WO2023184837A1 - Method for preventing single crystal hollow guide vane from being recrystallized - Google Patents

Method for preventing single crystal hollow guide vane from being recrystallized Download PDF

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WO2023184837A1
WO2023184837A1 PCT/CN2022/114643 CN2022114643W WO2023184837A1 WO 2023184837 A1 WO2023184837 A1 WO 2023184837A1 CN 2022114643 W CN2022114643 W CN 2022114643W WO 2023184837 A1 WO2023184837 A1 WO 2023184837A1
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hollow guide
single crystal
wax
mold
guide vane
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PCT/CN2022/114643
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French (fr)
Chinese (zh)
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贾玉亮
杜应流
蔡俊成
张吉星
汪兴芳
张丽
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安徽应流航源动力科技有限公司
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Priority to DE112022002432.1T priority Critical patent/DE112022002432T5/en
Publication of WO2023184837A1 publication Critical patent/WO2023184837A1/en

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22CFOUNDRY MOULDING
    • B22C7/00Patterns; Manufacture thereof so far as not provided for in other classes
    • B22C7/02Lost patterns
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22CFOUNDRY MOULDING
    • B22C9/00Moulds or cores; Moulding processes
    • B22C9/02Sand moulds or like moulds for shaped castings
    • B22C9/04Use of lost patterns
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22CFOUNDRY MOULDING
    • B22C9/00Moulds or cores; Moulding processes
    • B22C9/10Cores; Manufacture or installation of cores
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22CFOUNDRY MOULDING
    • B22C9/00Moulds or cores; Moulding processes
    • B22C9/10Cores; Manufacture or installation of cores
    • B22C9/108Installation of cores
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22CFOUNDRY MOULDING
    • B22C9/00Moulds or cores; Moulding processes
    • B22C9/22Moulds for peculiarly-shaped castings
    • B22C9/24Moulds for peculiarly-shaped castings for hollow articles
    • CCHEMISTRY; METALLURGY
    • C30CRYSTAL GROWTH
    • C30BSINGLE-CRYSTAL GROWTH; UNIDIRECTIONAL SOLIDIFICATION OF EUTECTIC MATERIAL OR UNIDIRECTIONAL DEMIXING OF EUTECTOID MATERIAL; REFINING BY ZONE-MELTING OF MATERIAL; PRODUCTION OF A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; SINGLE CRYSTALS OR HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; AFTER-TREATMENT OF SINGLE CRYSTALS OR A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; APPARATUS THEREFOR
    • C30B11/00Single-crystal growth by normal freezing or freezing under temperature gradient, e.g. Bridgman-Stockbarger method
    • C30B11/002Crucibles or containers for supporting the melt
    • CCHEMISTRY; METALLURGY
    • C30CRYSTAL GROWTH
    • C30BSINGLE-CRYSTAL GROWTH; UNIDIRECTIONAL SOLIDIFICATION OF EUTECTIC MATERIAL OR UNIDIRECTIONAL DEMIXING OF EUTECTOID MATERIAL; REFINING BY ZONE-MELTING OF MATERIAL; PRODUCTION OF A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; SINGLE CRYSTALS OR HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; AFTER-TREATMENT OF SINGLE CRYSTALS OR A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; APPARATUS THEREFOR
    • C30B29/00Single crystals or homogeneous polycrystalline material with defined structure characterised by the material or by their shape
    • C30B29/10Inorganic compounds or compositions
    • C30B29/52Alloys
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/20Hydro energy

