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A nickel-based superalloy and gas turbine engine components

A nickel-based superalloy and gas turbine technology, applied in the field of superalloys, can solve the problems of mechanical properties such as fatigue strength, yield strength and ultimate tensile strength, and achieve good mechanical properties, good temperature bearing capacity and stability of the alloy. improved effect

Active Publication Date: 2018-07-17
深圳市万泽中南研究院有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] Although nickel-based superalloys have excellent high-temperature properties such as fatigue resistance, corrosion resistance, and oxidation resistance, nickel-based alloys that have been served at high temperatures for a long time will have obvious mechanical properties such as fatigue strength, yield strength, and ultimate tensile strength. decline

Method used

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  • A nickel-based superalloy and gas turbine engine components
  • A nickel-based superalloy and gas turbine engine components
  • A nickel-based superalloy and gas turbine engine components

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Embodiment Construction

[0025] In order to make the objectives, technical solutions and advantages of the present invention clearer, the technical solutions of the present invention will be clearly described below in conjunction with the embodiments of the present invention. Obviously, the described embodiments are part of the embodiments of the present invention, not all of them. the embodiment. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0026] The sources of the raw materials used in the present invention are not particularly limited, and they can be purchased from the market or prepared according to preparation methods well known to those skilled in the art.

[0027] The superalloy and its prepared articles in the present invention have no special limitation on its preparation method and sources of other raw materials, as long as ...

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Abstract

The invention provides nickel-base superalloy. The nickel-base superalloy is composed of, by mass, 18-20% of Co, 13-15% of Cr, 2.9-3.5% of Al, 3.3-3.7% of Ti, 0.9-1.1% of Ta, 1.8-2.2% of W, 2.5-3.5% of Mo, 0.4-0.6% of Nb, 0.1-0.3% of Hf, 0.02-0.06% of C, 0.003-0.012% of B, 0.02-0.06% of Zr and the balance Ni and inevitable impurities. By optimizing elements of Al, Ti, Nb and Ta, the volume fraction of gamma' is increased, so that the precipitation capacity of harmful phases during the long-time service process at a high temperature of the superalloy material is lowered, and the structure stability of the material is improved. By adjusting the contents of W and Mo, the solution strengthening effect is improved, and the content of TCP phases is lowered. In addition, the contents of Hf and B of the alloy are adjusted, the content of Ta is increased, so that the stability of the gamma' phase and MC phase is improved, and precipitation of a previous particle boundary (PPB) is effectively improved. Accordingly, the harmful phase generation tendency of the nickel-base superalloy during high-temperature long-time service is well eliminated, and the fatigue performance of the alloy material is improved.

Description

technical field [0001] The invention relates to the technical field of superalloys, in particular to a nickel-based superalloy and gas turbine engine components. Background technique [0002] Generally speaking, superalloys refer to high-temperature metal materials that can work for a long time at temperatures above 600°C and under certain stress conditions. performance. With the rapid development of industry, superalloys have shown good application prospects in various fields, and are mainly used to manufacture high-temperature components such as turbine blades, guide vanes, turbine disks, high-pressure compressor disks, and combustion chambers of gas turbine engines. [0003] According to the preparation process, superalloy materials can be divided into deformed superalloys, cast superalloys and powder metallurgy superalloys. Superalloy materials can be divided into iron-based superalloys, nickel-based superalloys and cobalt-based superalloys according to matrix elements...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): C22C19/05
CPCC22C19/056
Inventor 冯赣江孙乃荣熊江英
Owner 深圳市万泽中南研究院有限公司