发明名称 Rotor Blade De-Icing System
摘要 An aircraft includes a heat absorbent material carried by an airfoil susceptible to ice buildup and a transmitter spaced apart from the heat absorbent material. A method includes the process of transmitting the heat energy from the transmitter to the heat absorbent material that in turn warms the airfoil to break apart ice buildup.
申请公布号 US2012256053(A1) 申请公布日期 2012.10.11
申请号 US201213422599 申请日期 2012.03.16
申请人 MCCOLLOUGH JAMES M.;AUBERT ROGER;BELL HELICOPTER TEXTRON INC. 发明人 MCCOLLOUGH JAMES M.;AUBERT ROGER
分类号 B64D15/00 主分类号 B64D15/00
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