接异常。采用三种状态试件对连接异常进行了验证分析,通过显微组织分析和显微硬度测试分析了激光全息检测连接异常的原因。结果表明:凸耳与电铸镍的焊接热传导使镀铜层的显微组织由原来的柱状晶转变为粗大的等轴晶,并且镀铜层显微硬度随电铸镍焊缝熔深的增大而降低,从而使焊缝区附近的镀铜层与正常位置处产生微观变形差异,最终造成激光全息检测的连接异常。

       

      Abstract: The φ20 mm abnormal connection was detected in the back of the lug and electroformed nickel welding position by laser holography detection when zirconium copper (Zr-Cu) inner wall and electroformed nickel outer wall of the hydraulic body were formed in a rocket engine. Three kinds of specimens were used to verified the origin of the abnormal connection, and the reasons for the abnormal connection of laser holography detection were analyzed by microstructure analysis and micro-hardness test. The results show that the original columnar crystals were changed to coarse equiaxed crystals because of the welding heat conduction between the lug and electroformed nickel, and the micro-hardness of the copper coating decreased with the increase of the penetration depth of the electroformed nickel welding, which made the micro deformation difference between the copper coating near the welding zone and the normal position, and eventually led to the abnormal connection of the laser holography detection.

       

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