2020
DOI: 10.1016/j.renene.2020.06.142
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Probabilistic failure rate model of a tidal turbine pitch system

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Cited by 10 publications
(6 citation statements)
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“…Let 𝜆 𝑖 be the failure rate of component i during the normal life phase of the bathtub curve under the independent failure. Assuming that the product lifespan obeys the exponential distribution during this period [10,18], the failure probability đč 𝑖 of component i can be expressed as:…”
Section: Conventional Optimal Modelmentioning
confidence: 99%
“…Let 𝜆 𝑖 be the failure rate of component i during the normal life phase of the bathtub curve under the independent failure. Assuming that the product lifespan obeys the exponential distribution during this period [10,18], the failure probability đč 𝑖 of component i can be expressed as:…”
Section: Conventional Optimal Modelmentioning
confidence: 99%
“…Equation ( 16) was integrated numerically using the results for the axial trust shown in Figure 4 that yielded P m = 820 kN. The rating life, Equation (13), accounts only for fatigue failure of a properly manufactured rolling bearing, which operates under conventional operating conditions, i.e., when the bearing is properly mounted, protected from foreign matter, adequately lubricated and not exposed to extreme temperature or excessive loads [36]. However, the actual operating conditions of a bearing may differ from the conventional ones.…”
Section: Evaluation Of the Failure Rate Of The Main Bearingmentioning
confidence: 99%
“…Since there are significant uncertainties associated with the influence factors and the technique itself, it was suggested, in the context of mechanical components of a HATT, to treat these factors and, subsequently, the resulting failure rate as random variables [12]. This probabilistic approach to failure rates was further developed and implemented for components of a pitch system of a HATT in [13]. In this work, the influence of specific characteristics of components of the pitch systems on their failure rates was taken into account.…”
Section: Introductionmentioning
confidence: 99%
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“…First, the number of load cycles in the dynamic rotor load simulation history is counted, then, the component fatigue is calculated and accumulated, and finally, test loads are derived, regarding the criterion of fatigue-equivalence [8]. The significance of the entire process is based on the correct selection of the critical component [11]. If the critical component is not known, the described process must be repeated for each possibly critical component, including the execution of experimental investigations.…”
Section: Introductionmentioning
confidence: 99%