发明名称 HEATING DESIGN FOR ROTORCRAFT BLADE DE-ICING AND ANTI-ICING
摘要 A heater mat assembly for a blade using an electrical current is provided including a first heating element region configured to generate a first amount of heat using the electrical current and disposed at a first region of the heater mat assembly. A second heating element region extends form the first heating element region and is configured to generate a second amount of heat using the electrical current. The second amount of heat is different than the first amount of heat.
申请公布号 WO2016144683(A1) 申请公布日期 2016.09.15
申请号 WO2016US20625 申请日期 2016.03.03
申请人 SIKORSKY AIRCRAFT CORPORATION 发明人 ZHAO, Wenping;CHAUDHRY, Zaffir A.;WANG, Jinliang;NGUYEN, Dean
分类号 B64D15/12;B64C27/46;B64C27/473;B64D15/14;B64D15/22;H05B3/34 主分类号 B64D15/12
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