Mandrel for use in a method of making a composite flange
申请(专利)号:
GB20090017320
申请日期:
2007-06-07
公开/公告号:
GB2470087A
公开/公告日期:
2010-11-10
申请(专利权)人:
GKN AEROSPACE SERVICES LIMITED
摘要:
The mandrel (3) is curved and comprises a solid triangular cross-section; composite material is applied to external surfaces of the curved mandrel (3) and is cured to produce the flange which comprises a curved hollow member with a triangular cross-section. The mandrel (3) comprises at least two parts which can be dismantled for removal from the formed flange; these parts can be segments (3A, 3B) with mitred surfaces, one on top of the other optionally with end plates. Alternatively, the parts can be tessellating sections joined together. As a further option, the mandrel can be of soluble material. The formed flange is mounted on a pipe to form a structure which can be joined with another like structure or a further structural element, e.g. in aircraft construction.
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