Definitions

  • the present invention relates to the technical field of investment casting, and in particular to a method for preventing recrystallization of single crystal hollow guide vanes.
  • Recrystallization control technology is one of the key technologies in the development of single-crystal blades.
  • the control of recrystallization of hollow blades at home and abroad is mostly focused on electrolytic corrosion and carburization.
  • U.S. Patent US2014/022990 preliminarily discusses the impact of casting fillets on recrystallization, and analyzes the causes of recrystallization at the casting corners. When the casting fillets are smaller, the alloy solidifies to produce more concentrated residues.
  • Recrystallization of single-crystal blades is caused by casting stress-driven effects and is formed during subsequent high-temperature heat treatment.
  • the exit of the inner cavity of the traditional single crystal hollow guide vane has a sharp angle structure, as shown in Figures 1 and 2.
  • the exit of the inner cavity of the single crystal hollow guide vane wax model 1, the surface of the wax model at the exit of the inner cavity is the end surface 1a of the wax model, and the inner cavity
  • the inner wall surface 1b is coplanar with the surface of the core 2, and the wax pattern end surface 1a is perpendicular to the adjacent inner cavity inner wall surface 1b; see Figure 2, the sharp corner structure of this part forms stress concentration during casting.
  • Recrystallization areas 5 will be formed at the sharp corners, causing defects in the hollow guide blades and affecting performance.
  • the length t1 of the positioning section of the core 2 extending into the mold shell 3 is 10mm to 20mm, resulting in an increase in the thickness of the mold shell. , affecting the solidification heat dissipation efficiency and stability.
  • the main purpose of the present invention is to provide a method for preventing the recrystallization of single-crystal hollow guide blades.
  • the corner structure effectively prevents recrystallization at the sharp corner structure of single crystal hollow guide blades, avoids stress concentration after solidification, ensures the quality of single crystal hollow guide blade castings, improves the qualification rate of single crystal hollow guide blades, and can effectively Solve problems in background technology.
  • the technical solution adopted by the present invention is: a method for preventing recrystallization of single crystal hollow guide blades, which includes the following steps:
  • step 3 Put the optimized core into the modified pressing mold in step 1), and inject wax through a wax injection machine to obtain a hollow guide blade wax pattern;
  • step 3 Mold the hollow guide vane wax shell in step 3), and after drying and hardening, obtain the hollow guide vane shell;
  • the structure at the exit of the wax pattern cavity optimized in step 1 is the end surface of the wax pattern.
  • the inner wall surface of the wax pattern interior cavity is coplanar with the surface of the core.
  • the end surface of the wax pattern is perpendicular to the inner wall surface of the adjacent wax pattern interior cavity.
  • the arc radius R of the arc surface in step 1 is 0.4-1.2mm.
  • step 2 the height of the shoulder is the same as the height of the end wall of the wax pattern, both are t3.
  • step 2 the length t2 of the shoulder is 2-10mm, making the length of t2 smaller than the length of t1, reducing the length of the positioning section of the core into the mold shell, reducing the thickness of the mold shell, and improving the solidification and heat dissipation efficiency and stability of the molten metal. .
  • the hollow guide blade mold shell includes a wax mold, a core and a mold shell.
  • the end face of the core close to the mold shell has an inward concave arc surface structure, which matches the corresponding mold shell's outward protruding arc surface structure.
  • the beneficial effects produced by the present invention are: the present invention optimizes the structure of the exit of the inner cavity of the wax model and the matching structure of the core and the exit of the inner cavity of the wax model, and designs it into a rounded structure, which is effective It effectively prevents recrystallization at the sharp corner structure of the single crystal hollow guide blade, avoids stress concentration after solidification, ensures the quality of the single crystal hollow guide blade casting, and improves the qualification rate of the single crystal hollow guide blade.
  • Figure 1 is a schematic structural diagram of the exit of the inner cavity of a traditional single crystal hollow guide blade
  • Figure 2 is a schematic diagram of recrystallization formed at the exit of the inner cavity of a traditional single crystal hollow guide blade
  • Figure 3 is a schematic diagram of the structural optimization of the inner cavity outlet of the single crystal hollow guide blade of the present invention.
  • a method to prevent recrystallization of single crystal hollow guide vanes includes the following steps:
  • the core 2 To optimize the core structure, bend the core 2 along the arc surface 1c of the hollow guide blade to form a convex shoulder 2a.
  • the convex shoulder 2a fits the arc surface 1c, and the convex shoulder 2a surrounds the longitudinal section of the core 2.
  • the height of the shoulder 2a is the same as the height of the side wall of the wax mold end face 1a, both are t3.
  • the length t2 of the shoulder 2a is 2-10mm.
  • the length of t2 is less than the length of t1, which reduces the insertion of the core 2 into the mold shell.
  • the length of the positioning section 3 reduces the thickness of the mold shell 3 and improves the solidification and heat dissipation efficiency and stability of the molten metal.
  • step 3 Put the optimized core into the modified pressing mold in step 1), and inject wax through a wax injection machine to obtain a hollow guide blade wax pattern;
  • the hollow guide blade shell includes a wax mold 1, a core 2 and a shell 3.
  • the core 2 is close to
  • the end surface of the mold shell 3 has an inward concave arc surface structure, and the corresponding mold shell 3 has an outward protruding arc surface structure, which can reduce the thickness of the mold shell to a certain extent and improve the heat dissipation effect.
  • the working principle of the invention is: by modifying and matching the core and the wax mold, the core convex shoulder at the outlet of the inner cavity of the single crystal hollow guide blade is formed, and the sharp corner structure at the outlet of the inner cavity of the single crystal hollow guide blade is optimized into a round shape.
  • the angular structure reduces the casting stress concentration during solidification, thereby preventing the occurrence of recrystallization and avoiding the casting stress concentration during solidification.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Inorganic Chemistry (AREA)
  • Crystals, And After-Treatments Of Crystals (AREA)
  • Molds, Cores, And Manufacturing Methods Thereof (AREA)

