The invention relates to the technical field of
wind power blade fatigue tests, and discloses a blade
dynamic loading method based on double-shaft
coupling resonance, which comprises the steps of forced loading in the shimmy direction, pulse type follow-up loading in the
flapping direction and
phase synchronization, and is characterized in that the loading frequency in the shimmy direction is set to be always close to the current resonant frequency in the
flapping direction; the amplitude of the exciting force in the shimmy direction is dynamically adjusted according to the
vibration response in the
flapping direction, in the thrust loading stage, when the displacement in the flapping direction reaches a
peak value, a thrust pulse is applied to the flapping direction, the magnitude of the thrust pulse is decreased progressively along with attenuation of the
vibration amplitude, energy needed by active excitation is reduced through the
modal coupling effect, and the active excitation effect is improved. Pulse thrust is only applied in a displacement
peak value interval in the flapping direction, free attenuation is achieved in other time, invalid
energy consumption is avoided, the amplitude is adjusted in a self-adaptive mode, so that shimmy excitation force is dynamically optimized along with flapping
vibration response, overload or insufficient excitation is avoided, and rigidity degradation in the blade testing process is adapted.