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JP2010229894A - Impeller and method for manufacturing same - Google Patents

Impeller and method for manufacturing same Download PDF

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Publication number
JP2010229894A
JP2010229894A JP2009078486A JP2009078486A JP2010229894A JP 2010229894 A JP2010229894 A JP 2010229894A JP 2009078486 A JP2009078486 A JP 2009078486A JP 2009078486 A JP2009078486 A JP 2009078486A JP 2010229894 A JP2010229894 A JP 2010229894A
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Prior art keywords
blade
side plate
impeller
core plate
nickel
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JP2009078486A
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JP5131237B2 (en
Inventor
Kazumi Fujii
和美 藤井
Takeshi Tsukamoto
武志 塚本
Takeya Ohashi
健也 大橋
Shinji Imaoka
信治 今岡
Kenji Yaegashi
賢司 八重樫
Tetsuya Kuwano
哲也 桑野
Yoshimasa Chiba
由昌 千葉
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Hitachi Plant Technologies Ltd
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Hitachi Plant Technologies Ltd
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/02Selection of particular materials
    • F04D29/023Selection of particular materials especially adapted for elastic fluid pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/28Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
    • F04D29/284Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for compressors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00Manufacture
    • F05D2230/20Manufacture essentially without removing material
    • F05D2230/23Manufacture essentially without removing material by permanently joining parts together
    • F05D2230/232Manufacture essentially without removing material by permanently joining parts together by welding
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/95Preventing corrosion
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00Materials; Properties thereof
    • F05D2300/10Metals, alloys or intermetallic compounds
    • F05D2300/11Iron
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00Materials; Properties thereof
    • F05D2300/10Metals, alloys or intermetallic compounds
    • F05D2300/16Other metals not provided for in groups F05D2300/11 - F05D2300/15
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00Materials; Properties thereof
    • F05D2300/60Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/611Coating

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Coating By Spraying Or Casting (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Butt Welding And Welding Of Specific Article (AREA)

Abstract

<P>PROBLEM TO BE SOLVED: To provide an impeller having a new structure of which surface is coated with high corrosion resistant material, which has a complicated shape and high corrosion resistance, and which is used in a pump and a centrifugal compressor, and a new method for manufacturing the impeller. <P>SOLUTION: Alloy containing iron as the main component is used as base material for a structure member of the impeller and surface of the structure member is coated by nickel base alloy. The impeller is manufactured by providing a prescribed groove on the abutment surface of the structure member abutted on a coated blade, and welding the blade and the structure member after inserting the blade in the groove. <P>COPYRIGHT: (C)2011,JPO&INPIT

Description

本発明は、各種ガスや空気等の気体搬送に用いられる遠心圧縮機、各種液体の搬送装置に用いられる軸流ポンプ等の羽根車およびその製造方法に係り、特に複雑な形状からなる羽根車およびその製造方法に関する。   The present invention relates to an impeller such as a centrifugal compressor used for conveying various gases and air, an axial flow pump used for various liquid conveying devices, and a manufacturing method thereof, and more particularly to an impeller having a complicated shape and It relates to the manufacturing method.

遠心圧縮機等に用いられる羽根車の中で、図12に示される心板2、側板3、羽根1から構成される羽根車10の製造では、通常それらの構成部材を溶接して接合し一体化する。この羽根車の溶接方法としては、図13に示されるように個別部材として加工され表面にニッケル基合金等からなる耐食性の耐食被覆層4を被覆した羽根1、心板2、側板3を、アーク溶接、MIG溶接、TIG溶接等のアーク溶接方法で溶接部に肉盛ビード6を形成して肉盛溶接する方法がある。また図14に示されるように、精密鋳造と機械加工による削り出し等で心板2と一体に形成した羽根1を、羽根を溶接する開先(溝部)を開孔した側板3と重ね合わせて、開先をアーク溶接法で充填肉盛ビード7を形成して肉盛溶接して羽根端部と側板を接合する方法が多く用いられている。   Among the impellers used in centrifugal compressors and the like, in the manufacture of the impeller 10 composed of the core plate 2, the side plate 3, and the vanes 1 shown in FIG. Turn into. As shown in FIG. 13, the impeller is welded with the blade 1, the core plate 2, and the side plate 3 processed as individual members and coated with a corrosion-resistant corrosion-resistant coating layer 4 made of a nickel-based alloy or the like on the surface. There is a method of overlay welding by forming the overlay beads 6 in the welded portion by an arc welding method such as welding, MIG welding, or TIG welding. Further, as shown in FIG. 14, the blade 1 formed integrally with the core plate 2 by precision casting and machining or the like is overlapped with the side plate 3 having a groove (groove) where the blade is welded. A method of joining the blade end portion and the side plate by forming the filling overlay bead 7 by the arc welding method and overlay welding is often used.

しかし、前者は多数の部材の位置合わせを必要とし充分な精度が得にくく所定の性能が得られない問題がある。また心板2と側板3との間の空隙が狭い場合には、溶接部に溶接棒や溶接トーチが入らずに溶接が困難になるなどの問題がある。さらに、耐食被覆層を有する構成部材を溶接する場合には溶接部の充填肉盛ビード7部分での化学組成が大きく変化し、所定の強度や耐食性が得られない問題がある。   However, the former requires alignment of a large number of members, and there is a problem that sufficient accuracy is difficult to obtain and a predetermined performance cannot be obtained. Moreover, when the space | gap between the core plate 2 and the side plate 3 is narrow, there exists a problem that welding becomes difficult without a welding rod or a welding torch entering a welding part. Furthermore, when a component having a corrosion-resistant coating layer is welded, there is a problem that the chemical composition in the filled overlay bead 7 portion of the welded portion is greatly changed, and predetermined strength and corrosion resistance cannot be obtained.

後者は、側板の外側から溶接するために心板2と側板3との間の空隙が狭い場合にも適用できる利点があるが、溶接時の入熱量が多いために溶接後の変形が大きく、また溶接アークの不均一により羽根1と側板3との接合部に形成される肉盛ビードの形状や化学組成が不均質になりやすい等の問題がある。   The latter has the advantage that it can be applied even when the gap between the core plate 2 and the side plate 3 is narrow in order to weld from the outside of the side plate, but because of the large amount of heat input during welding, the deformation after welding is large, Further, there is a problem that the shape and chemical composition of the built-up bead formed at the joint between the blade 1 and the side plate 3 are likely to be non-uniform due to non-uniform welding arc.

