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    火箭发动机喷注器焊缝熔深的涡流检测

    Eddy current testing of weld penetration of rocket engine injector

    • 摘要: 喷注器是液体火箭发动机燃烧室的关键部件。喷注器存在大量电子束焊缝,其焊缝熔深关系到喷注器的可靠性,可能影响火箭发动机的安全稳定运行。针对火箭发动机喷注器电子束焊缝熔深质量缺乏有效检测评价的问题,开展了相应的涡流检测方法有效性研究。首先,基于退化磁矢位的棱边有限元法开展了电子束焊缝熔深涡流检测数值模拟,分析了Pancake和TR构型涡流检测探头评价焊缝熔深的可行性和灵敏度。其次,根据数值仿真结果设计制作了适于喷注器焊缝检测的Pancake和TR涡流检测探头,通过试验进一步验证了涡流检测方法评价电子束焊缝熔深的可行性。试验结果表明,Pancke探头对焊缝熔深检测评价具有更高的灵敏度,涡流检测方法能有效评价喷注器电子束焊缝熔深。

       

      Abstract: The injector serves is a critical component in liquid rocket engine combustion chambers. Numerous electron beam welds exist in injectors, where weld penetration depth directly affects injector reliability and may impact the safe and stable operation of rocket engines. Addressing the lack of effective detection and evaluation methods for electron beam weld penetration quality in rocket engine injectors, this study investigated the effectiveness of eddy current testing methods. First, numerical simulations of electron beam weld penetration eddy current testing were conducted using edge finite element methods based on reduced magnetic vector potentials, analyzing the feasibility and sensitivity of Pancake and TR configuration eddy current probes for evaluating weld penetration. Subsequently, based on simulation results, specially designed Pancake and TR eddy current probes for injector weld inspection were fabricated, with experiments further validating the feasibility of eddy current methods for evaluating electron beam weld penetration. Results indicated that Pancake probes exhibited higher sensitivity for weld penetration detection, confirming that eddy current methods could effectively evaluate electron beam weld penetration in injectors.

       

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