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.
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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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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