|국가/구분||United States(US) Patent 등록|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 8 인용 특허 : 5|
An ice protection system and method are provided that facilitate the prevention or reduction in ice formation upon an aerodynamic surface. The ice protection system may include at least one induction coil spaced apart from an electrically conductive layer of an aerodynamic surface and disposed interior of an exterior surface of the aerodynamic surface. For example, the ice protection system may include a plurality of induction coils with each induction coil being spaced apart from the other induction coils such that the respective induction coils are ass...
1. An ice protection system comprising: an engine nacelle inlet having an electrically conductive layer comprising a metallic erosion barrier proximate an exterior surface and an acoustic liner comprising a composite facesheet, a honeycomb core and a composite backsheet positioned interior of the electrically conductive layer, wherein the composite facesheet defines a plurality of perforations and the metallic erosion barrier defines a plurality of perforations aligned and coextensive with respective perforations of the composite facesheet;at least one i...