发明名称 AIRCRAFT ICE PROTECTION SYSTEM AND METHOD
摘要 A system and method for ice protection of a component, wherein the system is adapted to be adhesively bonded to a surface of the component. The system includes a heating element layer, at least one thermally conductive adhesive layer that adhesively bonds a first side of the heating element layer to the component, an insulation layer, at least one thermally insulating adhesive layer that adhesively bonds a second side of the heating element to the insulation layer, an electrical bus bar adapted to provide a connection between a power supply and the heating element layer, and at least one temperature sensor.
申请公布号 US2014014640(A1) 申请公布日期 2014.01.16
申请号 US201213680177 申请日期 2012.11.19
申请人 MRA SYSTEMS INC.;KELLY AEROSPACE THERMAL SYSTEMS, LLC;KELLY AEROSPACE THERMAL SYSTEMS, LLC;MRA SYSTEMS INC. 发明人 CALDER DAVID PATRICK;OPIFICIUS JULIAN ALEXANDER;PEDERSON ERIK THOMAS;FLOSDORF DAVID CENIT
分类号 B64D15/12 主分类号 B64D15/12
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