发明名称 COMPOSITE BLADE COMPRISING A PLATFORM EQUIPPED WITH A STIFFENER
摘要 Fibrous preform for a turbomachine blade and monobloc blade that can be formed from such a preform, bladed disk and turbomachine comprising such a blade; the fibrous preform, obtained by three-dimensional weaving, comprising a first longitudinal section able to form a blade root (21), a second longitudinal section extending the first longitudinal section upwards and able to form an air foil part (22), a first transverse section extending transversely from the junction between the first and second longitudinal sections and able to form a first platform (23), and a first stiffening strip extending downwards form the distal end of the first transverse section and able to form a first platform stiffener (25).
申请公布号 WO2016066954(A1) 申请公布日期 2016.05.06
申请号 WO2015FR52898 申请日期 2015.10.28
申请人 SNECMA 发明人 MARIN, SÉBASTIEN;DE GAILLARD, THOMAS ALAIN;LAGUERRE, AUDREY
分类号 B29B11/16;B29L31/08;F01D5/28 主分类号 B29B11/16
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