Dual flow turbine engine equipped with a precooler

B - Operations – Transporting – 64 – D

Patent

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Details

B64D 13/08 (2006.01) F02C 7/141 (2006.01) F02K 3/06 (2006.01) F02K 3/075 (2006.01) F02K 3/115 (2006.01)

Patent

CA 2631849

The invention concerns a precooler (30) having an annular cross-sectional shape about the axis (L-L) of the pod and arranged inside the rear part (10R) of the inner shroud (10) in contact with a cold fluid (9) exiting the fan duct (13).

Selon l'invention, le prérefroidisseur (30) présente une forme à section annulaire autour de l'axe (L-L) de la nacelle et est disposé à l'intérieur de la partie arrière (10R) du carénage interne (10) en contact avec le flux froid (9) sortant du canal de soufflante (13).

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