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Testing of rotor blades of wind turbines Arno van Wingerde ...

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LOAD 3<br />

LOAD 2<br />

LOAD 1+3<br />

c) Bending moment distribution along blade axis due to two concentrated loads at the blade<br />

Figure 6 bending moment distribution along the blade length<br />

Fatigue testing <strong>of</strong> <strong>rotor</strong> <strong>blades</strong><br />

A fatigue test <strong>of</strong> a <strong>rotor</strong> blade is notoriously more complex than a static test. All the<br />

previously outlined problems, regarding the need for a clean representation <strong>of</strong> the<br />

actual stress states across the cross section and along the length <strong>of</strong> the blade are<br />

still there, but a number <strong>of</strong> additional problems occur.<br />

Required testing time<br />

Actual bending<br />

moment distribution<br />

Bending moment<br />

due to<br />

test load<br />

Wind <strong>turbines</strong> experience about 10 8 -10 9 cycles, much more than virtually any other<br />

known structure, see Figure 7. Also, the loadings vary more than other structures,<br />

making fatigue testing <strong>of</strong> <strong>rotor</strong> <strong>blades</strong> particularly difficult.<br />

Figure 7 Overview <strong>of</strong> fatigue loaded structures [9]<br />

Assuming a frequency <strong>of</strong> 1 Hz, 10 8 -10 9 cycles would take about 3 to 32 years, which<br />

is highly impractical. Therefore the tests are carried out at a raised load level, so that<br />

10 6 or 2·10 6 cycles would suffice to reach the equivalent fatigue damage.<br />

However, many <strong>blades</strong> are tested at their natural frequency, which is typically below<br />

1 Hz, especially for larger <strong>blades</strong>, in which case 0.3 Hz. and lower are possible. <strong>Testing</strong><br />

outside <strong>of</strong> the natural frequency is possible, but requires vastly more force and

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