Gamma''strengthened high performance casting nickel-based high-temperature alloy

A high-performance nickel-based superalloy technology, applied in the field of industrial technology-metal material science, can solve the problems of rapid decline in alloy strength and durable life, and achieve good structural stability and excellent tensile properties

Active Publication Date: 2009-02-25
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

[0007] The purpose of the present invention is to overcome the shortcoming of rapid decline in alloy strength and durable life when the working temperature of K4169 alloy exceeds about 650°C, especially to provide a γ” strengthened High performance casting nickel base superalloy

Method used

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  • Gamma''strengthened high performance casting nickel-based high-temperature alloy
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  • Gamma''strengthened high performance casting nickel-based high-temperature alloy

Examples

Experimental program
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Effect test

Embodiment 1

[0015] The alloy of the present invention (No.1 alloy), the alloy composition is shown in Table 1.

[0016] The smelting process adopted is: after the master alloy is melted and cleaned, it is refined at 1500°C for 10 minutes, cooled to 1400°C for pouring, and the shell temperature is 800°C. The heat treatment system adopted is: 1180°C, 4 hours, air cooling→775°C, 4 hours, furnace cooling to 700°C→700°C, 10 hours, air cooling.

[0017] Table 1 No.1 alloy composition, wt%

[0018] Cr co A1 Ti Nb Ta Mo C B Y Ni 18.0 12.0 0.5 1.0 4.0 3.0 3.0 0.015 0.020 0.05 Bal

[0019] Table 2 Mechanical properties of No.1 alloy and its comparison with that of K4169

[0020]

[0021] The mechanical properties of No.1 alloy and its comparison with that of K4169 are shown in Table 2. It can be seen that the room temperature tensile yield strength and fracture strength of the invented No.1 alloy are not much improved compared with the K4169 alloy, ...

Embodiment 2

[0023] The No.2 alloy composition of the present invention is shown in Table 3, and the smelting and heat treatment process is the same as that of Example 1.

[0024] Table 3 No.2 alloy composition, wt%

[0025] Cr co A1 Ti Nb Ta Mo C B Y Ni 18.0 12.0 0.5 1.0 3.0 5.0 3.0 0.015 0.020 0.05 Bal

[0026] Table 4 shows the mechanical properties of No.2 alloy of the present invention and its comparison with that of K4169. It can be seen that the room temperature, 700°C tensile yield strength, fracture strength and 700°C / 580MPa durability life of No.2 alloy are significantly improved compared with K4169 alloy.

[0027] Table 4 Mechanical properties of No.2 alloy and its comparison with that of K4169

[0028]

Embodiment 3

[0030] The composition of No.3 alloy of the present invention is shown in Table 5, and the smelting and heat treatment process is the same as that of Example 1.

[0031] Table 5 No.3 alloy composition, wt%

[0032] Cr co Al Ti Nb Ta Mo W C B Y Ni

18.0

12.0

0.5

1.0

3.0

5.0

3.0 2.0 0.01

5 0.02

0 0.05 Bal

[0033] Table 6 shows the mechanical properties of No.3 alloy of the present invention and its comparison with that of K4169. It can be seen that the room temperature, 700°C tensile yield strength, fracture strength and 700°C / 580MPa durability life of No.3 alloy are significantly improved compared with K4169 alloy.

[0034] Table 6 Mechanical properties of No.3 alloy and its comparison with that of K4169

[0035]

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Abstract

The invention provides a gamma' intensified high-performance cast nickel-based high-temperature alloy, which is characterized in that the alloy comprises the compositions by weight percentage as follows: 0.007 to 0.07 percent of C, 0.007 to 0.09 percent of B, 0 to 0.10 percent of Ce, 0 to 0.10 percent of Y, 10.0 to 15.0 percent of Co, 15.0 to 20.0 percent of Cr, 1.0 to 4.0 percent of Mo, 0.2 to 3.0 percent of Al, 0.5 to 3.0 percent of Ti, 0 to 3.0 percent of W, 2.0 to 6.0 percent of Nb, 0 to 6.0 percent of Ta, and the residual amount of Ni, wherein, the contents of impurities by weight percentage are as follows: less than or equal to 0.01 percent of S, less than or equal to 0.01 percent of P, less than or equal to 0.2 percent of Si, less than or equal to 0.0005 percent of Pb, less than or equal to 0.0001 percent of Bi, less than or equal to 0.2 percent of Mn, and less than or equal to 0.5 percent of Fe. The invention changes the alloying compositions, not only has higher high-temperature mechanical performance, but also has excellent long-term application structural stability at 700 DEG C, and can meet the requirement of a cartridge receiver of an airspace engine or an aero-engine with higher service temperature and higher performance requirement.

Description

technical field [0001] The invention relates to industrial technology-metal material science, and particularly provides a γ"-strengthened high-performance casting nickel-based superalloy. Background technique [0002] Inconel 718 alloy was successfully developed by H.L.Eiselstein of INCO Alloys International Huntington Branch (Huntington), and was published in 1959. It is a body-centered tetragonal Ni3Nb (γ") and face-centered cubic Ni3 ( Al, Ti, Nb) (γ') precipitation strengthened nickel-chromium-iron-based deformed superalloy. The alloy has high tensile strength, yield strength, durable strength and plasticity between -253 and 650 ° C, and has Good corrosion resistance, radiation resistance, thermal processing and welding performance. [0003] In the context of the rapid development of superalloy overall precision casting technology, Inconel 718 alloy, originally developed as a deformed superalloy, has also been used in the aerospace industry in the form of casting alloy ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): C22C19/05
Inventor 陈伟李辉楼琅洪
Owner INST OF METAL RESEARCH - CHINESE ACAD OF SCI
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