4.7 Article

Dynamic Response of a Composite Fan Blade Excited Instantaneously by Multiple MFC Actuators

Journal

AEROSPACE
Volume 9, Issue 6, Pages -

Publisher

MDPI
DOI: 10.3390/aerospace9060301

Keywords

macro fiber composite actuator; composite fan blade; modal test

Funding

  1. Special Fund for National Science and Technology Major Project [2017-II-0007-0021]

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This study conducted dynamic response measurements of a composite fan blade using multiple MFC actuators to study its vibration characteristics. The results showed that different combinations of MFC actuators excitation led to significant differences in blade response and could change the high cycle fatigue location.
The vibration characteristics of a composite fan blade are much more complex than those of a solid titanium fan blade due to the anisotropic material properties and complex excitations coming from unsteady flow and mechanically induced vibration. In this study, the dynamic response measurement of a wide-chord composite fan blade was carried out to study the vibration characteristics using multiple macro fiber composite (MFC) actuators, which can generate complex excitation forces with different frequencies and peak values at different locations. The measured mode shapes and natural frequencies were compared with the finite element simulation results. Based on these results, the responses of the blade under the instantaneous excitation of three MFC actuators with different combinations of several natural frequencies were measured and compared. The results show that the responses of the blade excited by different combinations of MFC actuators with different frequencies were significantly different from those excited by a single MFC actuator. The superposition of different mode shapes may cause the change of the vibration stress state, which indicates that the high cycle fatigue location of the blade under complex excitations may change to an unexpected location. The results will be helpful in understanding the vibration characteristics of the composite blades under complex excitations, and the MFC actuator could be a potential tool in vibration active control.

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