Intermediate casing extension for an aircraft jet engine,...

Details Intermediate casing extension for an aircraft jet engine,... Intermediate casing extension for an aircraft jet engine,...

B - Operations, Transporting

64

D

B64D 29/00 (2006.01) B64C 7/02 (2006.01) B64D 27/10 (2006.01) B64D 29/06 (2006.01) F01D 25/24 (2006.01)

Patent

CA 2647439

The invention relates to an extension (30) of an intermediate casing for an aircraft jet engine, intended to project towards the downstream end from an external shell of the intermediate casing, this extension comprising an annular connecting downstream end (64) forming an annular groove (66) open radially towards the outside, intended to receive nacelle covers. According to the invention, the annular connecting downstream end (64) is produced by means of a plurality of angular sectors (76a, 76b).

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