A kind of preparation method of red copper and nickel base superalloy laminated composite component

A technology for nickel-based superalloys and composite components, applied in metal processing equipment, manufacturing tools, welding equipment, etc., can solve the problems of low material utilization rate and dust pollution, and achieve high-quality connection, high production efficiency, and joint interface stress. low effect

Active Publication Date: 2018-01-30
丹阳市金星镍材有限公司
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  • Abstract
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Problems solved by technology

At present, there are few studies on the welding of red copper and nickel-based superalloy dissimilar materials. The research mainly focuses on nickel-based corrosion-resistant alloy powder on the surface of red copper by thermal spraying or powder-feeding laser stacking to increase the corrosion resistance of red copper components. or hardness, and when powder materials are used, the material utilization rate is low, and there are problems such as dust pollution

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  • A kind of preparation method of red copper and nickel base superalloy laminated composite component
  • A kind of preparation method of red copper and nickel base superalloy laminated composite component
  • A kind of preparation method of red copper and nickel base superalloy laminated composite component

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Embodiment Construction

[0023] In order to make the purpose, technical solution and advantages of the present invention more clear, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention.

[0024] Such as figure 1 The size of the red copper and nickel-based superalloy composite component shown is 100mm×100mm×20mm, of which the copper component 1 (copper plate) is 12mm thick and the grade is T1; the nickel-based superalloy component 3 is GH3030, the thickness is 6mm, and the transition layer 2 is about 2mm thick.

[0025] Welding process platform: The processing device is composed of Fronius TPS400TIG power supply, IPG company YLS-6000 fiber laser heat source, Fronius wire feeder and KUKA robot; during processing, the heat source head and wire feeder tip are fixed on the KUKA robo...

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Abstract

The invention discloses a preparation method of a laminated composite structural member of red copper and nickel-base superalloy. The preparation method comprises the following steps of firstly, preparing a red copper structural member, and performing cleaning and preheating treatment on the red copper structural member; then, preparing a transition surfacing layer on the combined surface of the red copper structural member and the nickel-base superalloy by adopting a filler rod type TIG welding technology; and performing surfacing on the nickel-base superalloy structural member on the transition surfacing layer by adopting a silk feeding type laser or arc direct-melting depositing technique so as to obtain the laminated composite structural member of the red copper and the nickel-base superalloy, which consists of the red copper structural member, the transition surfacing layer and the nickel-base superalloy structural member. According to the preparation method disclosed by the invention, an applicable transition surfacing layer is prepared, so that the welding problem of the red copper and the nickel-base superalloy is effectively solved, and the laminated composite structural member has the characteristics of being high in production efficiency, good in mechanical property, long in service life, small in influence by the shape and the dimension of the mechanical property, wide in application range and the like.

Description

technical field [0001] The invention specifically relates to a preparation method of a red copper and nickel-based superalloy laminated composite component. Background technique [0002] In engineering components such as high-temperature nozzles, it is often required that the high-temperature side combined with the heat source has good high-temperature resistance, while the other side has good thermal conductivity. At present, the laminated composite structure of ceramics and red copper is mostly used, but the hardness and brittleness of ceramics are high, it is difficult to process, and it is greatly affected by geometric shape and size; at the same time, due to the great difference in thermophysical and mechanical properties of ceramics and metals, the two There are large thermal stress and residual stress at the welding joint interface, which is easy to cause cracks and fractures on the ceramic side, which in turn affects the life of the components. In addition, brazing ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B23K9/167B23K9/235B23K9/04B23K10/02B23K26/342B23K35/30B23K103/22
CPCB23K9/04B23K9/167B23K9/235B23K10/027B23K35/3033B23K35/304B23K2103/18B23K2103/22
Inventor 胥国祥杜宝帅
Owner 丹阳市金星镍材有限公司
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