A jet engine fan case is disclosed. The fan case may comprise an ice liner section and a rear liner section, wherein the ice liner section and the rear liner section are constructed from a constructed from a single, integral material. The ice liner section may comprise fiberglass and the rear liner section comprises fiberglass, such that the combined liner comprises a single piece. The combined liner may comprise a plurality of segments in the range of one segment to nine segments. The ice liner section may comprise a first cross-sectional profile and the rear liner section may comprise a second cross-sectional profile. The ice liner section may comprise a first cross-sectional profile and the rear liner section may comprise a second cross-sectional profile that is less than the first cross-sectional profile. The combined liner may comprise an uninterrupted aerodynamic surface.
COMBINED FAN CASE ICE LINER AND REAR LINER
KOMBINIERTE EISISOLIERUNG UND HINTERE ISOLIERUNG FÜR VENTILATORGEHÄUSE
CHEMISE ARRIÈRE ET CHEMISE ANTI-GLACE DE CARTER DE VENTILATEUR COMBINÉES
2016-10-12
Patent
Electronic Resource
English
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