INTERNAL ANTI-ICING EQUIPMENT FOR TURBO FAN ENGINE

PROBLEM TO BE SOLVED: To provide a system and a method to prevent the icing on an internal surface of a turbo fan engine 10 or to remove the ice from the internal surface. SOLUTION: A splitter area 18 combined with a booster compressor of the turbo fan engine 10 is specified. The splitter area 18 ha...

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Bibliographische Detailangaben
Hauptverfasser: WADIA ASPI R, HOLM RAYMOND G
Format: Patent
Sprache:eng
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Zusammenfassung:PROBLEM TO BE SOLVED: To provide a system and a method to prevent the icing on an internal surface of a turbo fan engine 10 or to remove the ice from the internal surface. SOLUTION: A splitter area 18 combined with a booster compressor of the turbo fan engine 10 is specified. The splitter area 18 has the internal surface of the turbo fan engine 10 exposed to an inlet icing condition. A resin body 26 is molded along a front edge of the splitter area 18, an electric coil 24 is mounted inside of the resin body 26, and the accumulation of ice on the splitter area 18 is prevented, or the ice is removed from the splitter area 18 during the icing condition. COPYRIGHT: (C)2004,JPO