发明授权
US4786347A Method of manufacturing an annular bladed member having an integral shroud 失效
制造具有整体护罩的环形叶片构件的方法

  • 专利标题: Method of manufacturing an annular bladed member having an integral shroud
  • 专利标题(中): 制造具有整体护罩的环形叶片构件的方法
  • 申请号: US741584
    申请日: 1985-06-05
  • 公开(公告)号: US4786347A
    公开(公告)日: 1988-11-22
  • 发明人: James P. Angus
  • 申请人: James P. Angus
  • 申请人地址: GB2 London
  • 专利权人: Rolls-Royce plc
  • 当前专利权人: Rolls-Royce plc
  • 当前专利权人地址: GB2 London
  • 优先权: GBX8417419 19840707
  • 主分类号: B29C45/00
  • IPC分类号: B29C45/00 B29C45/14 F01D5/28 F01D5/34 B65H81/00
Method of manufacturing an annular bladed member having an integral
shroud
摘要:
A gas turbine engine disc having integral, radially extending aerofoil blades and an integral shroud interconnecting the radially outer extents of the blades is described. In the manufacture thereof continuous fibres are wound around an annular array of inserts provided in a dividable disc. The inserts define the spaces between adjacent blades on the disc. A mixture of chopped carbon fibre and an epoxy resin matrix material is then injected into the central portion of the die interior. Any part of the wound fibres which has not been impregnated by the chopped fibre/resin matrix material is subsequently impregnated by a matrix material whereupon the die is opened to release the thus produced bladed disc.
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