发明名称 HOLLOW FAN BLADE FOR TURBINE ENGINE AND METHOD OF MANUFACTURING SUCH A BLADE
摘要 The invention relates to a method of manufacturing a single-piece hollow fan blade for turbine engines comprising a foot (2) extended by a rotor blade (4) in a radial direction, the method comprising the following stages: - making via forging of a single-piece fan blade (1) with a plurality of inserts; and - eliminating of the inserts so as to obtain a plurality of recesses (16) in this blade. The invention also relates to such a blade (1) fitted with a plurality of recesses (16) each extending substantially and radially along a curved central line (18).
申请公布号 CA2467839(A1) 申请公布日期 2004.11.27
申请号 CA20042467839 申请日期 2004.05.19
申请人 SNECMA MOTEURS 发明人 FRANCHET, JEAN-MICHEL PATRICK MAURICE;LHOMME, DANIEL GASTON;LORIEUX, ALAIN;DESPREAUX, JEAN-LOUIS;LEVEQUE, STEPHANE ANDRE
分类号 F04D29/38;B21J5/00;B21K3/04;B23P15/02;F01D5/14;F01D5/18;(IPC1-7):F01D5/18 主分类号 F04D29/38
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