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Method for controlling re-crystallization of directionally solidified nickel base high-temperature alloy by using coating method

A nickel-based superalloy, directional solidification technology, applied in chemical instruments and methods, crystal growth, post-processing details, etc., can solve problems such as inapplicability

Active Publication Date: 2012-10-10
沈阳中科三耐新材料股份有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Although this method can remove the recrystallization layer, it is obviously not suitable for thin-walled single crystal or oriented columnar nickel-based superalloy components

Method used

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  • Method for controlling re-crystallization of directionally solidified nickel base high-temperature alloy by using coating method
  • Method for controlling re-crystallization of directionally solidified nickel base high-temperature alloy by using coating method

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1DZ125

[0016] Example 1 DZ125L directionally solidified alloy 1# coating controls recrystallization.

[0017] The DZ125L directionally solidified nickel-based nickel-based superalloy plate was prepared by the directional solidification equipment, and a 2×12×12mm square was cut from the plate by wire cutting. Polish the surface of 12×12 (direction of oriented columnar crystal growth), and perform sandblasting treatment with a sandblasting device. Sandblasting parameters are as follows: sandblasting pressure is 0.3MPa, sandblasting time is 1min, and the sand particles are SiO 2 Glass ball.

[0018] Next, the coating is applied using arc ion plating equipment. During the coating process, the vacuum degree is 10 -2 Pa, first deposit a layer of Zr on the sample, and then deposit a layer of NiCoCrAlYSiB. The deposition time of Zr layer is 100min, and the time of NiCoCrAlYSiB layer is 2h. After deposition, the coated samples were subjected to stress relief annealing at 800 °C / 10 h. Th...

Embodiment 2

[0019] Example 2 DZ125L directionally solidified alloy 2# coating controls recrystallization.

[0020] The DZ125L directionally solidified nickel-based nickel-based superalloy plate was prepared by the directional solidification equipment, and a 2×12×12mm square was cut from the plate by wire cutting. Polish the surface of 12×12 (direction of oriented columnar crystal growth), and perform sandblasting treatment with a sandblasting device. Sandblasting parameters are as follows: sandblasting pressure is 0.3MPa, sandblasting time is 1min, and the sand particles are SiO 2 Glass ball.

[0021] Next, the coating is applied using arc ion plating equipment. During the coating process, the vacuum degree is 10 -2 Pa, first deposit a layer of graphite on the sample, the deposition time is 1h, and then deposit a layer of NiCoCrAlYSiB, the deposition time is 8h. After deposition, the coated samples were subjected to stress relief annealing at 800°C / 10h. Then these samples were subjec...

Embodiment 3

[0022] Example 3 DZ125L directionally solidified alloy 3# coating controls recrystallization.

[0023] The DZ125L directionally solidified nickel-based nickel-based superalloy plate was prepared by the directional solidification equipment, and a 2×12×12mm square was cut from the plate by wire cutting. Polish the surface of 12×12 (direction of oriented columnar crystal growth), and perform sandblasting treatment with a sandblasting device. Sandblasting parameters are as follows: sandblasting pressure is 0.3MPa, sandblasting time is 1min, and the sand particles are SiO 2 Glass ball.

[0024] Next, the coating is applied using arc ion plating equipment. During the coating process, the vacuum degree is 10 -2 Pa, first deposit a layer of CrC on the sample, the deposition time is 1h, and then deposit a layer of Cr 2 o 3 , the deposition time is 30min, and finally deposit a layer of NiCoCrAlYSiB, the deposition time is 8h. After deposition, the coated samples were subjected to ...

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Abstract

The invention provides a method for controlling re-crystallization of a directionally solidified nickel base high-temperature alloy by using a coating method, which is characterized by comprising the following steps of: coating a coating layer on the surface of a deformed directionally solidified nickel base high-temperature alloy; performing de-stressing annealing on a coating layer sample; and performing standard solution treatment on the directionally solidified nickel base high-temperature alloy, wherein the coating layer is Zr / NiCoCrAlYSiB, CrC / Cr2O3 / NiCoCrAlYSiB, Cr2O3 / NiCoCrAlYSiB, NiCoCrAlYSiB, C / NiCoCrAlYSiB or Zr / ZrO2 / NiCoCrAlYSiB. The method can significantly reduce the re-crystallization of the deformed nickel base high-temperature alloy.

Description

technical field [0001] The invention relates to the recrystallization control technology, and in particular provides a technology for controlling the recrystallization of directionally solidified columnar crystals and single crystal nickel-based superalloys by means of a coating method. Background technique [0002] Gas turbine and aero-engine blades are used at higher temperatures, and the blades are mainly affected by centrifugal force. At high temperatures, the strength of the grain boundary is not as strong as the intragranular strength, and the transverse grain boundary becomes the weak link of the blade. For this reason, people have developed oriented columnar crystals or even single crystal blades to eliminate transverse grain boundaries or all grain boundaries. These blades have better longitudinal mechanical properties and higher temperature capability than conventional polycrystalline blades. [0003] However, during the directional solidification process of the b...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): C22F1/10C21D1/68C30B33/02
Inventor 谢光张健楼琅洪孙超
Owner 沈阳中科三耐新材料股份有限公司