发明名称 Welding method of two parts of a blade.
摘要 A process is claimed for the welding of the two parts of a rotor blade (9,10), in which a flange (15) of sacrificial material is arranged between the contact surfaces (16,17) or around them in order to augment the heat produced by the rubbing of the leading edges and the flight of the rotor blade. The two parts of the rotor blade (9,10) are inserted between some pairs of jaws (1,2) and put in contact at their contact surfaces (16,17) by bringing the jaws together. The welding process used may be a linear friction welding process, a spark welding process or a forging and fusion welding process.
申请公布号 EP0669183(A1) 申请公布日期 1995.08.30
申请号 EP19950400354 申请日期 1995.02.21
申请人 SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION, "S.N.E.C.M.A." 发明人 COLLOT, ANDRE CLAUDE FELIX;FERTE, JEAN-PIERRE;JOLLY, ROGER
分类号 B23K11/04;B23K20/12;B23K37/04;F01D5/12 主分类号 B23K11/04
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