このような問題を解決する方法として、例えば特許文献1に見られるように、心板を鍛造と切削加工により形成するとともに羽根を精密鋳造により形成し、複数の羽根と心板とを組み合わせて羽根の位置を設定した後に複数の羽根と心板を溶接し、熱処理により所定の機械的性質を付与し、その後に精密仕上げ加工を施し、所定の形状と寸法に仕上げる技術が公開されている。   As a method for solving such a problem, for example, as seen in Patent Document 1, a core plate is formed by forging and cutting, and a blade is formed by precision casting, and a plurality of blades and a core plate are combined to form a blade. After the position is set, a technique is disclosed in which a plurality of blades and a core plate are welded, given a predetermined mechanical property by heat treatment, and then subjected to precision finishing to finish to a predetermined shape and size.

一方、遠心圧縮機や軸流ポンプ等に用いられる材料としては、炭素鋼からステンレス鋼まで鉄を主成分とする合金が通常用いられている。移送される気体の中には、硫化水素など金属に対して腐食性を有する気体も存在するため、移送対象となる気体の腐食性に応じて使用する金属材料を選定している。特に、腐食性の高い気体を移送する圧縮機等では、ニッケルを主成分とするニッケル基合金が用いられる場合もある。しかし、ニッケル基合金は、鉄を主成分とする合金と比較して材料強度が低い合金が多く、圧縮機やポンプの設計に制限を及ぼす場合がある。   On the other hand, as materials used for centrifugal compressors, axial pumps, and the like, alloys mainly composed of iron from carbon steel to stainless steel are usually used. Among gases to be transferred, there are gases that are corrosive to metals such as hydrogen sulfide, and therefore metal materials to be used are selected according to the corrosivity of the gas to be transferred. In particular, a nickel-base alloy containing nickel as a main component may be used in a compressor or the like that transports a highly corrosive gas. However, many nickel-based alloys have lower material strength than iron-based alloys, and may limit the design of compressors and pumps.

この問題を解決する方法として、例えば特許文献2に見られるように、ステンレス鋼からなるポンプ部品の母材表面にニッケル基合金で被覆することにより、鉄を主成分とする合金が持つ強度と、ニッケル基合金が持つ耐食性と耐摩耗性を有する被覆部材を提供する技術が公開されている。   As a method for solving this problem, for example, as seen in Patent Document 2, by coating the base material surface of a pump component made of stainless steel with a nickel-based alloy, the strength of an alloy containing iron as a main component, A technique for providing a covering member having the corrosion resistance and wear resistance of a nickel-based alloy has been disclosed.

特開平9−239484公報Japanese Patent Laid-Open No. 9-239484 特許第3886394号公報Japanese Patent No. 3886394

上記の公知技術では、複雑な形状の羽根車を製造後に羽根車表面を高耐食性材料で均一に被覆することが困難である、あるいは表面被覆部材に精密仕上げ加工を施して所定の形状と寸法に仕上げることが困難である等の技術課題がある。また、予めニッケル基合金で被覆した部材を溶接して遠心圧縮機等を製造した場合に、所定の形状と寸法に仕上げることが困難である他に、ニッケル基合金で被覆した部材の溶接部近傍が所定の強度や耐食性を得ることができない等の技術課題がある。   In the above-described known technology, it is difficult to uniformly coat the impeller surface with a highly corrosion-resistant material after manufacturing the impeller having a complicated shape, or the surface covering member is subjected to precision finishing to obtain a predetermined shape and size. There are technical problems such as difficulty in finishing. In addition, when a centrifugal compressor or the like is manufactured by welding a member previously coated with a nickel-base alloy, it is difficult to finish to a predetermined shape and size, and in the vicinity of the welded portion of the member coated with a nickel-base alloy However, there are technical problems such as inability to obtain predetermined strength and corrosion resistance.

本発明の目的は、材料強度に関する設計上の制限を少なくし、かつ安価で耐食性に優れた羽根車およびその製造方法を提供することにある。   An object of the present invention is to provide an impeller that reduces design restrictions on material strength, is inexpensive, and has excellent corrosion resistance, and a method for manufacturing the impeller.

本発明は、羽根と心板と側板を有し、前記羽根と心板と側板の少なくとも二つを溶接接合して形成された羽根車において、前記羽根と心板と側板に鉄を主成分とする合金を使用し、かつ前記羽根と心板と側板の表面をニッケルを主成分とするニッケル基合金の耐食被覆層で被覆し、前記羽根と心板と側板の溶接部が、前記ニッケル基合金の耐食被覆層に相当する成分を有する合金から構成されたことを特徴とする。   The present invention has an impeller having a blade, a core plate, and a side plate, and is formed by welding and joining at least two of the blade, the core plate, and the side plate. And the surfaces of the blade, core plate, and side plate are coated with a nickel-based alloy corrosion-resistant coating layer containing nickel as a main component, and the welded portion of the blade, core plate, and side plate is the nickel-based alloy. It is comprised from the alloy which has a component corresponded to this corrosion-resistant coating layer.

また、前記羽根と心板は予め一体に形成されていることを特徴とする。   The blade and the core plate are integrally formed in advance.

また、前記羽根が溶接される心板及び側板の少なくとも一方に、羽根先端を収容し溶接部の位置決めを行う開先を設けたことを特徴とする。   Further, at least one of the core plate and the side plate to which the blade is welded is provided with a groove that accommodates the blade tip and positions the welded portion.

また、前記開先内に前記羽根の先端を突出させたことを特徴とする。   Further, the tip of the blade is protruded into the groove.

また、羽根と心板と側板を有し、前記羽根と心板と側板の少なくとも二つを溶接接合して形成された羽根車において、前記羽根に耐食性合金を使用し、前記心板と側板に鉄を主成分とする合金を使用し、かつ前記心板と側板の表面をニッケルを主成分とするニッケル基合金の耐食被覆層で被覆し、前記羽根と心板と側板の溶接部が、前記ニッケル基合金の耐食被覆層に相当する成分を有する合金から構成されたことを特徴とする。   Further, in an impeller having a blade, a core plate, and a side plate, and formed by welding and joining at least two of the blade, the core plate, and the side plate, a corrosion-resistant alloy is used for the blade, and the core plate and the side plate are used. An iron-based alloy is used, and the surface of the core plate and the side plate is coated with a nickel-based alloy corrosion-resistant coating layer containing nickel as a main component, and the welded portion of the blade, the core plate, and the side plate is It is characterized by comprising an alloy having a component corresponding to a corrosion-resistant coating layer of a nickel-based alloy.

また、前記羽根を構成する耐食性合金としては、ニッケル基合金がよい。例えば、54mass%Ni−19mass%Cr−5mass%Nb−3mass%Moの組成を持つニッケル基合金、または42mass%Ni−32mass%Fe−21mass%Cr−3mass%Moの組成を持つニッケル基合金がよい。   Moreover, as a corrosion-resistant alloy which comprises the said blade | wing, a nickel base alloy is good. For example, a nickel-base alloy having a composition of 54 mass% Ni-19 mass% Cr-5 mass% Nb-3 mass% Mo or a nickel-base alloy having a composition of 42 mass% Ni-32 mass% Fe-21 mass% Cr-3 mass% Mo is preferable. .

