发明申请
US20150329211A1 AIRCRAFT ICE PROTECTION SYSTEM AND METHOD 有权
飞机冰保护系统和方法

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.
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