Foreign object damage tolerant nacelle anti-icing system

Details Foreign object damage tolerant nacelle anti-icing system Foreign object damage tolerant nacelle anti-icing system

B - Operations, Transporting

64

C

B64C 7/02 (2006.01) B64D 15/02 (2006.01) B64D 15/20 (2006.01) B64D 33/02 (2006.01) F01D 25/02 (2006.01) F02C 7/047 (2006.01) F02C 7/14 (2006.01)

Patent

CA 2509788

A nacelle for housing a gas turbine engine is disclosed. The nacelle comprises an inlet lip defining a leading edge of the nacelle and a conduit located within the inlet lip, the conduit having a fluid circulating therein. The fluid provides a heat source. An energy attenuating member is located within the inlet lip between the leading edge and the conduit. The energy attenuating member provides protection to the conduit from foreign object damage and is thermally conductive such that heat transfer communication between the conduit and the leading edge is provided.

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