また、前記羽根が溶接される心板及び側板の少なくとも一方に、羽根先端を収容し溶接部の位置決めを行う開先を設けたことを特徴とする。   Further, at least one of the core plate and the side plate to which the blade is welded is provided with a groove that accommodates the blade tip and positions the welded portion.

また、前記開先内に羽根の先端を突出させたことを特徴とする。   Further, the tip of the blade is protruded into the groove.

さらに、羽根と心板と側板を有し、前記羽根と心板と側板の少なくとも二つを溶接接合して形成された羽根車であって、前記羽根と心板と側板に鉄を主成分とする合金を使用し、かつ前記羽根と心板と側板の表面をニッケルを主成分とするニッケル基合金の耐食被覆層で被覆し、前記羽根と心板と側板の溶接部が、前記ニッケル基合金の耐食被覆層に相当する成分を有する合金から構成される羽根車において、鉄を主成分とする合金により前記羽根と心板と側板を形成する工程と、前記羽根と心板と側板の表面をニッケル基合金で被覆して耐食被覆層を形成する工程と、前記耐食被覆層が形成された羽根と心板及び側板の少なくとも一方を接合させて羽根位置を位置決めする工程と、接合された羽根と心板および側板の少なくとも一方を溶接する工程とを有することを特徴とする。   Further, the impeller has a blade, a core plate, and a side plate, and is formed by welding and joining at least two of the blade, the core plate, and the side plate, and the blade, the core plate, and the side plate mainly include iron. And the surfaces of the blade, core plate, and side plate are coated with a nickel-based alloy corrosion-resistant coating layer containing nickel as a main component, and the welded portion of the blade, core plate, and side plate is the nickel-based alloy. In the impeller composed of an alloy having a component corresponding to the corrosion-resistant coating layer, a step of forming the blade, the core plate, and the side plate with an iron-based alloy, and the surfaces of the blade, the core plate, and the side plate A step of forming a corrosion-resistant coating layer by coating with a nickel-based alloy, a step of positioning at least one of the blade, the core plate and the side plate on which the corrosion-resistant coating layer is formed, and the bonded blade Weld at least one of core plate and side plate And having a that step.

さらに、羽根と心板と側板を有し、前記羽根と心板と側板の少なくとも二つを溶接接合して形成される羽根車であって、前記羽根にニッケル基合金を使用し、心板と側板に鉄を主成分とする合金を使用し、かつ前記心板と側板の表面をニッケルを主成分とするニッケル基合金の耐食被覆層で被覆し、前記羽根と心板と側板の溶接部が、前記ニッケル基合金の耐食被覆層に相当する成分を有する合金から構成される羽根車において、ニッケル基合金で前記羽根を形成する工程と、鉄を主成分とする合金により前記心板と側板を形成する工程と、前記心板と側板の表面をニッケル基合金で被覆して耐食被覆層を形成する工程と、前記羽根と心板及び側板の少なくとも一方を接合させて羽根位置を位置決めする工程と、接合された羽根と心板および側板の少なくとも一方を溶接する工程とを有することを特徴とする。   Further, the impeller has a blade, a core plate, and a side plate, and is formed by welding and joining at least two of the blade, the core plate, and the side plate, using a nickel-based alloy for the blade, An iron-based alloy is used as the side plate, and the surface of the core plate and the side plate is coated with a nickel-based alloy corrosion-resistant coating layer containing nickel as a main component, and the welded portion between the blade, the core plate, and the side plate In the impeller composed of an alloy having a component corresponding to the corrosion-resistant coating layer of the nickel base alloy, the step of forming the blades with a nickel base alloy, and the core plate and the side plate with an alloy mainly composed of iron A step of forming a corrosion-resistant coating layer by coating the surfaces of the core plate and the side plate with a nickel-based alloy, and a step of positioning at least one of the blade, the core plate and the side plate, and positioning the blade position; Jointed feather and mandrel and Characterized in that a step of welding at least one plate.

さらに、前記羽根と接合される心板及び側板の少なくとも一方の突き合わせ面に開先を設け、前記羽根を前記開先に挿入した後に羽根と前記心板および側板の少なくとも一方を溶接することを特徴とする。   Furthermore, a groove is provided on at least one abutting surface of the core plate and the side plate joined to the blade, and at least one of the blade, the core plate, and the side plate is welded after the blade is inserted into the groove. And

さらに、前記羽根と接合される心板及び側板の少なくとも一方の前記羽根との接合面に前記羽根に向けて所定の断面形状と深さの開先を設ける工程と、前記開先の底部と羽根の端部とを裏波溶接する工程と、前記開先底部に溶加材を供給して開先を充填肉盛溶接する工程とを有することを特徴とする。   Furthermore, a step of providing a groove having a predetermined cross-sectional shape and depth toward the blade on a joint surface of at least one of a core plate and a side plate to be bonded to the blade, and a bottom portion of the groove and the blade And a process of supplying a filler metal to the groove bottom and filling and welding the groove.

本発明の羽根車では、構成部材の基材として強度の高い材料を用い基材表面を耐食性に優れるニッケルを主成分としたニッケル基合金で被覆しているため、強度と耐食性を兼ね備えた遠心圧縮機や軸流ポンプ等を提供できる効果がある。また、ニッケルの使用量を削減できるため、全体がニッケル基合金で製造された羽根車と比較して安価な羽根車を提供できる効果がある。   In the impeller of the present invention, a high-strength material is used as the base material of the constituent member, and the base material surface is coated with a nickel-based alloy mainly composed of nickel, which has excellent corrosion resistance. Therefore, centrifugal compression combines strength and corrosion resistance. There is an effect that a machine, an axial flow pump and the like can be provided. Moreover, since the usage-amount of nickel can be reduced, compared with the impeller manufactured entirely with the nickel base alloy, there exists an effect which can provide an inexpensive impeller.

また、構成部材の羽根にニッケル基合金を使用することにより、羽根車の耐久性をさらに向上することができる。   Moreover, durability of an impeller can further be improved by using a nickel base alloy for the blade | wing of a structural member.