Abstract

A method for preventing a single crystal hollow guide vane from being recrystallized. The method comprises optimizing a vertical sharp-angle structure at an outlet of an inner cavity of the single crystal hollow guide vane into a round-angle structure to form a cambered surface (1c) and modifying a profiling mold; bending a mold core (2) along the cambered surface of the hollow guide vane to form a shoulder (2a), which is attached to the cambered surface and surrounds a longitudinal section of the mold core to form an annular structure; putting the mold core into the modified profiling mold, and injecting wax by means of a wax injection machine to obtain a hollow guide vane wax mold (1); and obtaining a blank after housing making, dewaxing, pouring, and housing removal. The method effectively prevents the sharp-angle structure of the single crystal hollow guide vane from being recrystallized by means of optimizing the structure at an outlet of an inner cavity of a wax mold and a mold core structure to form the round-angle structure, avoids stress concentration after solidification, ensures the quality of a single crystal hollow guide vane casting, and increases the qualification rate of the single crystal hollow guide vane.

Description

一种防止单晶空心导向叶片再结晶的方法A method to prevent recrystallization of single crystal hollow guide blades 技术领域Technical field
本发明涉及熔模铸造技术领域,特别涉及一种防止单晶空心导向叶片再结晶的方法。The present invention relates to the technical field of investment casting, and in particular to a method for preventing recrystallization of single crystal hollow guide vanes.
背景技术Background technique
高温合金涡轮单晶叶片被誉为工业技术皇冠上的明珠,再结晶控制技术是单晶叶片研制的关键技术之一,目前国内外关于空心叶片再结晶的控制多集中于通过电解腐蚀、渗碳、溅射等物理化学方法,美国专利US2014/022990初步论述了铸造圆角对再结晶的影响,分析了铸造表明转角处再结晶的成因,当铸造圆角较小时,合金凝固产生较集中的残余应力,在热处理时会诱发再结晶;当铸造圆角加大时,合金凝固时的应力比较分散,残余应力较小,在热处理时不易诱发再结晶,只阐述了圆角结构可以降低再结晶的理论阐述,但没有提出具体实施方案,以及如何去在铸件上进行实施。High-temperature alloy turbine single-crystal blades are known as the crown jewel of industrial technology. Recrystallization control technology is one of the key technologies in the development of single-crystal blades. At present, the control of recrystallization of hollow blades at home and abroad is mostly focused on electrolytic corrosion and carburization. , sputtering and other physical and chemical methods, U.S. Patent US2014/022990 preliminarily discusses the impact of casting fillets on recrystallization, and analyzes the causes of recrystallization at the casting corners. When the casting fillets are smaller, the alloy solidifies to produce more concentrated residues. Stress will induce recrystallization during heat treatment; when the casting fillet is enlarged, the stress during solidification of the alloy is relatively dispersed and the residual stress is small, making it difficult to induce recrystallization during heat treatment. It is only explained that the rounded corner structure can reduce the risk of recrystallization. The theory is elaborated, but no specific implementation plan is proposed, and how to implement it on castings.
单晶叶片再结晶是由于铸造应力驱动作用下,在随后的高温热处理过程中形成的。传统的单晶空心导向叶片内腔出口为尖角结构,如图1、2,单晶空心导向叶片蜡模1内腔的出口处,内腔出口的蜡模表面为蜡模端面1a,内腔内壁表面1b与型芯2的表面共面,蜡模端面1a与邻接的内腔内壁表面1b垂直;参见图2,该部位的尖角结构在铸造时形成应力集中,热处理之后,在单晶铸件4上尖角部位会形成再结晶区域5,造成空心导向叶片缺陷,影响使用性能,此外,型芯2伸入型壳3内的定位段的长度t1为10mm~20mm,致使型壳厚度增大,影响凝固散热效率及稳定性。