Erosion Damage to Last-Stage Compressor Disk of a Heavy-duty Gas Turbine Engine | Erosionsschaden der Verdichterradscheibe einer Großgasturbine

2021 ◽  
pp. 245-252
Author(s):  
A. Neidel ◽  
T. Gädicke ◽  
S. Wallich ◽  
E. Engert
2021 ◽  
Vol 58 (11) ◽  
pp. 715-724
Author(s):  
A. Neidel ◽  
T. Gädicke ◽  
S. Riesenbeck

Abstract Short fillet welds used to fasten a large retainer ring to so-called dog bone seals failed in the turbine exhaust casing of a non-OEM heavy-duty gas turbine engine used for power generation. The subject fillet welds fractured due to high cycle fatigue loading. Neither weld imperfections nor any other material defects were found that could have contributed to the failure. It was concluded that an unfavorable design, specifying very short fillet welds for fastening the dog bone seal segments to the retainer ring, was the root cause of failure. In a purely static loading situation, this design would probably not have failed. However, in a dynamic loading scenario as is the case in any gas turbine engine exhaust, such a design is simply not sturdy enough.


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