本発明の実施例1の羽根車の模式図。The schematic diagram of the impeller of Example 1 of this invention. 本発明の実施例1の変形例の模式図。The schematic diagram of the modification of Example 1 of this invention. 本発明の実施例1の他の変形例の模式図。The schematic diagram of the other modification of Example 1 of this invention. 本発明の実施例2の羽根車の模式図。The schematic diagram of the impeller of Example 2 of this invention. 本発明の実施例2の変形例の模式図。The schematic diagram of the modification of Example 2 of this invention. 本発明の実施例2の他の変形例の模式図。The schematic diagram of the other modification of Example 2 of this invention. 本発明の実施例3の羽根車の模式図。The schematic diagram of the impeller of Example 3 of this invention. 本発明の実施例3の変形例の模式図。The schematic diagram of the modification of Example 3 of this invention. 本発明の実施例3の他の変形例の模式図。The schematic diagram of the other modification of Example 3 of this invention. 本発明の実施例4の羽根車の模式図。The schematic diagram of the impeller of Example 4 of this invention. 本発明の実施例4の羽根車の断面図。Sectional drawing of the impeller of Example 4 of this invention. 一般的な遠心圧縮機用羽根車の外観を示す斜視図。The perspective view which shows the external appearance of the general impeller for centrifugal compressors. 従来の羽根車溶接方法の一例を示す模式図。The schematic diagram which shows an example of the conventional impeller welding method. 従来の羽根車溶接方法の他の例を示す模式図。The schematic diagram which shows the other example of the conventional impeller welding method.

以下、本発明の詳細について実施例を用いて説明する。   Hereinafter, details of the present invention will be described using examples.

図1に、実施例1の羽根車110の模式図を示す。羽根車110は羽根101の上下に設けた心板102あるいは側板103の溶接部に、羽根端部が挿入される開先Gを設け、羽根101と心板102および側板103とが溶接された構造を有する。ここで、羽根101、心板102、側板103のいずれも、基材としてCrが約2mass%添加された低合金鋼が用いられその表面はニッケル基合金からなる耐食被覆層4で覆われている。   In FIG. 1, the schematic diagram of the impeller 110 of Example 1 is shown. The impeller 110 has a structure in which a groove G into which a blade end portion is inserted is provided at a welded portion of a core plate 102 or a side plate 103 provided above and below the blade 101, and the blade 101, the core plate 102, and the side plate 103 are welded. Have Here, each of the blade 101, the core plate 102, and the side plate 103 is made of a low alloy steel to which about 2 mass% of Cr is added as a base material, and the surface thereof is covered with a corrosion-resistant coating layer 4 made of a nickel-based alloy. .

次にこの羽根車110の製造方法を説明する。先ず、羽根車を構成する羽根101、心板102、側板103の各々の構成部材を、低合金鋼の鋳造あるいは鍛造等と切削加工とを組み合わせて所定の形状と寸法に加工した。次に、アーク溶射法を用いてニッケル基合金を各構成部材の表面に溶射付着させ耐食被覆層4を形成した。次に、耐食被覆層4を付着させた心板102と側板103に羽根101の溶接位置を位置決めする開先Gを加工形成した。   Next, a method for manufacturing the impeller 110 will be described. First, the constituent members of the blade 101, the core plate 102, and the side plate 103 constituting the impeller were processed into a predetermined shape and size by combining low alloy steel casting or forging and cutting. Next, a nickel-based alloy was sprayed and deposited on the surface of each component using an arc spraying method to form a corrosion-resistant coating layer 4. Next, a groove G for positioning the welding position of the blade 101 was formed on the core plate 102 and the side plate 103 to which the corrosion-resistant coating layer 4 was adhered.

羽根車の構成部材を以下の手順で組み合わせて羽根車を製造した。先ず、羽根101を心板102に形成した開先Gに挿入して位置決めした後に、羽根101と心板102との間に形成されるくさび状の空隙の羽根側に耐食被覆層4のニッケル基合金相当の化学組成を持つ溶接合金を供給し、TIG溶接法で溶解して心板102の羽根側に裏波ビード5を形成させた。裏波ビードは片側溶接において完全な溶接状態を持つ溶接部裏面に形成される波型のビードをいう。   The impeller was manufactured by combining the components of the impeller according to the following procedure. First, after the blade 101 is inserted into the groove G formed on the core plate 102 and positioned, the nickel base of the corrosion-resistant coating layer 4 is formed on the blade side of the wedge-shaped gap formed between the blade 101 and the core plate 102. A welding alloy having a chemical composition equivalent to the alloy was supplied and melted by the TIG welding method to form the back bead 5 on the blade side of the core plate 102. The back wave bead is a wavy bead formed on the back surface of the welded portion having a complete welded state in one-side welding.

次に、羽根101と心板102間の空隙に、耐食被覆層4のニッケル基合金相当の化学組成を持つ合金、すなわち耐食被覆層4に近い組成と耐食性を持つ合金を溶加材として供給し開先Gに肉盛溶接を行い、充填肉盛ビード7を形成し羽根101と心板102の空隙を充填して所定の形状を形成した。さらに、羽根101と心板102が溶接された溶接体と側板3を組み合わせて溶接位置を位置決めした後に、同様の手順で羽根101と側板103を裏波溶接し、次いで肉盛溶接により充填肉盛ビード7で羽根101と側板103の空隙を充填して羽根車110を製造した。   Next, an alloy having a chemical composition equivalent to the nickel-based alloy of the corrosion-resistant coating layer 4, that is, an alloy having a composition close to that of the corrosion-resistant coating layer 4 and corrosion resistance is supplied as a filler material into the gap between the blade 101 and the core plate 102. Overlay welding was performed on the groove G to form a filled overlaid bead 7, and the gap between the blade 101 and the core plate 102 was filled to form a predetermined shape. Furthermore, after positioning the welding position by combining the welded body to which the blade 101 and the core plate 102 are welded and the side plate 3, the blade 101 and the side plate 103 are welded in the same manner in the same procedure, and then filling is performed by overlay welding. An impeller 110 was manufactured by filling the gap between the blade 101 and the side plate 103 with the bead 7.

上記実施例が示すように、羽根車を構成する部材の基材として低合金鋼が用いられているため、低合金鋼がもつ強度をそのまま利用することができる。加えて、基材表面がニッケル基合金で被覆されているとともに、構成部材の溶加材として耐食被覆層4のニッケル基合金相当の溶接合金を用いることにより溶接部外表面もニッケル基合金が露出しているため、羽根車は耐食被覆層と同じ耐食性を有し、かつニッケルの使用量を削減できるためニッケル基合金で製造された羽根車と比較して安価な羽根車を提供できる。   As shown in the above embodiment, since the low alloy steel is used as the base material of the member constituting the impeller, the strength of the low alloy steel can be used as it is. In addition, the surface of the base material is coated with a nickel-base alloy, and a nickel-base alloy is also exposed on the outer surface of the welded portion by using a weld alloy corresponding to the nickel-base alloy of the corrosion-resistant coating layer 4 as a filler for the constituent members. Therefore, since the impeller has the same corrosion resistance as the corrosion-resistant coating layer and can reduce the amount of nickel used, it is possible to provide an impeller that is less expensive than an impeller manufactured from a nickel-based alloy.

