发明名称 Method of manufacturing a hollow blade for a turbomachine
摘要 In a method of manufacturing a hollow blade for a turbomachine in which a plurality of primary sheet-like parts having anti-diffusion coatings in predefined areas are assembled face to face and diffusion welded together before being deformed to shape by pressurized gas and superplastic forming. The assembly, before being diffusion welded together, is subjected to a preheating treatment in an oven to remove the binder from the anti-diffusion coatings, and then, without moving the assembly, the interior of the assembly is evacuated while simultaneously progressively increasing the temperature at a rate V to a value T to produce a permanent plastic deformation of the parts, the interior of the assembly then being maintained in vacuo at the temperature T while an isostatic pressure is applied to the exterior of the assembly so as to produce a compacting of the anti-diffusion material and a prewelding of the facing areas which are not coated with the anti-diffusion material.
申请公布号 US5896658(A) 申请公布日期 1999.04.27
申请号 US19970951292 申请日期 1997.10.16
申请人 SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION "SNECMA" 发明人 CALLE, GILLES MICHEL GEORGES LOUIS;KLEIN, GILLES CHARLES
分类号 B21D26/02;B21D26/021;B21D26/055;B21D53/78;B23K20/00;B23K20/18;B23P15/04;F01D5/18;F01D25/00;F04D29/38;(IPC1-7):B23P15/00 主分类号 B21D26/02
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