Proceedings of the Korean Society for Noise and Vibration Engineering Conference (한국소음진동공학회:학술대회논문집)
- 2014.10a
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- Pages.916-921
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- 2014
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- 1598-2548(pISSN)
Kinematic design improvement and validation of ATF(Active Trailing-edge Flap) for helicopter vibration reduction
헬리콥터의 진동하중 저감을 위한 능동 뒷전플랩의 기구학적 설계 개선 및 검증
- Published : 2014.10.29
Abstract
In this paper, an improved small-scaled blade prototype was designed with the flap-driving mechanism classified as an active vibration reduction method, in order to reduce vibratory load in the helicopter. In detail, the previous Active Trailing-Edge Flap based on piezoelectric actuator, called SNUF(Seoul National University Flap), failed to achieve the target value (
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