Metallurgical Evaluation of a Fractured Gas Turbine Combustor Dome

Thursday, October 1, 2026: 11:20 AM
306B (Québec City Convention Centre)
Mr. Alan Soto, GE Aerospace , GE Aerospace, Queretaro, QA, Mexico
The presentation covers a case study where thermal fatigue cracking was observed extending from eroded/oxidized regions on the hot side at the eyelet radius leading to the baffle (with Thermal Barrier Coating) liberation. The investigation describes the metallurgical findings observed and suspected factors involved to understand root cause.