发明名称 Dynamic sealing system for sealing labyrinth between internal wall of stator and rotor of turbojet of aircraft, has connection element whose portion is deformable to allow deformation of connection element relative to wall of stator
摘要 <p>The system (12) has a revolution element (20) mounted on an internal wall (24) of a stator. Revolution lips (30) are radially oriented based on rotation of a rotor around a main axis of the stator. External radial ends of the lips move near a face of the revolution element. The revolution element is mounted on the stator via a connection element (32), where an intermediate portion (40) of the connection element is elastically deformable according to a radial direction to allow radial deformation of the connection element relative to the internal wall of the stator.</p>
申请公布号 FR2982314(A1) 申请公布日期 2013.05.10
申请号 FR20110060201 申请日期 2011.11.09
申请人 SNECMA 发明人 GARIN FABRICE, MARCEL, NOEL;BLANCHARD STEPHANE, PIERRE, GUILLAUME;PASQUIS PATRICK, CLAUDE;SCHWEBLEN WILFRIED, LIONEL
分类号 F01D11/02;F01D25/28 主分类号 F01D11/02
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