Recrystallization of single-crystal blades is caused by casting stress-driven effects and is formed during subsequent high-temperature heat treatment. The exit of the inner cavity of the traditional single crystal hollow guide vane has a sharp angle structure, as shown in Figures 1 and 2. The exit of the inner cavity of the single crystal hollow guide vane wax model 1, the surface of the wax model at the exit of the inner cavity is the end surface 1a of the wax model, and the inner cavity The inner wall surface 1b is coplanar with the surface of the core 2, and the wax pattern end surface 1a is perpendicular to the adjacent inner cavity inner wall surface 1b; see Figure 2, the sharp corner structure of this part forms stress concentration during casting. After heat treatment, in the single crystal casting 4 Recrystallization areas 5 will be formed at the sharp corners, causing defects in the hollow guide blades and affecting performance. In addition, the length t1 of the positioning section of the core 2 extending into the mold shell 3 is 10mm to 20mm, resulting in an increase in the thickness of the mold shell. , affecting the solidification heat dissipation efficiency and stability.
发明内容Contents of the invention
本发明的主要目的在于提供一种防止单晶空心导向叶片再结晶的方法,通过对蜡模内腔出口处的结构以及型芯与蜡模内腔出口处相配合的结构进行优化,设计成圆角结构,有效地防止了单晶空心导向叶片尖角结构处产生再结晶,避免凝固后应力集中,保证了单晶空心导向叶片铸件的质量,提高了单晶空心导向叶片的合格率,可以有效解决背景技术中的问题。The main purpose of the present invention is to provide a method for preventing the recrystallization of single-crystal hollow guide blades. By optimizing the structure of the exit of the inner cavity of the wax mold and the matching structure of the core and the exit of the inner cavity of the wax mold, it is designed into a round shape. The corner structure effectively prevents recrystallization at the sharp corner structure of single crystal hollow guide blades, avoids stress concentration after solidification, ensures the quality of single crystal hollow guide blade castings, improves the qualification rate of single crystal hollow guide blades, and can effectively Solve problems in background technology.
为实现上述目的,本发明采取的技术方案为:一种防止单晶空心导向叶片再结晶的方法,包括如下步骤:In order to achieve the above object, the technical solution adopted by the present invention is: a method for preventing recrystallization of single crystal hollow guide blades, which includes the following steps:
1)对单晶空心导向叶片蜡模结构部位优化,该部位位于单晶空心导向叶片蜡模内腔的出口处,在该部位中将单晶空心导向叶片内腔出口处的垂直尖角结构优化成圆角结构,形成圆弧面,并根据优化后的叶片蜡模内腔出口处的结构修改压型模具;1) Optimize the structure of the wax pattern of the single crystal hollow guide vane, which is located at the exit of the inner cavity of the single crystal hollow guide vane wax pattern, and optimize the vertical sharp corner structure at the exit of the inner cavity of the single crystal hollow guide vane. A rounded corner structure is formed to form an arc surface, and the pressing mold is modified according to the structure at the exit of the inner cavity of the optimized blade wax model;
2)对型芯结构优化,在型芯沿着空心导向叶片的圆弧面弯曲,形成凸肩,凸肩与圆弧面贴合,凸肩环绕型芯的纵向截面形成环状结构;2) Optimize the core structure, bend the core along the arc surface of the hollow guide blade to form a convex shoulder, the convex shoulder fits the arc surface, and the convex shoulder surrounds the longitudinal section of the core to form an annular structure;
3)把优化后的型芯放入到步骤1)中修改后的压型模具中,通过注蜡机注蜡得到空心导向叶片蜡模;3) Put the optimized core into the modified pressing mold in step 1), and inject wax through a wax injection machine to obtain a hollow guide blade wax pattern;
4)对步骤3)中的空心导向叶片蜡模制壳,干燥硬化后,得到空心导向叶片型壳;4) Mold the hollow guide vane wax shell in step 3), and after drying and hardening, obtain the hollow guide vane shell;
5)对空心导向叶片型壳脱蜡、浇注、脱壳后,得到单晶空心导向叶片毛坯件,并对毛坯件加工处理得到单晶空心导向叶片铸件。5) After dewaxing, pouring and shelling the hollow guide blade shell, a single crystal hollow guide blade blank is obtained, and the blank is processed to obtain a single crystal hollow guide blade casting.
步骤1所优化的蜡模内腔出口处的结构为蜡模端面,蜡模内腔内壁表面与型芯表面共面,蜡模端面与邻接的蜡模内腔内壁表面垂直。The structure at the exit of the wax pattern cavity optimized in step 1 is the end surface of the wax pattern. The inner wall surface of the wax pattern interior cavity is coplanar with the surface of the core. The end surface of the wax pattern is perpendicular to the inner wall surface of the adjacent wax pattern interior cavity.
