ASSEMBLY FOR TURBOMACHINE

Disclosed is an assembly for a turbomachine comprising: a first rotor comprising: a disc (120), and a plurality of vanes (122) capable of fluttering relative to the disc (120), a second rotor (140), and a damper (2) configured to dampen a movement of the first rotor relative to the second rotor (140), in a plane orthogonal to the longitudinal axis, the damper (2) comprising: a first bearing portion (21) that comes to bear on the first rotor in a first bearing zone extending over a first angular sector around the longitudinal axis, a second bearing portion (22) that comes to bear on the first rotor in a second bearing zone extending over a second angular sector around the longitudinal axis, and a third bearing portion (23) that comes to bear on the second rotor (140). 本公开是一种用于涡轮机的组件，该组件包括：●第一转子，该第一转子包括：●盘(120)，以及●多个叶片(122)，多个叶片能够相对于盘(120)颤动，●第二转子(140)，以及●阻尼器(2)，该阻尼器被构造成阻尼第一转子相对于第二转子(140)在正交于纵向轴线的平面中的运动，该阻尼器(2)包括：●第一支承部分(21)，该第一支承部分在第一支承区域中支承在第一转子上，该第一支承区域围绕纵向轴线在第一角扇区上延伸，●第二支承部分(22)，该第二支承部分在第二支承区域中支承在第一转子上，该第二支