さらに、上記の構成によれば、羽根101の端部が心板102と側板103の開先Gの内部に突出して溶接されるため、強固な接合強度と高い寸法精度を持つ羽根車が得られる。   Furthermore, according to the above configuration, since the end portion of the blade 101 protrudes into the groove G of the core plate 102 and the side plate 103 and is welded, an impeller having strong joint strength and high dimensional accuracy can be obtained. .

上記実施例は、外装体を形成する心板102と側板103の両方に羽根101の位置決めをする開先を形成したが、図2に示す変形例、図3に示す他の変形例のように、心板2と側板3の一方のみに位置決め用の開先Gを形成し、羽根111または121の一端を開先Gに挿入して位置を決定し肉盛溶接により羽根と心板または側板の空隙を充填し、他端は通常の肉盛溶接法により他の部材を接合して同様の溶接手順により羽根車を製造してもよい。この場合は、図1の実施例に比べやや寸法精度と強度に劣るが、工程が簡略化されるとともに実用上十分な性能が得られる。   In the above embodiment, the groove for positioning the blades 101 is formed on both the core plate 102 and the side plate 103 forming the exterior body, but as in the modification shown in FIG. 2 and the other modification shown in FIG. The groove G for positioning is formed only in one of the core plate 2 and the side plate 3, and one end of the blade 111 or 121 is inserted into the groove G to determine the position, and the blade and the core plate or side plate are formed by overlay welding. The impeller may be manufactured by a similar welding procedure by filling the gap and joining the other end to the other end by a normal overlay welding method. In this case, the dimensional accuracy and strength are slightly inferior to those of the embodiment of FIG. 1, but the process is simplified and practically sufficient performance is obtained.

図4は、本発明の実施例2の羽根車210の模式図である。羽根車210は羽根201の両端の心板202あるいは側板203に羽根端部が挿入される開先Gを設け、羽根201と心板202、あるいは側板203とが溶接された構造を有する。   FIG. 4 is a schematic diagram of an impeller 210 according to the second embodiment of the present invention. The impeller 210 has a structure in which a groove G into which a blade end portion is inserted is provided in the core plate 202 or the side plate 203 at both ends of the blade 201 and the blade 201 and the core plate 202 or the side plate 203 are welded.

ここで、羽根201は、耐食性を有する54mass%Ni−19mass%Cr−5mass%Nb−3mass%Moの組成を持つニッケル基合金を加工して作成し、心板202、側板203は、いずれも13mass%Crのマルテンサイト系ステンレス鋼が基材として用いられており、その表面はニッケル基合金からなる耐食被覆層4で覆われている。   Here, the blade 201 is made by processing a nickel-base alloy having a composition of 54 mass% Ni-19 mass% Cr-5 mass% Nb-3 mass% Mo having corrosion resistance, and the core plate 202 and the side plate 203 are both 13 mass. % Cr martensitic stainless steel is used as a substrate, and its surface is covered with a corrosion-resistant coating layer 4 made of a nickel-based alloy.

次に、この羽根車の製造方法を示す。先ず、羽根車210を構成する羽根201、心板202、側板203の各々の構成部材は、素材金属の鋳造あるいは鍛造等と切削加工とを組み合わせて、所定の形状と寸法に加工された。ここで、心板202と側板203に羽根201の溶接位置を決定する開先Gを予め加工形成した。次に、アーク溶射法を用いて心板202と側板203の表面全面にニッケル基合金からなる耐食被覆層4を付着させた。   Next, the manufacturing method of this impeller is shown. First, each of the constituent members of the blade 201, the core plate 202, and the side plate 203 constituting the impeller 210 was processed into a predetermined shape and size by a combination of casting or forging of a raw metal and cutting. Here, a groove G for determining the welding position of the blade 201 was formed on the core plate 202 and the side plate 203 in advance. Next, the corrosion-resistant coating layer 4 made of a nickel-based alloy was adhered to the entire surface of the core plate 202 and the side plate 203 using an arc spraying method.

このように開先を設けてからニッケル基合金の被覆を行い、開先内まで合金層を設けることにより、開先内の溶接金属部との溶接性が向上する。また、開先内に鋼材が露出していないため、耐食性を低下させる鉄とニッケルとの混合層が生じにくい。一方、被覆層を設けてから開先を設けることは、作業工程が容易であり好ましい。   Thus, after providing a groove | channel, it coat | covers with a nickel base alloy, and a weldability with the weld metal part in a groove | channel improves by providing an alloy layer in the groove | channel. Moreover, since the steel material is not exposed in the groove, a mixed layer of iron and nickel that lowers the corrosion resistance is unlikely to occur. On the other hand, providing the groove after providing the coating layer is preferable because the working process is easy.

各々表面被覆された心板202と側板203と羽根201を以下の手順で組み合わせて、羽根車を製造した。先ず、羽根201と心板202との空隙の羽根側、および、羽根201と側板203との空隙の羽根側に、耐食被覆層4のニッケル基合金と相当の化学組成を持つ溶接金属を若干溶着させた。次に、溶接金属が溶着された羽根201を心板202に形成した開先Gに挿入して位置決めを行った。   The impeller was manufactured by combining the core plate 202, the side plate 203, and the blades 201, which were respectively surface-coated, in the following procedure. First, a slightly weld metal having a chemical composition equivalent to the nickel-based alloy of the corrosion-resistant coating layer 4 is deposited on the blade side of the gap between the blade 201 and the core plate 202 and on the blade side of the gap between the blade 201 and the side plate 203. I let you. Next, the blades 201 welded with the weld metal were inserted into the groove G formed on the core plate 202 for positioning.

先ず始めに、羽根201に溶着させた溶接金属をTIG溶接法で再溶解し、心板2の羽根面側に裏波ビード5を形成させた。次に、羽根201と心板202の空隙に耐食被覆層4のニッケル基合金相当の化学組成を持つ合金を溶加材として供給して開先に充填肉盛ビード7を形成し、羽根201と心板202の空隙を充填して、所定の形状を形成した。   First, the weld metal welded to the blade 201 was redissolved by the TIG welding method, and the back bead 5 was formed on the blade surface side of the core plate 2. Next, an alloy having a chemical composition equivalent to the nickel-based alloy of the corrosion-resistant coating layer 4 is supplied as a filler material into the gap between the blade 201 and the core plate 202 to form the filled cladding bead 7 in the groove, A predetermined shape was formed by filling the gap of the core plate 202.

さらに、羽根201と心板202が溶接された溶接体と側板203を組み合わせて、羽根201と心板202の接合方法と同様の手順で、羽根201と側板203を接合し、羽根車210を製造した。   Further, the blade 201 and the side plate 203 are joined in the same procedure as the joining method of the blade 201 and the core plate 202 by combining the welded body in which the blade 201 and the core plate 202 are welded, and the side plate 203 to manufacture the impeller 210. did.