步骤1中圆弧面的圆弧半径R为0.4-1.2mm。The arc radius R of the arc surface in step 1 is 0.4-1.2mm.
步骤2中凸肩的高度与蜡模端面侧壁的高度相同均为t3。In step 2, the height of the shoulder is the same as the height of the end wall of the wax pattern, both are t3.
步骤2中凸肩的长度t2为2-10mm,使得t2的长度小于t1的长度,减少型芯入型壳内的定位段长度,降低了型壳的厚度,提高金属液凝固散热效率以及稳定性。In step 2, the length t2 of the shoulder is 2-10mm, making the length of t2 smaller than the length of t1, reducing the length of the positioning section of the core into the mold shell, reducing the thickness of the mold shell, and improving the solidification and heat dissipation efficiency and stability of the molten metal. .
步骤4中空心导向叶片型壳包括蜡模、型芯和型壳,型芯靠近型壳的端面向内凹有弧面结构,配合对应的型壳向外凸出弧面结构。In step 4, the hollow guide blade mold shell includes a wax mold, a core and a mold shell. The end face of the core close to the mold shell has an inward concave arc surface structure, which matches the corresponding mold shell's outward protruding arc surface structure.
与传统技术相比,本发明产生的有益效果是:本发明通过对蜡模内腔出口处的结构以及型芯与蜡模内腔出口处相配合的结构进行优化,设计成圆角结构,有效地防止了单晶空心导向叶片尖角结构处产生再结晶,避免凝固后应力集中,保证了单晶空心导向叶片铸件的质量,提高了单晶空心导向叶片的合格率。Compared with traditional technology, the beneficial effects produced by the present invention are: the present invention optimizes the structure of the exit of the inner cavity of the wax model and the matching structure of the core and the exit of the inner cavity of the wax model, and designs it into a rounded structure, which is effective It effectively prevents recrystallization at the sharp corner structure of the single crystal hollow guide blade, avoids stress concentration after solidification, ensures the quality of the single crystal hollow guide blade casting, and improves the qualification rate of the single crystal hollow guide blade.
附图说明Description of drawings
图1为传统单晶空心导向叶片内腔出口处的结构示意图;Figure 1 is a schematic structural diagram of the exit of the inner cavity of a traditional single crystal hollow guide blade;
图2为传统单晶空心导向叶片内腔出口处形成再结晶的示意图;Figure 2 is a schematic diagram of recrystallization formed at the exit of the inner cavity of a traditional single crystal hollow guide blade;
图3为本发明的单晶空心导向叶片内腔出口处结构优化的示意图。Figure 3 is a schematic diagram of the structural optimization of the inner cavity outlet of the single crystal hollow guide blade of the present invention.
图中:1、蜡模;1a、蜡模端面;1b、蜡模内腔内壁表面;1c、圆弧面;2、型芯;2a、凸肩;3、型壳;4、单晶铸件;5、再结晶区域。In the picture: 1. Wax mold; 1a, end face of the wax mold; 1b, inner wall surface of the wax mold cavity; 1c, arc surface; 2. core; 2a, shoulder; 3. mold shell; 4. single crystal casting; 5. Recrystallization area.
具体实施方式Detailed ways
为使本发明实现的技术手段、创作特征、达成目的与功效易于明白了解,下面结合具体实施方式,进一步阐述本发明。In order to make the technical means, creative features, objectives and effects achieved by the present invention easy to understand, the present invention will be further elaborated below in conjunction with specific implementation modes.
如图3所示,一种防止单晶空心导向叶片再结晶的方法,包括如下步骤:As shown in Figure 3, a method to prevent recrystallization of single crystal hollow guide vanes includes the following steps:
1)对单晶空心导向叶片蜡模结构部位优化,该部位位于单晶空心导向叶片蜡模1内腔的出口处,所优化的蜡模1内腔出口处的结构为蜡模端面1a,蜡模内腔内壁表面1b与型芯表面共面,蜡模端面1a与邻接的蜡模内腔内壁表面1b垂直,在该部位中将单晶空心导向叶片内腔出口处的垂直尖角结构,即1a与1b 的垂直交接处,优化成圆角结构,在蜡模表面形成圆弧面1c,圆弧面1c的圆弧半径R为0.4-1.2mm,并根据优化后的叶片蜡模内腔出口处的结构修改压型模具;1) Optimize the structural part of the single crystal hollow guide vane wax pattern. This part is located at the exit of the inner cavity of the single crystal hollow guide vane wax pattern 1. The optimized structure at the exit of the inner chamber of the wax pattern 1 is the wax pattern end face 1a. The inner wall surface 1b of the mold cavity is coplanar with the surface of the core, and the end surface 1a of the wax mold is perpendicular to the inner wall surface 1b of the adjacent wax mold cavity. In this position, the single crystal hollow guide blade has a vertical sharp angle structure at the exit of the inner cavity, that is, The vertical intersection of 1a and 1b is optimized into a rounded structure, forming an arc surface 1c on the surface of the wax model. The arc radius R of the arc surface 1c is 0.4-1.2mm, and according to the optimized outlet of the inner cavity of the blade wax model The structural modification of the pressing mold;
