Recessed engine nacelle

Details Recessed engine nacelle Recessed engine nacelle

B - Operations, Transporting

64

D

B64D 27/00 (2006.01) B64C 7/02 (2006.01)

Patent

CA 2514385

A gas turbine engine nacelle (16) includes an inner skin (38) surrounded by a radially outer skin (40). The inner skin (38) terminates at an exhaust outlet (44). The outer skin (40) terminates at a recess (46) in the inner skin (38) extending into a closed cavity (48) under the outer skin (40).

L'invention concerne un carter-moteur pour turbine à gaz (16), qui comprend un revêtement intérieur (38) entouré par un revêtement extérieur radial (40). Le revêtement intérieur (38) se termine en un orifice d'échappement (44). Le revêtement extérieur (40) aboutit dans un retrait (46) ménagé dans le revêtement intérieur (38) s'étendant à l'intérieur d'une cavité fermée (48) sous le revêtement extérieur (40).

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