| 摘要 |
The present invention relates to a turbomachine rotor, particularly to the attachment of the blades ( 2 ), particularly the fan blades, to a rotor disk ( 4 ). The invention relates in particular to a turbomachine rotor comprising a disk ( 4 ) the periphery of which has a plurality of slots ( 41 ), a plurality of removable blades ( 2 ), each blade ( 2 ) comprising a blade root ( 22 ) housed in one of the slots ( 41 ), and a downstream flange ( 7 ), secured to said disk ( 4 ) and against which each blade root ( 22 ) bears. According to the invention, the rotor comprises, between each blade root ( 22 ) and the downstream flange ( 7 ), an elastic buffer ( 8 ) intended to maintain a gap between the blade root ( 22 ) and the downstream flange ( 7 ).
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