2)对型芯结构优化,在型芯2沿着空心导向叶片的圆弧面1c弯曲,形成凸肩2a,凸肩2a与圆弧面1c贴合,凸肩2a环绕型芯2的纵向截面形成环状结构,凸肩2a的高度与蜡模端面1a侧壁的高度相同均为t3,凸肩2a的长度t2为2-10mm,t2的长度小于t1的长度,减少型芯2入型壳3内的定位段长度,降低了型壳3的厚度,提高金属液凝固散热效率以及稳定性。2) To optimize the core structure, bend the core 2 along the arc surface 1c of the hollow guide blade to form a convex shoulder 2a. The convex shoulder 2a fits the arc surface 1c, and the convex shoulder 2a surrounds the longitudinal section of the core 2. Forming a ring structure, the height of the shoulder 2a is the same as the height of the side wall of the wax mold end face 1a, both are t3. The length t2 of the shoulder 2a is 2-10mm. The length of t2 is less than the length of t1, which reduces the insertion of the core 2 into the mold shell. The length of the positioning section 3 reduces the thickness of the mold shell 3 and improves the solidification and heat dissipation efficiency and stability of the molten metal.
3)把优化后的型芯放入到步骤1)中修改后的压型模具中,通过注蜡机注蜡得到空心导向叶片蜡模;3) Put the optimized core into the modified pressing mold in step 1), and inject wax through a wax injection machine to obtain a hollow guide blade wax pattern;
4)对步骤3)中的空心导向叶片蜡模制壳,干燥硬化后,得到空心导向叶片型壳,该空心导向叶片型壳包括蜡模1、型芯2和型壳3,型芯2靠近型壳3的端面向内凹有弧面结构,配合对应的型壳3向外凸出弧面结构,能够一定程度的降低型壳的厚度,提高散热效果。4) Mold the hollow guide blade wax shell in step 3). After drying and hardening, a hollow guide blade shell is obtained. The hollow guide blade shell includes a wax mold 1, a core 2 and a shell 3. The core 2 is close to The end surface of the mold shell 3 has an inward concave arc surface structure, and the corresponding mold shell 3 has an outward protruding arc surface structure, which can reduce the thickness of the mold shell to a certain extent and improve the heat dissipation effect.
5)对空心导向叶片型壳脱蜡、浇注、脱壳后,得到单晶空心导向叶片毛坯件,并对毛坯件加工处理得到单晶空心导向叶片铸件。5) After dewaxing, pouring and shelling the hollow guide blade shell, a single crystal hollow guide blade blank is obtained, and the blank is processed to obtain a single crystal hollow guide blade casting.
本发明的工作原理是:通过型芯与蜡模修改匹配,使单晶空心导向叶片内腔出口处的型芯凸肩成型,将单晶空心导向叶片内腔出口处的尖角结构优化成圆角结构,减小了凝固过程中的铸造应力集中,从而防止了再结晶的发生,避免凝固时铸造应力集中。The working principle of the invention is: by modifying and matching the core and the wax mold, the core convex shoulder at the outlet of the inner cavity of the single crystal hollow guide blade is formed, and the sharp corner structure at the outlet of the inner cavity of the single crystal hollow guide blade is optimized into a round shape. The angular structure reduces the casting stress concentration during solidification, thereby preventing the occurrence of recrystallization and avoiding the casting stress concentration during solidification.
以上只通过说明的方式描述了本发明的某些示范性实施例,毋庸置疑,对于本领域的普通技术人员,在不偏离本发明的精神和范围的情况下,可以用各种不同的方式对所描述的实施例进行修正。因此,上述附图和描述在本质上是说明性的,不应理解为对本发明权利要求保护范围的限制。Certain exemplary embodiments of the present invention have been described above only by way of illustration. It goes without saying that those skilled in the art can implement various embodiments in various ways without departing from the spirit and scope of the present invention. The described embodiments are modified. Therefore, the above drawings and descriptions are illustrative in nature and should not be construed as limiting the scope of the claims of the present invention.

