发明申请
- 专利标题: BLISK COMPRISING A HUB HAVING A RECESSED FACE ON WHICH A FILLING MEMBER IS MOUNTED
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申请号: US15554936申请日: 2016-03-01
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公开(公告)号: US20180087389A1公开(公告)日: 2018-03-29
- 发明人: Philippe Gérard Edmond Joly , François Jean Comin , Laurent Jablonski , Damien Merlot , Jean-Marc Claude Perrollaz
- 申请人: Safran Aircraft Engines
- 优先权: FR1551736 20150302
- 国际申请: PCT/FR2016/050460 WO 20160301
- 主分类号: F01D5/34
- IPC分类号: F01D5/34
摘要:
A fan blisk for a turbomachine, the blisk comprising a hub delimited by an upstream face and a downstream face in addition to an outer peripheral face and a revolving inner peripheral face delimiting an inner opening, the hub carrying blades each having a leading edge and a trailing edge, the hub and the blades forming a one-piece assembly. The upstream face and/or the downstream face is offset, being located along the axis of rotation (AX) between the leading edges and the trailing edges of the blades, the blisk (bladed disk) comprising a filling member mounted on the offset face, the filling member comprising an inner centring ferrule engaging in the inner face of the hub, a radial portion resting against the offset face and an outer ferrule extending the outer peripheral face of the hub.
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