Ioannis Chatzisavvas, Ilya Arsenyev, Rene Grahnert
Design and optimization of squirrel cage geometries in aircraft engines toward robust whole engine dynamics
Číslo: 2/2023
Periodikum: Applied and Computational Mechanics
DOI: 10.24132/acm.2023.841
Klíčová slova: jet engines; rotor dynamics; squirrel cage; optimization; vibration
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Fully automatized coupled analysis process chain is implemented, allowing to compute the influence of the SQCs geometry variation onto the full rotor dynamics and structural performance of the SQC. Two global optimization techniques are employed to explore the SQCs design space and find optimal 3D geometries, using the aforementioned coupled process.
Optimization results are compared and discussed in detail, indicating the importance of the numerical optimization to improve fatigue life of the squirrel cage. It is shown that optimized and non-optimized SQC designs, both fulfilling rotor dynamics goals, can have significantly different performance regarding their fatigue life. Moreover, the advantage of the coupled process is illustrated, allowing to find superior SQC designs by considering both disciplines simultaneously in comparison with a sequential (uncoupled) approach, when the target elastic properties of an SQC, selected only based on the rotor dynamics requirements, may lead to sub-optimal fatigue life.