Claims (6)

  1. 一种防止单晶空心导向叶片再结晶的方法,其特征在于:包括如下步骤:A method for preventing recrystallization of single crystal hollow guide blades, which is characterized by: including the following steps:
    1)对单晶空心导向叶片蜡模结构部位优化,该部位位于单晶空心导向叶片蜡模内腔的出口处,在该部位中将单晶空心导向叶片内腔出口处的垂直尖角结构优化成圆角结构,形成圆弧面,并根据优化后的叶片蜡模内腔出口处的结构修改压型模具;1) Optimize the structure of the wax pattern of the single crystal hollow guide vane, which is located at the exit of the inner cavity of the single crystal hollow guide vane wax pattern, and optimize the vertical sharp corner structure at the exit of the inner cavity of the single crystal hollow guide vane. A rounded corner structure is formed to form an arc surface, and the pressing mold is modified according to the structure at the exit of the inner cavity of the optimized blade wax model;
    2)对型芯结构优化,在型芯沿着空心导向叶片的圆弧面弯曲,形成凸肩,凸肩与圆弧面贴合,凸肩环绕型芯的纵向截面形成环状结构;2) Optimize the core structure, bend the core along the arc surface of the hollow guide blade to form a convex shoulder, the convex shoulder fits the arc surface, and the convex shoulder surrounds the longitudinal section of the core to form an annular structure;
    3)把优化后的型芯放入到步骤1)中修改后的压型模具中,通过注蜡机注蜡得到空心导向叶片蜡模;3) Put the optimized core into the modified pressing mold in step 1), and inject wax through a wax injection machine to obtain a hollow guide blade wax pattern;
    4)对步骤3)中的空心导向叶片蜡模制壳,干燥硬化后,得到空心导向叶片型壳;4) Mold the hollow guide vane wax shell in step 3), and after drying and hardening, obtain the hollow guide vane shell;
    5)对空心导向叶片型壳脱蜡、浇注、脱壳后,得到单晶空心导向叶片毛坯件,并对毛坯件加工处理得到单晶空心导向叶片铸件。5) After dewaxing, pouring and shelling the hollow guide blade shell, a single crystal hollow guide blade blank is obtained, and the blank is processed to obtain a single crystal hollow guide blade casting.
  2. 根据权利要求1所述的一种防止单晶空心导向叶片再结晶的方法,其特征在于:步骤1所优化的蜡模内腔出口处的结构为蜡模端面,蜡模内腔内壁表面与型芯表面共面,蜡模端面与邻接的蜡模内腔内壁表面垂直。A method for preventing recrystallization of single crystal hollow guide blades according to claim 1, characterized in that: the structure at the exit of the wax mold cavity optimized in step 1 is the end face of the wax mold, and the inner wall surface of the wax mold cavity is in line with the shape of the wax mold. The core surfaces are coplanar, and the end surface of the wax pattern is perpendicular to the inner wall surface of the adjacent wax pattern cavity.
  3. 根据权利要求1所述的一种防止单晶空心导向叶片再结晶的方法,其特征在于:步骤1中圆弧面的圆弧半径R为0.4-1.2mm。A method for preventing recrystallization of single crystal hollow guide blades according to claim 1, characterized in that: in step 1, the arc radius R of the arc surface is 0.4-1.2 mm.
  4. 根据权利要求1所述的一种防止单晶空心导向叶片再结晶的方法,其特征在于:步骤2中凸肩的高度与蜡模端面侧壁的高度相同均为t3。A method for preventing recrystallization of single crystal hollow guide blades according to claim 1, characterized in that in step 2, the height of the shoulder is the same as the height of the end face side wall of the wax mold, both of which are t3.
  5. 根据权利要求1所述的一种防止单晶空心导向叶片再结晶的方法,其特征在于:步骤2中凸肩的长度t2为2-10mm。A method for preventing recrystallization of single crystal hollow guide blades according to claim 1, characterized in that in step 2, the length t2 of the shoulder is 2-10 mm.
  6. 根据权利要求1所述的一种防止单晶空心导向叶片再结晶的方法,其特 征在于:步骤4中空心导向叶片型壳包括蜡模、型芯和型壳,型芯靠近型壳的端面向内凹有弧面结构,配合对应的型壳向外凸出弧面结构。A method for preventing recrystallization of single crystal hollow guide blades according to claim 1, characterized in that: in step 4, the hollow guide blade mold shell includes a wax mold, a core and a mold shell, and the end of the core close to the mold shell faces There is a concave arc structure on the inside, and the corresponding shell has a convex arc structure on the outside.
PCT/CN2022/114643 2022-03-28 2022-08-25 Method for preventing single crystal hollow guide vane from being recrystallized WO2023184837A1 (en)

