Fan rotor for an airplane turbojet engine

Details Fan rotor for an airplane turbojet engine Fan rotor for an airplane turbojet engine

F - Mech Eng,Light,Heat,Weapons

04

D

F04D 29/32 (2006.01) F01D 5/30 (2006.01)

Patent

CA 2760470

The invention relates to the locking of the blade roots in the respective slots of a fan rotor in an airplane turbojet engine. According to the invention, each blade root (17) is received in a slot closed by a main latch (28) and an additional latch (32) separate from the main latch and spaced apart therefrom by a predetermined distance.

Verrouillage des pieds d'aubes dans les rainures respectives d'un rotor de soufflante de turboréacteur d'avion. Selon l'invention, chaque pied d'aube (17) est logé dans une rainure fermée par un verrou principal (28) et un verrou supplémentaire (32) distinct du verrou principal et espacé de celui-ci d'une distance prédéterminée.

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