Device to join two tubular parts from an aircraft turbojet...

Details Device to join two tubular parts from an aircraft turbojet... Device to join two tubular parts from an aircraft turbojet...

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 25/24 (2006.01) F02C 7/045 (2006.01)

Patent

CA 2428167

According to the invention, a rigid ring (31) with an at least approximately S-shaped cross section is housed in a recess (32) of the core of the acoustic protection (14) of the rear part (11R) of the piece (11) and is secured to the latter.

- Selon l'invention, un anneau rigide (31) à section au moins approximativement à la forme d'un S est logé dans un évidement (32) de l'âme de la protection acoustique (14) de la partie arrière (11R) de la pièce (11) et est solidarisé de cette dernière.

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