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A nickel-cobalt-based deformed superalloy and its preparation method

A technology for deforming high-temperature alloys and high-temperature alloys, which is applied in the field of high-temperature alloys

Active Publication Date: 2021-07-06
INST OF METAL RESEARCH - CHINESE ACAD OF SCI
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, there is currently no related technology for strengthening alloys by introducing special grain boundaries in nickel-cobalt-based wrought superalloys

Method used

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  • A nickel-cobalt-based deformed superalloy and its preparation method
  • A nickel-cobalt-based deformed superalloy and its preparation method
  • A nickel-cobalt-based deformed superalloy and its preparation method

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preparation example Construction

[0051] Specifically, the preparation method of the nickel-cobalt-based deformed superalloy provided in the embodiment of the present invention includes the following steps:

[0052] Solution treatment: the hot-rolled sheet (that is, the nickel-cobalt-based superalloy after hot-rolling treatment) is solution-treated at a temperature of 0.85-0.95Tm for 2-4h, and then water-cooled to room temperature, and the solution-treated sheet is Pickling and drying. Here, the Tm mentioned in the present invention refers to the melting point temperature of the nickel-cobalt-based superalloy.

[0053] Deformation treatment: cold rolling the plate after solid solution treatment with a total deformation of 50-80%, lubricated with emulsion, and the reduction rate of each pass is 10-15%.

[0054] Annealing treatment: Before annealing, wash and dry the cold-rolled sheet with alkali, then anneal the cold-rolled sheet at a temperature of 0.8-0.9Tm in a vacuum or a hydrogen-reducing environment for ...

Embodiment 1

[0062] In this embodiment, a nickel-cobalt-based deformed superalloy is prepared, which includes the following steps:

[0063] Preparation of ingots: Put the raw materials into a high-frequency vacuum induction melting furnace, heat the temperature to 1500°C, and the vacuum degree is 0.5×10 -2Pa, after all the raw materials are melted, it is refined at a temperature of 1550°C for 6 minutes, and then an inert gas is introduced, and a crucible is cast into an ingot. Among them, the formula of raw materials is as follows: Co 25%, Ta 2%, Cr 15%, Ti 5.5%, Al 2%, W 2%, Mo 2%, Nb 1%, Mn 0.5%, V 0.1%, C 0.003% , Zr 0.02%, B 0.02%, and the balance is Ni. Among them, the Tm of the nickel-cobalt-based superalloy is 1335°C, and the solid solution temperature of the precipitated phase is 1160°C.

[0064] Preparation of electroslag refining ingot: After the ingot is cooled, cut the riser of the ingot and polish the surface, use the polished ingot as the electrode of electroslag remelting,...

Embodiment 2

[0072] In this embodiment, a nickel-cobalt-based deformed superalloy is prepared, which includes the following steps:

[0073] Preparation of ingots: Put the raw materials into the high-frequency vacuum induction melting furnace according to the above ratio, heat the temperature to 1600°C, and the vacuum degree is 0.6×10 -2 Pa, after all the raw materials are melted, refine at a temperature of 1550°C for 5 minutes, then pass in an inert gas, and cast a crucible into an ingot. Among them, the formula of raw materials is as follows: Co 25%, Ta 2%, Cr 15%, Ti 5.5%, Al 2%, W2%, Mo 2%, Nb 1%, Mn 0.5%, V 0.1%, C 0.003%, Zr 0.02%, B 0.02%, and the balance being Ni. Among them, the Tm of the nickel-cobalt-based superalloy is 1335°C, and the solid solution temperature of the precipitated phase is 1160°C.

[0074] Preparation of electroslag refining ingot: After the ingot is cooled, cut the riser of the ingot and polish the surface, use the polished ingot as the electrode of electrosl...

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Abstract

The invention relates to a nickel-cobalt-based deformed superalloy and a preparation method thereof, and relates to the technical field of superalloys. The technical solution mainly adopted is: the nickel-cobalt-based deformed superalloy has special grain boundaries, and the volume fraction of the special grain boundaries is ≥ 25%. The preparation method of the nickel-cobalt-based deformed superalloy comprises the following steps: performing solution treatment on the nickel-cobalt-based superalloy after the hot rolling treatment; performing a total deformation of the nickel-cobalt-based superalloy after the solution treatment to 50- 80% cold rolling; in a vacuum or hydrogen reduction environment, anneal the deformed nickel-cobalt-based superalloy at a temperature of 0.8-0.9Tm for 5-30min; perform aging treatment on the annealed nickel-cobalt-based superalloy , to obtain nickel-cobalt-based deformation superalloy. The invention is mainly used to introduce special grain boundaries into nickel-cobalt-based deformed superalloys, increase the volume fraction of special grain boundaries, and improve the strength of alloys without increasing the degree of alloying. It is a nickel-cobalt-based deformed superalloy as High temperature structural parts provide strength guarantee.

Description

technical field [0001] The invention relates to the technical field of high-temperature alloys, in particular to a nickel-cobalt-based deformed high-temperature alloy and a preparation method thereof. Background technique [0002] Superalloys are key materials in the fields of aviation power, gas turbines, supercritical power plants, nuclear energy and petrochemicals, and their performance is an important symbol that determines the level of national technological development. Plates or foils of wrought superalloys can be used as thermal protection components for aircraft outer panels, flame tubes or combustion chambers of engines; these applications have harsh service environments and require wrought superalloys to be lightweight, heat-resistant, corrosion-resistant, and long-lasting at high temperatures. characteristics, to meet the lightweight and high Mach performance index of the aircraft, so that it has excellent maneuverability. [0003] With the development of techno...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): C22C19/05C22C30/00C22F1/10C22F1/02C22C1/02
CPCC22C1/023C22C19/055C22C19/056C22C30/00C22F1/002C22F1/02C22F1/10
Inventor 张瑞王新广崔传勇周亦胄孙晓峰
Owner INST OF METAL RESEARCH - CHINESE ACAD OF SCI