发明名称 ROTOR BLADE DEICER
摘要 The present invention relates to a deicer for a rotor blade. The deicer for a rotor blade includes: a preceding edge which is extended along a longitudinal direction of a rotor blade and is placed in order to precede in the rotation direction; and a following edge which faces the preceding edge in the longitudinal direction and is placed in order to follow in the rotation direction. The deicer for a rotor blade comprises: a first heating mat unit which covers the preceding edge is placed in part of the top surface and the bottom surface of the rotor blade, and has a resistance body; a second heating mat unit which is placed on the top surface of the rotor blade in order to be adjacent to the first heating mat unit, and includes a resistance body; a third heating mat unit which is placed on the bottom surface of the rotor blade in order to be adjacent the first heating mat unit, and has a resistance body; and a fourth heating mat unit and a fifth heating mat unit which are placed on the bottom surface of the rotor blade in order to be adjacent to the third heating mat unit, and have a resistance body.
申请公布号 KR20140076156(A) 申请公布日期 2014.06.20
申请号 KR20120144388 申请日期 2012.12.12
申请人 KOREA AEROSPACE INDUSTRIES, LTD. 发明人 KIM, KYUNG SAM
分类号 B64D15/18;B64C11/16;H05B3/20 主分类号 B64D15/18
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