发明名称 SMART TAB DEVICE USED FOR VIBRATION AND NOISE CONTROL ON MANNED OR UNMANNED HELICOPTER ROTOR BLADE AND THE WORKING METHODOLOGY OF THE SAME
摘要 PURPOSE: A smart tap for a helicopter and a driving method thereof are provided to apply a driving tap to a rotor blade for a manned/unmanned helicopter and to satisfy noise reduction demanded in the international civil aviation organization. CONSTITUTION: A smart tap for a helicopter is mounted on a rotor blade(B) of a helicopter and comprises a tap(10) and an piezoelectric actuator(20). The tap is hinge coupled to the end of the rotor blade. The other end of the tap is hinge-turned to the outside of the rotor blade around a pivot(11) as a shaft. The piezoelectric actuator turns the tap according to displacement by receiving electric field signals.
申请公布号 KR20120068145(A) 申请公布日期 2012.06.27
申请号 KR20100129611 申请日期 2010.12.17
申请人 KOREA AEROSPACE RESEARCH INSTITUTE 发明人 KIM, DEOG KWAN;CHUNG, KI HOON;SONG, KUEN WOONG;KIM, SEUNG HO
分类号 B64C27/51;B64C13/16;B64C27/467;B64C27/473 主分类号 B64C27/51
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