2018
DOI: 10.1007/s12206-018-1006-y
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A method of determining test load for full-scale wind turbine blade fatigue tests

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Cited by 10 publications
(4 citation statements)
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“…In fact, there are significant differences in the fatigue damage mechanisms of composites at different stress ratios, and the SaSm${S}_{\rm{a}} - {S}_{\rm{m}}$ plane is usually divided into compression‐compression (C‐C), compression‐tension (C‐T) and tension‐tension (T‐T) loading zones according to the value of the stress ratio 13,21 . However, a large number of comparative results of CLD models and fatigue test data indicate that the SaSm${S}_{\rm{a}} - {S}_{\rm{m}}$ plane should be divided into four zones that is, C‐C, C‐T, tension‐compression (T‐C) and tension‐tension (T‐T) loading zones, 31,32 as shown in Figure 5. Each load zone should be determined separately in the p ‐CLD modeling and the equal probability quantile points within each load zone should be co‐linear.…”
Section: P‐cld Modeling Methodologymentioning
confidence: 99%
See 1 more Smart Citation
“…In fact, there are significant differences in the fatigue damage mechanisms of composites at different stress ratios, and the SaSm${S}_{\rm{a}} - {S}_{\rm{m}}$ plane is usually divided into compression‐compression (C‐C), compression‐tension (C‐T) and tension‐tension (T‐T) loading zones according to the value of the stress ratio 13,21 . However, a large number of comparative results of CLD models and fatigue test data indicate that the SaSm${S}_{\rm{a}} - {S}_{\rm{m}}$ plane should be divided into four zones that is, C‐C, C‐T, tension‐compression (T‐C) and tension‐tension (T‐T) loading zones, 31,32 as shown in Figure 5. Each load zone should be determined separately in the p ‐CLD modeling and the equal probability quantile points within each load zone should be co‐linear.…”
Section: P‐cld Modeling Methodologymentioning
confidence: 99%
“…I G U R E 2 S-N Curve and CLD model for engineering structures 32. CLD, constant amplitude life diagram.…”
mentioning
confidence: 99%
“…The fatigue load spectrum of the blade is introduced, and the fatigue cumulative damage of the section where each node of the blade finite element model is calculated by using the fatigue test target load calculation method proposed in Reference [8], and the target load with the stress ratio 1 r = − in the flap and edgewise of the section is generated respectively. Since the stress ratio Step 3.…”
Section: Test Load Distribution Optimization Methods Based On Particl...mentioning
confidence: 99%
“…Second, simultaneously carry out the flap-wise and edgewise direction loading test, shorten the test cycle time [4][5]. According to the test loading form, the fatigue test of full-scale structures is mainly divided into forced displacement type and resonance excitation type [6]. Compared to the forced displacement type, the resonant excitation type fatigue test system can obtain a large blade amplitude with a small excitation force, and has the advantages of low cost, short test cycle and suitable for large wind turbine blades [7].…”
Section: Introductionmentioning
confidence: 99%