上記実施例2が示すように、羽根車の心板202と側板203の構成部材としてマルテンサイト系ステンレス鋼が用いられているためその強度を利用することができる。加えて、心板202と側板203の基材表面がニッケル基合金で被覆されているとともに、心板202および側板203と羽根201の溶接部の外表面もニッケル基合金が露出しているため、羽根車201は耐食被覆層と同等の耐食性を有する。さらに、心板202と側板203の基材がマルテンサイト系ステンレス鋼であって羽根車に使用するニッケルの量を削減できるため、ニッケル基合金で製造された羽根車と比較して、安価な羽根車を提供できる。   As the second embodiment shows, since martensitic stainless steel is used as a constituent member of the impeller core plate 202 and the side plate 203, the strength can be utilized. In addition, since the base material surfaces of the core plate 202 and the side plate 203 are coated with the nickel base alloy, and the nickel base alloy is also exposed on the outer surface of the welded portion of the core plate 202 and the side plate 203 and the blade 201, The impeller 201 has a corrosion resistance equivalent to that of the corrosion-resistant coating layer. Furthermore, since the base material of the core plate 202 and the side plate 203 is martensitic stainless steel and the amount of nickel used for the impeller can be reduced, the impeller is less expensive than an impeller manufactured from a nickel-based alloy. Can provide a car.

実施例2は羽根201に54mass%Ni−19mass%Cr−5mass%Nb−3mass%Moの組成を持つ耐食性のニッケル基合金を用いるため、実施例1より高価になるものの、最も損傷を受けやすい羽根部分の耐久性が大幅に向上する。   Since the second embodiment uses a corrosion-resistant nickel-based alloy having a composition of 54 mass% Ni-19 mass% Cr-5 mass% Nb-3 mass% Mo for the vane 201, the vane is most easily damaged although it is more expensive than the first embodiment. The durability of the part is greatly improved.

上記実施例は、心板2と側板3の両方に羽根201の位置決めをする開先Gを形成したが、図5に示す変形例、図6に示す他の変形例のように、羽根211、羽根221を用意し、心板202と側板203の少なくとも一方のみに位置決め用の開先Gを形成して溶接し、他方は通常の肉盛溶接法により部材を接合し、同様の溶接手順により羽根車を製造してもよい。この場合も、図4の実施例2に比べやや寸法精度と強度に劣るが、工程が簡略化されるとともに実用上十分な性能が得られる。   In the above embodiment, the groove G for positioning the blade 201 is formed on both the core plate 2 and the side plate 3, but as in the modification shown in FIG. 5 and the other modification shown in FIG. A blade 221 is prepared, a positioning groove G is formed on at least one of the core plate 202 and the side plate 203 and welded, and the other is joined by a normal overlay welding method. A car may be manufactured. In this case as well, the dimensional accuracy and strength are slightly inferior to those of Example 2 in FIG. 4, but the process is simplified and practically sufficient performance is obtained.

図7は、本発明の実施例3の羽根車の模式図である。羽根車310は羽根301の両端に、羽根を溶接するための開先Gを有し、羽根301と心板302あるいは側板303が溶接された構造を有する。ここで、羽根301は、耐食性を有する42mass%Ni−32mass%Fe−21mass%Cr−3mass%Moの組成を持つニッケル基合金を加工して作成し、心板302、側板303は、いずれも約9mass%のNiが添加された低合金鋼が基材として用いられており、その表面はニッケル基合金からなる耐食被覆層4で覆われている。   FIG. 7 is a schematic diagram of an impeller according to a third embodiment of the present invention. The impeller 310 has a groove G for welding the blades at both ends of the blade 301, and has a structure in which the blade 301 and the core plate 302 or the side plate 303 are welded. Here, the blade 301 is made by processing a nickel-based alloy having a composition of 42 mass% Ni-32 mass% Fe-21 mass% Cr-3 mass% Mo having corrosion resistance, and the core plate 302 and the side plate 303 are all about A low alloy steel to which 9 mass% Ni is added is used as a substrate, and the surface thereof is covered with a corrosion-resistant coating layer 4 made of a nickel-based alloy.

次に、この羽根車の製造方法を示す。先ず、羽根車を構成する羽根301、心板302、側板303の各々の構成部材は、素材金属を鋳造あるいは鍛造等と切削加工とを組み合わせて所定の形状と寸法に加工された。ここで、心板302と側板303に羽根301を溶接するための開先Gを予め加工形成した。次に、アーク溶射法を用いて心板302と側板303の表面全面にニッケル基合金の耐食被覆層4を付着させた。   Next, the manufacturing method of this impeller is shown. First, the constituent members of the blade 301, the core plate 302, and the side plate 303 constituting the impeller were processed into a predetermined shape and size by combining raw metal casting or forging and cutting. Here, a groove G for welding the blade 301 to the core plate 302 and the side plate 303 was formed in advance. Next, the corrosion-resistant coating layer 4 of the nickel base alloy was adhered to the entire surface of the core plate 302 and the side plate 303 by using an arc spraying method.

次にニッケル基合金で表面被覆された心板302と側板303と羽根301を以下の手順で組み合わせて羽根車310を製造した。先ず、羽根301と心板302とを位置決めした後に、羽根301と心板302の空隙に羽根301に使用したニッケル基合金相当の化学組成を持つ合金を供給し、レーザー溶接法で挿入した合金を溶解することにより、心板302の羽根面側に裏波ビード5を形成させた。次に、羽根301と心板302の空隙に羽根301に使用したニッケル基合金相当の化学組成を持つ合金を溶加材として供給して開先Gに充填肉盛ビード7を形成して、羽根301と心板302の広い空隙を充填し所定の形状を形成した。   Next, the impeller 310 was manufactured by combining the core plate 302, the side plate 303, and the blades 301, which were surface-coated with a nickel-based alloy, in the following procedure. First, after positioning the blade 301 and the core plate 302, an alloy having a chemical composition equivalent to the nickel-based alloy used for the blade 301 is supplied to the gap between the blade 301 and the core plate 302, and the alloy inserted by laser welding is used. By melting, the back bead 5 was formed on the blade surface side of the core plate 302. Next, an alloy having a chemical composition equivalent to the nickel-based alloy used for the blade 301 is supplied as a filler material to the space between the blade 301 and the core plate 302 to form the fill-up bead 7 in the groove G. A wide gap between 301 and the core plate 302 was filled to form a predetermined shape.

さらに、羽根301と心板302が溶接された溶接体と側板303を組み合わせて、羽根301と心板302を接合した方法と同様の手順で羽根301と側板303を裏波溶接し、肉盛溶接により羽根301と側板303の空隙を埋めて羽根車310を製造した。   Furthermore, the blade 301 and the side plate 303 are back welded in the same procedure as the method of joining the blade 301 and the core plate 302 by combining the welded body in which the blade 301 and the core plate 302 are welded and the side plate 303, and overlay welding. Thus, the impeller 310 was manufactured by filling the gap between the blade 301 and the side plate 303.

実施例3は羽根に42mass%Ni−32mass%Fe−21mass%Cr−3mass%Moの組成を持つニッケル基合金を用いるため、実施例1より高価になるものの、最も損傷を受けやすい羽根部分の耐久性が大幅に向上する。   Since Example 3 uses a nickel-base alloy having a composition of 42 mass% Ni-32 mass% Fe-21 mass% Cr-3 mass% Mo for the blade, although it is more expensive than Example 1, the durability of the blade portion that is most susceptible to damage The characteristics are greatly improved.

上記実施例は、外装体を形成する心板302と側板303の両方に羽根301の位置決めをする開先を形成したが、図8に示す変形例、図9に示す他の変形例のように、羽根311、羽根321を用意し、心板302と側板303の少なくとも一方のみに位置決め用の開先Gを形成して充填肉盛ビード7を形成し、他方は通常の肉盛溶接法により接合部材を製造し、同様の溶接手順により羽根車を製造してもよい。この場合も、図7の実施例3に比べやや寸法精度と強度に劣るが、工程が簡略化されるとともに実用上十分な性能が得られる。   In the above embodiment, the groove for positioning the blades 301 is formed on both the core plate 302 and the side plate 303 forming the exterior body. However, as in the modification shown in FIG. 8 and the other modification shown in FIG. The blade 311 and the blade 321 are prepared, the groove G for positioning is formed only in at least one of the core plate 302 and the side plate 303 to form the filled overlay bead 7, and the other is joined by a normal overlay welding method. A member may be manufactured and an impeller may be manufactured with the same welding procedure. In this case as well, the dimensional accuracy and strength are slightly inferior to those of Example 3 in FIG. 7, but the process is simplified and practically sufficient performance is obtained.

図10に実施例4の模式図を示す。実施例4は羽根401、心板402、側板403から構成される軸流ポンプで用いられる羽根車410を示す。図11はその断面図である。所定の性能を得るため、羽根車410は図10(b)に示すように羽根401と心板402を一体成形した三次元曲面を有しており、精密鋳造した後に機械加工により正確な寸法精度を得ている。   FIG. 10 shows a schematic diagram of the fourth embodiment. The fourth embodiment shows an impeller 410 used in an axial flow pump including a blade 401, a core plate 402, and a side plate 403. FIG. 11 is a sectional view thereof. In order to obtain a predetermined performance, the impeller 410 has a three-dimensional curved surface in which the blade 401 and the core plate 402 are integrally formed as shown in FIG. 10B, and accurate dimensional accuracy is obtained by machining after precision casting. Have gained.

羽根車410の製造方法は、まず側板403の羽根401の溶接される部分に開先Gを形成し、羽根401先端を開先Gに挿入し突き合わせた後、突合せ部を溶接する開先突合せ溶接法により、図10(a)に示すように一体に羽根車を製造する。   In the manufacturing method of the impeller 410, first, a groove G is formed in a portion of the side plate 403 where the blade 401 is welded, and the tip of the blade 401 is inserted into the groove G and abutted. As shown in FIG. 10 (a), the impeller is integrally manufactured by the method.

羽根401と心板402、側板403の構成は、実施例1〜3で説明したと同様の各種の複合金属材料が用いられる。   As the configurations of the blade 401, the core plate 402, and the side plate 403, various composite metal materials similar to those described in the first to third embodiments are used.

実施例4では羽根401と心板402が予め一体に形成されているため、寸法精度及び強度に優れた羽根車を得ることができ、また加工工程を大幅に短縮することができる。   In Example 4, since the blades 401 and the core plate 402 are integrally formed in advance, an impeller excellent in dimensional accuracy and strength can be obtained, and the processing steps can be greatly shortened.

101、111、121、201、211、221、301、311、321:羽根
102、202、302:心板
103、203、303:側板
4:耐食被覆層
5:裏波ビード部
6:肉盛ビード部
7:充填肉盛ビード部
G:開先
101, 111, 121, 201, 211, 221, 301, 311, 321: blades 102, 202, 302: core plate 103, 203, 303: side plate 4: corrosion-resistant coating layer 5: reverse bead 6: overlay bead Part 7: Filled overlay bead part G: Groove

Claims (15)

羽根と心板と側板を有し、前記羽根と心板と側板の少なくとも二つを溶接接合して形成された羽根車において、
前記羽根と心板と側板に鉄を主成分とする合金を使用し、かつ前記羽根と心板と側板の表面をニッケルを主成分とするニッケル基合金の耐食被覆層で被覆し、前記羽根と心板と側板の溶接部が、前記ニッケル基合金の耐食被覆層に相当する成分を有する合金から構成されたことを特徴とする羽根車。
In an impeller having a blade, a core plate, and a side plate, and formed by welding and joining at least two of the blade, the core plate, and the side plate,
An alloy containing iron as a main component is used for the blade, core plate, and side plate, and the surface of the blade, core plate, and side plate is coated with a nickel-based alloy corrosion-resistant coating layer containing nickel as a main component, An impeller characterized in that the welded portion between the core plate and the side plate is made of an alloy having a component corresponding to the corrosion-resistant coating layer of the nickel-based alloy.
請求項1に記載された羽根車において、前記羽根と心板は予め一体に形成されていることを特徴とする羽根車。   2. The impeller according to claim 1, wherein the blade and the core plate are integrally formed in advance. 請求項1または2に記載された羽根車において、前記羽根が溶接される心板及び側板の少なくとも一方に、羽根先端を収容し溶接部の位置決めを行う開先を設けたことを特徴とする羽根車。   3. The impeller according to claim 1, wherein at least one of a core plate and a side plate to which the blade is welded is provided with a groove for receiving the blade tip and positioning the welded portion. car. 請求項3に記載された羽根車において、前記開先内に前記羽根の先端を突出させたことを特徴とする羽根車。   4. The impeller according to claim 3, wherein a tip of the blade is protruded into the groove. 羽根と心板と側板を有し、前記羽根と心板と側板の少なくとも二つを溶接接合して形成された羽根車において、
前記羽根にニッケル基合金を使用し、前記心板と側板に鉄を主成分とする合金を使用し、かつ前記心板と側板の表面をニッケルを主成分とするニッケル基合金の耐食被覆層で被覆し、前記羽根と心板と側板の溶接部が、前記ニッケル基合金の耐食被覆層に相当する成分を有する合金から構成されたことを特徴とする羽根車。
In an impeller having a blade, a core plate, and a side plate, and formed by welding and joining at least two of the blade, the core plate, and the side plate,
A nickel-based alloy is used for the blades, an alloy mainly composed of iron is used for the core plate and the side plate, and the surface of the core plate and the side plate is a corrosion-resistant coating layer of a nickel-based alloy mainly composed of nickel. An impeller characterized in that the welded portion of the blade, the core plate, and the side plate is made of an alloy having a component corresponding to the corrosion-resistant coating layer of the nickel-based alloy.
請求項5に記載された羽根車において、前記羽根が溶接される心板及び側板の少なくとも一方に、羽根先端を収容し溶接部の位置決めを行う開先を設けたことを特徴とする羽根車。   6. The impeller according to claim 5, wherein a groove for accommodating the tip of the blade and positioning the welded portion is provided in at least one of the core plate and the side plate to which the blade is welded. 請求項6に記載された羽根車において、前記開先内に羽根の先端を突出させたことを特徴とする羽根車。   The impeller according to claim 6, wherein a tip of the blade protrudes into the groove. 請求項1乃至7のいずれか1項に記載の羽根車を有する遠心圧縮機。   A centrifugal compressor having the impeller according to any one of claims 1 to 7. 請求項1乃至7のいずれか1項に記載の羽根車を有する軸流ポンプ。   The axial flow pump which has an impeller of any one of Claims 1 thru | or 7. 羽根と心板と側板を有し、前記羽根と心板と側板の少なくとも二つを溶接接合して形成された羽根車であって、前記羽根と心板と側板に鉄を主成分とする合金を使用し、かつ前記羽根と心板と側板の表面をニッケルを主成分とするニッケル基合金の耐食被覆層で被覆し、前記羽根と心板と側板の溶接部が、前記ニッケル基合金の耐食被覆層に相当する成分を有する合金から構成される羽根車において、
鉄を主成分とする合金により前記羽根と心板と側板を形成する工程と、前記羽根と心板と側板の表面をニッケル基合金で被覆して耐食被覆層を形成する工程と、前記耐食被覆層が形成された羽根と心板及び側板の少なくとも一方を接合させて羽根位置を位置決めする工程と、接合された羽根と心板および側板の少なくとも一方を溶接する工程とを有することを特徴とする羽根車の製造方法。
An impeller having a blade, a core plate, and a side plate, and formed by welding and joining at least two of the blade, the core plate, and the side plate, and an alloy mainly composed of iron in the blade, the core plate, and the side plate And the surfaces of the blade, core plate, and side plate are coated with a nickel-based alloy corrosion-resistant coating layer containing nickel as a main component, and the welded portion of the blade, core plate, and side plate is corrosion-resistant of the nickel-based alloy. In an impeller composed of an alloy having a component corresponding to the coating layer,
Forming the blade, the core plate, and the side plate from an alloy containing iron as a main component; coating the surfaces of the blade, the core plate, and the side plate with a nickel-based alloy to form a corrosion-resistant coating layer; and the corrosion-resistant coating. And a step of positioning at least one of the blade, the core plate, and the side plate on which the layer is formed, and a step of welding at least one of the bonded blade, the core plate, and the side plate. The manufacturing method of an impeller.
羽根と心板と側板を有し、前記羽根と心板と側板の少なくとも二つを溶接接合して形成される羽根車であって、前記羽根にニッケル基合金を使用し、心板と側板に鉄を主成分とする合金を使用し、かつ前記心板と側板の表面をニッケルを主成分とするニッケル基合金の耐食被覆層で被覆し、前記羽根と心板と側板の溶接部が、前記ニッケル基合金の耐食被覆層に相当する成分を有する合金から構成される羽根車において、
ニッケル基合金で前記羽根を形成する工程と、鉄を主成分とする合金により前記心板と側板を形成する工程と、前記心板と側板の表面をニッケル基合金で被覆して耐食被覆層を形成する工程と、前記羽根と心板及び側板の少なくとも一方を接合させて羽根位置を位置決めする工程と、接合された羽根と心板および側板の少なくとも一方を溶接する工程とを有することを特徴とする羽根車の製造方法。
An impeller having a blade, a core plate, and a side plate, formed by welding and joining at least two of the blade, the core plate, and the side plate, and using a nickel-based alloy for the blade, An iron-based alloy is used, and the surface of the core plate and the side plate is coated with a nickel-based alloy corrosion-resistant coating layer containing nickel as a main component, and the welded portion of the blade, the core plate, and the side plate is In an impeller composed of an alloy having a component corresponding to a corrosion-resistant coating layer of a nickel-based alloy,
Forming the blades with a nickel-based alloy; forming the core plate and the side plate with an iron-based alloy; and coating the surface of the core plate and the side plate with a nickel-based alloy to form a corrosion-resistant coating layer. A step of forming, a step of positioning at least one of the blade, the core plate, and the side plate by positioning the blade, and a step of welding at least one of the bonded blade, the core plate, and the side plate. Manufacturing method of impeller.
請求項10または11に記載された羽根車の製造方法において、前記羽根と接合される心板及び側板の少なくとも一方の突き合わせ面に開先を設け、前記羽根を前記開先に挿入した後に羽根と前記心板および側板の少なくとも一方を溶接することを特徴とする羽根車の製造方法。   The impeller manufacturing method according to claim 10 or 11, wherein a groove is provided on at least one abutting surface of a core plate and a side plate to be joined to the blade, and the blade is inserted into the groove after the blade is inserted into the groove. An impeller manufacturing method comprising welding at least one of the core plate and the side plate. 請求項10または11に記載された羽根車の製造方法において、前記羽根と接合される心板及び側板の少なくとも一方の前記羽根との接合面に前記羽根に向けて所定の断面形状と深さの開先を設ける工程と、前記開先の底部と羽根の端部とを裏波溶接する工程と、前記開先底部に溶加材を供給して開先を充填肉盛溶接する工程とを有することを特徴とする羽根車の製造方法。   The impeller manufacturing method according to claim 10 or 11, wherein a predetermined cross-sectional shape and depth are formed toward the blade on a joint surface of at least one of a core plate and a side plate joined to the blade. A step of providing a groove, a step of welding the bottom of the groove and the end of the blade, and a step of supplying a filler material to the groove bottom and filling and welding the groove. The manufacturing method of the impeller characterized by the above-mentioned. 請求項10乃至13のいずれか1項に記載の製造方法により製造された羽根車を有する遠心圧縮機。   A centrifugal compressor having an impeller manufactured by the manufacturing method according to claim 10. 請求項10乃至13のいずれか1項に記載の製造方法により製造された羽根車を有する軸流ポンプ。   An axial flow pump having an impeller manufactured by the manufacturing method according to any one of claims 10 to 13.
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