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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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