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The box fin of the multiplex operation press reactor null turbine engine which is used for the execution of manner and the said manner which produce the

机译:多重操作压力反应堆空涡轮发动机的箱形翅片用于执行方式和所述方式来产生气体。

摘要

PROBLEM TO BE SOLVED: To provide a method of manufacturing a hollow blade of a turbine engine, made of a TA6V-type titanium alloy, capable of the additional work of parts forming due to unrisky torsion inducing a buckling type undulatory motion along a central fibrous structure, and a multiple operating press furnace in combination. ;SOLUTION: A long fibrous structure in an element is secured, namely, as adjusting a deformative speed so as to have various fibrous structures of the element extended by a distrubution controlled at both sides of a central fibrous structure, this method comprises a hot-forming job by means of isothermally forming a blade 9 at a temperature within 700°C to 940°C under the action between at least two punches 46 and one hole-down 45 to lock this blade 9 placed on a forming die 21.;COPYRIGHT: (C)1998,JPO
机译:要解决的问题:提供一种制造涡轮发动机空心叶片的方法,该叶片由TA6V型钛合金制成,由于不易扭转,会导致沿中心纤维的屈曲型起伏运动,从而能够完成零件成型的附加工作。结构,与多操作压力炉结合使用。 ;解决方案:固定元件中的长纤维结构,即调节变形速度,以使该元件的各种纤维结构通过中心纤维结构两侧的分布控制而延伸,该方法包括热通过在至少两个冲头46和一个向下的孔45之间的作用下在700℃至940℃之间的温度下等温地形成刀片9以将刀片9锁定在成形模具21上而等温地形成刀片9; COPYRIGHT :(C)1998,日本特许厅

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