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METHOD FOR WELDING BLADES to the drum axial compressor friction welding and related devices

机译:将叶片焊接到滚筒轴向压缩机的摩擦焊方法及相关装置

摘要

1. A method of attaching the blades (18, 20, 22) to the rotor (14) an axial turbomachine (2) by friction welding, comprising the steps of: a) placing the rotor (14) for providing the surface (38) for coupling one of the blades ; b) begin moving blade frictional motion (18, 20, 22) relative to the surface (38) coupling to the blade (18, 20, 22), preferably in the median plane of contact between the blade and said surface to achieve the welding temperature, wherein the rotor (14 ) is held in a fixed position in the plane of movement of the friction l patki (18, 20, 22); and c) immobilize blade (18, 20, 22) and prokovyvayut blade (18, 20, 22) to the rotor (14), wherein the movement blade (18, 20, 22) in step (b) is orbitalnym.2. A method according to claim 1, characterized in that the rotor is a drum (14) of the compressor, preferably comprising a hollow body (16) having a generally circular symmetry about the rotor axis and defining an internal cavity with a first opening in the front end of the drum and a second hole in tortse.3 back. A method according to claim 1, characterized in that step (a) includes positioning the support (51) in the rotor (14) on the inner surface opposite to the surface (38) interface designed for the blade, for fixing said surface relative to conjugation forging pressure acting on the blade (18, 20, 22) in step (c) .4. A method according to claim 1, characterized in that the bearing arrangement (51) in the drum (14) comprises a drum insert (14) of the core (52), wherein the core is the basis for the support (51) opposite the inner surface of the drum, said core is preferably positioned along at IU
机译:1.一种通过摩擦焊接将叶片(18、20、22)附接到轴向涡轮机(2)的转子(14)上的方法,该方法包括以下步骤:a)放置转子(14)以提供表面(38) )用于联接叶片之一; b)开始移动叶片相对于联接至叶片(18、20、22)的表面(38)的摩擦运动(18、20、22),优选地在叶片与所述表面之间的接触的中间平面中以实现焊接温度,其中转子(14)在摩擦力l patki(18、20、22)的运动平面中保持在固定位置; c)将叶片(18、20、22)和前导叶叶片(18、20、22)固定在转子(14)上,其中步骤(b)中的运动叶片(18、20、22)是轨道性的。 2.根据权利要求1所述的方法,其特征在于,所述转子是所述压缩机的鼓(14),优选地包括中空体(16),所述中空体关于所述转子轴线具有大致圆形的对称性,并且限定了在所述转子中具有第一开口的内部空腔。鼓的前端和tortse.3后面的第二个孔。 2.根据权利要求1所述的方法,其特征在于,步骤(a)包括将所述支撑件(51)定位在所述转子(14)中与所述叶片设计的表面(38)界面相对的内表面上,以相对于所述叶片固定所述表面。步骤(c)中作用在叶片(18、20、22)上的共轭锻造压力.4。 2.根据权利要求1所述的方法,其特征在于,所述鼓(14)中的所述轴承装置(51)包括所述芯(52)的鼓插入件(14),其中,所述芯是与所述芯相对的支撑件(51)的基础。滚筒的内表面,所述芯优选沿IU定位

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