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High temperature yield strength improvement process of gh4738 alloy forgings after vacuum brazing

A yield strength and alloy technology, which is applied in the field of heat treatment of high-temperature alloys, can solve problems such as the decrease of alloy high-temperature yield strength and difficulty in meeting technical requirements, and achieve the effects of increasing cooling rate, shortening aging treatment time, and weakening the growth tendency

Active Publication Date: 2022-04-29
UNIV OF SCI & TECH BEIJING
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  • Claims
  • Application Information

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Problems solved by technology

[0007] In view of the above analysis, the present invention aims to provide a process for improving the high-temperature yield strength of GH4738 alloy forgings after vacuum brazing, so as to solve the problem that the existing vacuum brazing and aging treatment reduce the high-temperature yield strength of the alloy, and it is difficult to meet the technical requirements.

Method used

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  • High temperature yield strength improvement process of gh4738 alloy forgings after vacuum brazing
  • High temperature yield strength improvement process of gh4738 alloy forgings after vacuum brazing
  • High temperature yield strength improvement process of gh4738 alloy forgings after vacuum brazing

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Embodiment 1

[0032] Dimensions processed by multi-fire die forging are Take the GH4738 alloy forging as an example.

[0033] First place the GH4738 alloy forging in a vacuum heat treatment furnace for vacuum brazing: vacuumize until the pressure in the furnace is not greater than 10 -3 Pa, then raise the temperature from room temperature to 1040°C at a rate of 10°C / min, keep it warm for 20min, refill with 1.6bar argon, and immediately start the stirring fan in the equipment to cool quickly, and then take it out of the furnace and air cool it when it is below 60°C.

[0034] After the vacuum brazing treatment, a two-stage aging treatment is carried out: the first-stage treatment temperature is 845°C, the holding time is 4h, and then air-cooled to room temperature; the second-stage treatment temperature is 760°C, the holding time is 4h, and then air-cooled to room temperature. The microstructure of the alloy after heat treatment figure 1As shown, the fine and dispersed secondary γ′ phase m...

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Abstract

The invention discloses a process for improving the high-temperature yield strength of a GH4738 alloy forging after vacuum brazing, and belongs to the technical field of high-temperature alloy heat treatment. Including the following steps: Vacuum brazing treatment: at a pressure not greater than 10 ‑3 In a vacuum environment of Pa, heat up from room temperature to the brazing temperature of 1000-1080°C, keep it warm for 10-30min, and fill it with argon to cool it below 60°C; The time is 4±0.1h, then air-cooled to room temperature; the second stage of treatment temperature is 760±10°C, the holding time is 4±0.1h, and then air-cooled to room temperature. The invention improves the cooling rate of the alloy after vacuum brazing, shortens the aging treatment time, and obtains a finely dispersed gamma' strengthening phase, which has an unexpected effect in improving the high-temperature yield strength of the GH4738 alloy forging after brazing treatment. Among them, the yield strength at 540°C can reach 850MPa, which is 13.6% higher than that before process optimization; the yield strength at 760°C can reach 820MPa, which is 18.0% higher than that before process optimization.

Description

technical field [0001] The invention relates to a process for improving the high-temperature yield strength of a GH4738 alloy forging after vacuum brazing, and belongs to the technical field of high-temperature alloy heat treatment. Background technique [0002] Superalloys usually refer to a class of alloys formed by using Group VIII elements (iron, cobalt, nickel, etc.) as the base material and adding a large amount of strengthening elements. Superalloys can be used for a long time above 650 ° C, have good oxidation resistance, corrosion resistance, excellent tensile, durability, fatigue properties and long-term tissue stability and other comprehensive properties, and are currently widely used in hot-end components such as aero engines and gas turbines . Among many superalloy systems, nickel-based wrought superalloys are widely used in various high-performance engine hot-end rotating parts due to their good high-temperature forging properties and comprehensive properties....

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): C22F1/10C22F1/02C22C19/05
CPCC22F1/10C22F1/02C22C19/056
Inventor 郑磊王丹刘红亮闵慧娜赵鑫魏鑫董建邰清安孟晔金莹
Owner UNIV OF SCI & TECH BEIJING
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