TY - CONF A1 - Zhu, Jiangchao A1 - Madia, Mauro A1 - Schurig, M. A1 - Schlums, H. A1 - Zerbst, Uwe T1 - Fracture mechanics-based structural integrity assessment of aeroengine turbine disks under overspeed conditions N2 - Aero-engine turbine disks are safety-relevant components which are operated under high thermal and mechanical stress conditions. The actual part qualification and certification procedures make use of spin-tests conducted on productionsimilar disks. While these tests provide, on the one hand, a reliable definition of the critical conditions for real components, on the other hand they represent a relevant cost item for engine manufacturers. The aim of this work is to present part of a fracture mechanics-based procedure under development which aims at replacing the tests on production-similar disks with lab tests on fracture mechanics specimens. In particular, the rimpeeling failure mode is considered as case study. A semi-circular surface crack is modelled at the most stressed region at the diaphragm of a turbine disk, with the crack plane perpendicular to the radial direction. The crack is therefore subjected to a biaxial stress state and grows under increasing rotational speed until it triggers the rim-peeling failure. The finite element simulation of the cracked disk considers the real thermal and mechanical loading conditions. In order to design a lab representative specimen, beside the crack driving force, expressed in terms of � -integral, also the constraint to plastic deformation e.g., stress triaxiality, at the crack-tip must be similar for the same crack in the specimen and in the disk. This has been achieved and as expected, both the highest � -integral and constraint factor are calculated at the same location along the crack front for both disk and specimen. The results of the structural integrity assessment in the form of a Failure Assessment Diagram (FAD) show good agreement between designed specimen and disk both in terms of expected failure mode and value of the critical speed. Probabilistic aspects are also considered in the calculations. T2 - ASME Turbo Expo 2022: Turbomachinery Technical Conference and Exposition (GT2022) CY - Rotterdam, The Netherlands DA - 13.06.2022 KW - Fracture mechanics KW - Burst KW - Turbine disk PY - 2022 SP - 1 EP - 7 PB - ASME AN - OPUS4-55903 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Zhu, J. A1 - Madia, Mauro A1 - Schurig, M. A1 - Kruse, Julius A1 - Conrad, F. A1 - Schlums, H. A1 - Kontermann, C. A1 - Zerbst, Uwe T1 - Anwendung von repräsentativen Proben zur Bewertung der Strukturintegrität von sicherheitsrelevanten Komponenten N2 - Sicherheitsrelevante Bauteile, bei denen ein Versagen im Betrieb katastrophale Folgen haben könnte, sind in der Regel für eine sehr geringe Ausfallwahrscheinlichkeit ausgelegt und unterliegen strengen Qualifizierungsverfahren gemäß den von den Aufsichtsbehörden festgelegten Richtlinien. Die Hersteller sind oft gezwungen, Tests an realen oder skalierten Komponenten durchzuführen, um die Strukturintegrität unter definierten Belastungsbedingungen sicherzustellen, die in der Regel strenger sind als die im Betrieb zu erwartenden. Dies ist in der Regel mit einem enormen experimentellen und finanziellen Aufwand verbunden. Daher versuchen die Unternehmen, neue Strategien wie digitale Zwillinge zu entwickeln, mit denen die Kosten massiv gesenkt werden können, ohne die Sicherheit zu beeinträchtigen. In dieser Arbeit wird ein neues quasistatisches Prüf- und Bewertungskonzept vorgestellt, dessen Hauptidee darin besteht, die experimentelle Prüfung von Bauteilen durch die Prüfung von für das Bauteil repräsentativen Proben zu ersetzen oder zumindest zu reduzieren. Der größte Vorteil des vorgeschlagenen Konzepts besteht darin, dass die Versuche auf Laborprüfmaschinen durchgeführt werden können. Die Wirksamkeit der Methodik wird anhand der Bewertung der Strukturintegrität einer Turbinenscheibe aus einer Ni-Basis-Superlegierung für Flugzeugtriebwerke bei Überdrehzahl demonstriert. T2 - 57. Tagung des DVM-Arbeitskreises Bruchmechanik und Bauteilsicherheit CY - Köln, Germany DA - 18.02.2025 KW - Strukturintegrität KW - Bruchmechanik KW - Turbinenscheibe KW - Repräsentative Proben PY - 2025 DO - https://doi.org/10.48447/BR-2025-536 SP - 231 EP - 240 PB - DVM CY - Berlin AN - OPUS4-62602 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Zhu, Jiangchao A1 - Madia, Mauro A1 - Schurig, Michael A1 - Fedelich, Bernard A1 - Schlums, H. A1 - Zerbst, Uwe T1 - Burst Behaviours Of Aero Engine Turbine Disk At Overspeed Conditions N2 - Aero-engine turbine disks are safety-relevant components which are operated under high thermal and mechanical stress conditions. The actual part qualification and certification procedures make use of spin-tests conducted on production-similar disks. The aim of this work is to present part of a fracture mechanics-based procedure under development which aims at replacing the tests on production-similar disks with lab tests on fracture mechanics specimens. The finite element simulation of the cracked disk considers the real thermal and mechanical loading conditions. In order to design a lab representative specimen, beside the crack driving force, expressed in terms of 𝐽-integral, also the constraint to plastic deformation e.g., stress triaxiality, at the crack-tip must be similar for the same crack in the specimen and in the disk. This has been achieved and as expected, both the highest 𝐽 -integral and constraint factor are calculated at the same location along the crack front for both disk and specimen. The results of the structural integrity assessment in the form of a Failure Assessment Diagram (FAD) show good agreement between designed specimen and disk both in terms of expected failure mode and value of the critical speed. In addition, probabilistic aspects are also considered in the calculations. T2 - 43rd Int. Conference on Materials Mechanics, June 5-10, 2022, Greece CY - Sani, Chalkidiki, Greece DA - 05.06.2022 KW - Structural integrity KW - Turbine disk KW - Fracture mechanics KW - Overspeed PY - 2022 SP - 1 EP - 13 AN - OPUS4-57279 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER -