Turboprop aircraft engine

B - Operations – Transporting – 64 – D

Patent

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Details

B64D 33/02 (2006.01) F02C 7/04 (2006.01) F02C 7/052 (2006.01)

Patent

CA 2424497

The invention relates to a turboprop aircraft engine with at least one outer air intake 1 and with at least one downstream inner duct system 2 for the delivery of air to a compressor, characterized in that the inner duct system 2 spirals around the center axis of the engine.

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