|국가/구분||United States(US) Patent 등록|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 1 인용 특허 : 35|
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 heati...
1. A method of protecting a component on an aircraft from ice formation, the method comprising: forming a heating element layer;attaching an electrical bus bar to the heating element layer;encapsulating the heating element layer, at least one thermal sensor, and the electrical bus bar to form a laminated structure, wherein a first thermally conductive adhesive layer is disposed at a first side of the laminated structure and a first thermally insulating adhesive layer is disposed at a second side of the laminated structure;curing the laminated structure;a...