Volume 7B: Structures and Dynamics 2017
DOI: 10.1115/gt2017-63193
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Modal Analyses of an Axial Turbine Blisk With Intentional Mistuning

Abstract: The potential of intentional mistuning to reduce the maximum forced response is analyzed within the development of an axial turbine blisk for ship diesel engine turbocharger applications. The basic idea of the approach is to provide an increased aerodynamic damping level for particular engine order excitations and mode shapes without any significant distortions of the aerodynamic performance. The mistuning pattern intended to yield a mitigation of the forced response is derived from an optimization study apply… Show more

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Cited by 4 publications
(3 citation statements)
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“…16), nearly all other TWM participating to the response are contributing additional damping. The resulting aerodynamic damping [18] can be computed by…”
Section: Forced Response Analyses and Robustnessmentioning
confidence: 99%
“…16), nearly all other TWM participating to the response are contributing additional damping. The resulting aerodynamic damping [18] can be computed by…”
Section: Forced Response Analyses and Robustnessmentioning
confidence: 99%
“…e intentionally mistuned design of blisks is performed in the recent years. For example, the intentional mistuning was introduced to reduce the forced response of blade [32][33][34][35]. In addition, some other scholars conducted the reliability and optimization of blades [36][37][38].…”
Section: Introductionmentioning
confidence: 99%
“…As a consequence, some blades may be more excited than others in a narrow frequency range near the non-mistuned (nominal geometry) theoretical value. Despite this, controlled mistuning can be intentionally introduced and optimized in order to reduce the overall vibrational magnitude [7][8][9]. The mistuning introduced is usually significantly larger than the additional random (or stochastic) mistuning [10].…”
Section: Introductionmentioning
confidence: 99%