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Method for preparing single-crystal high-temperature alloy by combining solid-solution-state columnar crystals with crystal selection

A high-temperature alloy and columnar crystal technology, which is applied in the field of preparation of single-crystal superalloys, can solve the problems of large crystal orientation deviation and low performance of single-crystal turbine blades, and achieve the effect of reducing difficulty and cost

Active Publication Date: 2021-06-18
AVIC BEIJING INST OF AERONAUTICAL MATERIALS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] The purpose of the present invention is to provide a method for preparing single crystal superalloys by using solid solution columnar crystals combined with crystal selection to solve the large crystal orientation deviation in the preparation of single crystal superalloys by the crystal selection method in the prior art, which leads to single crystal turbines. Technical issues with lower blade performance

Method used

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  • Method for preparing single-crystal high-temperature alloy by combining solid-solution-state columnar crystals with crystal selection
  • Method for preparing single-crystal high-temperature alloy by combining solid-solution-state columnar crystals with crystal selection
  • Method for preparing single-crystal high-temperature alloy by combining solid-solution-state columnar crystals with crystal selection

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Experimental program
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Effect test

Embodiment 1

[0036] Preparation of Ni-14Mo-7AL single crystal high temperature alloy bar, its specific steps are:

[0037] The first step is to prepare a part wax mold and a spirally crystal wax mold; after melting the wax at a temperature of 75 ° C, inject the parts mold, and press molding at a pressure of 0.5 MPa, and produce a part wax mold; The spirally crystallizer mold is injected into the spirally selected crystallizer mold at a temperature of 75 ° C, and is pressed into 0.5 MPa pressure, and the spiral-selected crystal wax mold is prepared, and the spiral-free wax mold comprises a spiral section and a lactone section. Two parts;

[0038] In the second step, the part wax mold is welded at one end of the helical section of the spiral selection wax mold; the welded parts wax mold and the spiral crystallizer wax mold are pulpted, and the pulp is subjected to the shining. The surface of the surface layer used is 65 to 100 mesh mixed sand, repeated turning wax mold, so that the sand is evenl...

Embodiment 2

[0043] Preparation of Ni-13.5Mo-7.6Al-0.05B ​​single crystal high temperature alloy bar, its specific steps are:

[0044] The first step is to prepare a part wax mold and a helical cleavage wax mold; the wax material is melted into the parts mold at a temperature of 100 ° C, and is pressed into the part mold in the pressure of 8 MPa, and the parts wax mold is made; wax material After melting at a temperature of 100 ° C, inward injection into the spirally crystallizer mold, and press molded at a pressure of 8 MPa, prepared a spirally crystallizer wax mold, and the spiral selection of the wax mold including the spiral segment and the lactone section. ;

[0045] In the second step, the welded parts wax mold and the helix-free wax mold are pulpted. After the slurry, the slurry is shaked, the surface layer sand is 65 ~ 100 mesh, and the wax is repeatedly rotated. The mold is evenly distributed on the surface of the wax mold; the surface is floating, and the drying chamber is placed in ...

Embodiment 3

[0050] Preparation of Ni-12Mo-7.2Al-0.02B single crystal high temperature alloy plate, its specific steps are:

[0051] The first step is to prepare a part wax mold and a helical cleavage wax mold; the wax material is melted into the parts mold at a temperature of 120 ° C, and is pressed into the part mold in the pressure of 5 MPa, and the parts wax mold is made; wax material After melting at 120 ° C, the spirally selected crystal mold is injected, and the mold is pressed under the pressure of 5 MPa, and the spiral-selected crystal wax mold is obtained, and the helix-free wax mold includes a spiral segment and a lactone section. ;

[0052] In the second step, the part wax mold is welded to the spiral section of the spiral selection wax mold; 7 mm ceramic refractory slurry is applied to the outside of the part wax mold and the spirally crystallizer wax mold, and then at 150 ° C temperature Death waxing, after 3 hours at 800 ° C for 3 hours, the ceramic shell is obtained, correspond...

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Abstract

The invention relates to a method for preparing a single-crystal high-temperature alloy by combining solid-solution-state columnar crystals with crystal selection, and belongs to the field of preparation of single-crystal high-temperature alloys. The solid-solution-state columnar crystals are selected and placed in a crystal starting section of a crystal selector, and crystal grains in the solid-solution-state columnar crystals form final single crystals in the single crystal preparation process. According to the method, the single-crystal high-temperature alloy is prepared by combining the solid-solution-state columnar crystals with the crystal selection method, by controlling the selected columnar crystals with <001> direction of crystal grain deviating from the solidification direction within 5 degrees, which is obviously smaller than the deviation range of the crystal orientation of the single-crystal high-temperature alloy controlled by a current crystal selection method, the defect that the crystal orientation deviation is large when the single-crystal high-temperature alloy is prepared by the current crystal selection method is overcome.

Description

Technical field [0001] The present invention relates to the field of preparation of single crystal high temperature alloys, and in particular, a method of preparing a single crystal high temperature alloy using a solid-soluble cylindrical crystal binding crystal. Background technique [0002] The nickel-based single crystal high temperature alloy has excellent high temperature comprehensive performance, and is the preferred material of the aviation engine and the bottom gas turbine blade, and its mechanical properties have significant anisotropy. Controlling its <001> direction in the preparation of single crystal blades, which is consistent with the maximum stress direction, and it can achieve the best service performance. At present, it is primarily prepared a single crystal high temperature alloy in the study of the selected method. The essence of the selected crystal method is that the grains compete in the crystallizer to obtain a single grain, and can only control the...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B22C9/04B22D27/04C30B15/08C30B29/52
CPCB22C9/04B22D27/045C30B15/08C30B29/52
Inventor 杨振宇郑帅郑素杰骆凯伦张剑骆宇时戴圣龙
Owner AVIC BEIJING INST OF AERONAUTICAL MATERIALS