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Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB8332567D0 (en) * 1983-12-07 1984-01-11 Rolls Royce Investment casting
DE3873305D1 (en) * 1988-01-13 1992-09-03 Rolls Royce Plc DEVICE FOR SUPPORTING A CORE IN A MOLD.
CN112705671A (en) * 2020-12-10 2021-04-27 中国科学院金属研究所 Wax module structure of cover plate block casting cantilever structure single crystal blade
CN113070454A (en) * 2021-03-16 2021-07-06 贵阳航发精密铸造有限公司 Casting device and method for non-preferred orientation single crystal guide hollow blade
CN113458343A (en) * 2021-07-05 2021-10-01 中国航发北京航空材料研究院 Method for preventing inner cavity of single crystal hollow blade from recrystallizing
CN113492197A (en) * 2021-07-05 2021-10-12 中国航发北京航空材料研究院 Wax mold method for avoiding recrystallization and micro-porosity of single-crystal hollow blade
CN114850397A (en) * 2022-03-28 2022-08-05 安徽应流航源动力科技有限公司 Method for preventing single crystal hollow guide blade from recrystallizing

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7047786B2 (en) * 1998-03-17 2006-05-23 Stresswave, Inc. Method and apparatus for improving the fatigue life of components and structures
JP2007277697A (en) * 2006-03-16 2007-10-25 Jfe Steel Kk High tensile strength thick steel plate having excellent fatigue crack propagation resistance and brittle crack propagation arrest property and its production method
US9320077B2 (en) 2012-07-17 2016-04-19 Innovative Sonic Corporation Method and apparatus for reducing signaling overhead in a wireless communication network
CN104550731B (en) * 2014-12-06 2017-08-11 沈阳工业大学 The preparation technology that the anti-surface stray crystal of single crystal hollow turbo blade is formed with recrystallization

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB8332567D0 (en) * 1983-12-07 1984-01-11 Rolls Royce Investment casting
DE3873305D1 (en) * 1988-01-13 1992-09-03 Rolls Royce Plc DEVICE FOR SUPPORTING A CORE IN A MOLD.
CN112705671A (en) * 2020-12-10 2021-04-27 中国科学院金属研究所 Wax module structure of cover plate block casting cantilever structure single crystal blade
CN113070454A (en) * 2021-03-16 2021-07-06 贵阳航发精密铸造有限公司 Casting device and method for non-preferred orientation single crystal guide hollow blade
CN113458343A (en) * 2021-07-05 2021-10-01 中国航发北京航空材料研究院 Method for preventing inner cavity of single crystal hollow blade from recrystallizing
CN113492197A (en) * 2021-07-05 2021-10-12 中国航发北京航空材料研究院 Wax mold method for avoiding recrystallization and micro-porosity of single-crystal hollow blade
CN114850397A (en) * 2022-03-28 2022-08-05 安徽应流航源动力科技有限公司 Method for preventing single crystal hollow guide blade from recrystallizing

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