首页> 外国专利> Applying material layer on workpiece made of material containing titanium aluminide, comprises heating workpiece by induction at preheating temperature and applying powdery additive on heated surface of workpiece by deposition welding

Applying material layer on workpiece made of material containing titanium aluminide, comprises heating workpiece by induction at preheating temperature and applying powdery additive on heated surface of workpiece by deposition welding

机译:在由含铝化钛的材料制成的工件上施加材料层,包括在预热温度下通过感应加热工件,以及通过熔敷焊接在工件的受热表面上施加粉末状添加剂

摘要

Applying at least one material layer on a workpiece (10) made of a material containing titanium aluminide, comprises: heating the workpiece in a locally restricted area by induction at a provided preheating temperature; and applying a powdery additive on the heated surface of the workpiece by deposition welding, preferably laser-, laser-powder-, plasma-, micro plasma-, tungsten inert gas or micro tungsten inert gas-deposition welding, where the additive comprises titanium aluminide. Independent claims are also included for: (1) surface finishing, plating, dimensional correction or repairing the workpiece, comprising preparing the workpiece, and applying at least one layer of the additive; (2) plating, dimensional correction or repairing the surface of a shank, preferably acute angled groove of a component made of the material containing titanium aluminide, where a zone of the workpiece in a region of a groove-radius (14) is not heated by a predetermined additional critical temperature of the material depending on the shape of the groove, and a coil is used for inductive heating of the workpiece and/or its position is adjusted relative to the groove in the groove, preferably its shape; (3) plating, dimensional correction or repairing a functional area of a Z-groove of a top cover strip of a turbine blade, a sealing fin on a turbine bladed discs, a blade tip of a compressor rotor blade or a portion of a casing of a turbo-machine; (4) producing a workpiece, preferably a turbine- or compressor blade, or a turbine- or compressor housing, or any of their parts, comprising preparing a substrate made of the material containing titanium aluminide, and applying a layer of at least one additive until a predetermined contour of the workpiece is formed or packed; (5) a device for applying material layers on the workpiece by deposition welding, comprising a holding device for holding the workpiece, a feeding device for feeding a powdery, titanium aluminide-containing additive, a melting device for melting the additive, where the melting device is arranged for generating a laser- or plasma jet and for directing the laser- or plasma jet on the workpiece, and a preheating device for preheating the workpiece. A device is designed and equipped for carrying out the above mentioned method. The preheating device is designed and equipped for inductive, locally restricted heating the surface of the workpiece; and (6) a workpiece with at least one material layer.
机译:在由包含铝化钛的材料制成的工件(10)上施加至少一个材料层包括:通过在提供的预热温度下感应加热在局部受限区域中的工件;通过沉积焊接,优选地通过激光,激光粉末,等离子,微等离子体,钨极惰性气体或微钨极惰性气体沉积焊接在工件的加热表面上施加粉末状添加剂,其中添加剂包括铝化钛。还包括以下方面的独立权利要求:(1)对工件进行表面精加工,电镀,尺寸校正或修复,包括制备工件,并施加至少一层添加剂。 (2)电镀,尺寸校正或修复柄的表面,最好是由含铝化钛的材料制成的零件的锐角槽,其中工件的在槽半径(14)区域内的区域没有加热通过取决于凹槽的形状的材料的预定的另外的临界温度,并且线圈被用于感应加热工件和/或其相对于凹槽在凹槽中的位置被调节,优选是其形状。 (3)电镀,尺寸校正或修复涡轮机叶片顶盖条的Z形槽的功能区域,涡轮机叶片盘上的密封鳍片,压缩机转子叶片的叶片尖端或一部分壳体涡轮机的; (4)生产工件,优选为涡轮机或压缩机叶片,或涡轮机或压缩机壳体,或其任何部件,包括制备由包含铝化钛的材料制成的基底,并施加至少一种添加剂的层直到形成或填充工件的预定轮廓; (5)一种用于通过熔敷焊接在工件上施加材料层的设备,包括:用于保持工件的保持设备;用于进给粉末状的含铝化钛的添加剂的进给设备;用于熔化添加剂的熔化设备,其中装置被布置用于产生激光束或等离子体束并且用于将激光束或等离子体束引导到工件上,以及用于预热工件的预热装置。设计并装备了用于执行上述方法的设备。预热装置的设计和装备是感应地局部加热工件表面。 (6)具有至少一层材料层的工件。

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