JPH07332289A - Impeller - Google Patents
ImpellerInfo
- Publication number
- JPH07332289A JPH07332289A JP13010294A JP13010294A JPH07332289A JP H07332289 A JPH07332289 A JP H07332289A JP 13010294 A JP13010294 A JP 13010294A JP 13010294 A JP13010294 A JP 13010294A JP H07332289 A JPH07332289 A JP H07332289A
- Authority
- JP
- Japan
- Prior art keywords
- side plate
- blade
- manufacturing
- main plate
- impeller
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Landscapes
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
(57)【要約】
【構成】ドーナツ形の円板である主板1および、一定の
曲線4を描きつつ主板1の中心部から外周部へ放射状に
取り付けられた、あるいは主板1と一体となった翼2お
よび、主板1と対称位置に間隙を介して翼2に取り付け
られるドーナツ形の円板である側板内輪部3aと側板外
輪部3bで構成されている。
【効果】機械加工工数を低減することができる。また、
分割した側板の合わせ部を連続溶接化することができる
ため、品質が向上し、かつ工数も低減することができ
る。
(57) [Summary] [Structure] Main plate 1 which is a donut-shaped disc and radially attached from the central portion to the outer peripheral portion of main plate 1 while drawing a constant curve 4 or integrated with main plate 1. It is composed of a blade 2 and a side plate inner ring portion 3a and a side plate outer ring portion 3b which are doughnut-shaped disks attached to the blade 2 at positions symmetrical to the main plate 1 with a gap. [Effect] The number of machining steps can be reduced. Also,
Since the joined portions of the divided side plates can be continuously welded, the quality can be improved and the number of steps can be reduced.
Description
【0001】[0001]
【産業上の利用分野】本発明は、回転機械の回転体であ
るロータに1枚あるいは、複数枚取り付けられる羽根車
に係り、特に、主板と側板の間隙に一定の曲線を描きつ
つ軸中心から外周部へ放射状に複数枚配置された翼の曲
率が大きい場合の羽根車において、その製作方法に好適
な回転機械に関する。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an impeller attached to a rotor, which is a rotating body of a rotary machine, or a plurality of impellers, and particularly, to draw a constant curve in a gap between a main plate and a side plate from an axial center. The present invention relates to a rotary machine suitable for a manufacturing method of an impeller in which a plurality of blades radially arranged on an outer peripheral portion have a large curvature.
【0002】[0002]
【従来の技術】この種の羽根車に関する形状および、製
作方法の一般的な従来技術を、図3,図4,図5およ
び、図6により説明する。2. Description of the Related Art A general prior art of a shape and a manufacturing method for an impeller of this type will be described with reference to FIGS. 3, 4, 5 and 6.
【0003】図3は、従来技術羽根車の説明図である。
ドーナツ形の円板である主板1および、一定の曲線4を
描きつつ主板1の中心部から外周部へ放射状に複数枚取
り付けられる、あるいは主板1と一体となった翼2およ
び、主板1と対称位置に間隙を介して翼2に取り付けら
れるドーナツ形の円板である側板3で構成されている。FIG. 3 is an illustration of a prior art impeller.
Main plate 1 which is a donut-shaped disc, and a plurality of blades 2 which are attached radially from the central portion of the main plate 1 to the outer peripheral portion while drawing a constant curve 4 or which are integrated with the main plate 1 and the main plate 1 are symmetrical It is composed of a side plate 3 that is a donut-shaped disc that is attached to the wing 2 with a gap at a position.
【0004】図4は、主板1に翼2の付根部を溶接し、
溶着金属5aによって接合される場合の主板1と翼2の
接合部の断面図である。図5は、翼2を主板1の材料か
ら機械加工によって削り出すことによって主板1と翼2
が一体となっている場合の断面図である。In FIG. 4, the root portion of the blade 2 is welded to the main plate 1,
FIG. 7 is a cross-sectional view of a joint portion between the main plate 1 and the blade 2 when they are joined by the weld metal 5a. FIG. 5 shows that the blade 2 is machined from the material of the blade 1 to form the blade 1 and the blade 2.
FIG. 4 is a cross-sectional view of the case in which is integrated.
【0005】図6は、図3の羽根車を製作する際の従来
技術を示す斜視図である。FIG. 6 is a perspective view showing a conventional technique for manufacturing the impeller of FIG.
【0006】従来技術では、図4,図5に示した構造の
主板1,翼2に側板3を組み合わせて、翼2と側板3と
の接合部付根を溶接による溶着金属5bによって接合し
ていた。この製作方法は、羽根車を製作する際に一般的
に用いられる方法である。この種の製作方法の類似した
公知例には、特開昭52−14906 号,特開昭51−73607号
公報がある。以下、上記製作方法を製作方法Aと称す
る。In the prior art, the main plate 1 and the blade 2 having the structure shown in FIGS. 4 and 5 are combined with the side plate 3, and the root of the joint between the blade 2 and the side plate 3 is joined by the weld metal 5b by welding. . This manufacturing method is a method generally used when manufacturing an impeller. Similar known examples of this type of manufacturing method are disclosed in JP-A-52-14906 and JP-A-51-73607. Hereinafter, the above manufacturing method is referred to as a manufacturing method A.
【0007】図3に示した羽根車を製作する方法とし
て、製作方法A以外に関連する公知例は、特開昭54−97
547 号公報がある。この公知例を図7により説明する。As a method for manufacturing the impeller shown in FIG. 3, other than the manufacturing method A, a known example is disclosed in JP-A-54-97.
There is 547 publication. This known example will be described with reference to FIG.
【0008】機械加工即ち切削によって得られる溝6を
施した主板1または側板3を介し、羽根車の外側から翼
2の溶接を行い主板1または側板3を翼2を固着する第
一のパスにおいて、被覆溶接材料なしのタングステン電
極7をイナートガス8の被包のもとで使用し(ティグ溶
接)、翼2に対し角をシームするに必要な過剰材料9
を、形成された溝6の底壁により主板1または側板3を
介して供給し、溝6は主板1または側板3の全壁厚を通
り抜けない閉止スロットと呼ばれるものとし、この閉止
スロットの次の充填パスでは同じティグ溶接で溶加材を
使用し、第一のパスおよび次の充填パスで使用されるテ
ィグ法を電流,電圧,溶接速度およびタングステン電極
7の位置が閉止スロット全長に沿って一定に保たれるよ
う自動化したことを特徴とする回転機械の主板1および
側板3の翼2をアーク溶接する方法である。また、この
種の製作方法に類似した公知例には、特開昭61−262465
号,特開昭62−28071 号,特開昭62−107866号,特開昭
62−46191 号,特開昭62−187569号,特開昭55−40201
号,特開昭55−64193 号,特開昭47−19442 号,特開昭
48−45448 号,特開昭48−88039 号,特開昭49−65951
号,特開昭64−48682号,特開昭55−22471 号,特開平2
−121796 号特開昭63−26285 号,特開昭63−26286
号,特開昭63−203286号公報がある。上記公知例はティ
グ溶接以外に、アーク溶接,電子ビーム溶接,エレクト
ロスラグ溶接,ろう付け等を応用したものがあるが、基
本的な製作方法案はどの例も類似していると考えられ
る。以下これらの製作方法をまとめて製作方法Bと称す
る。In the first pass, in which the blade 2 is fixed to the main plate 1 or the side plate 3 by welding the blade 2 from the outside of the impeller through the main plate 1 or the side plate 3 having the groove 6 obtained by machining or cutting. Using the tungsten electrode 7 without coating welding material under encapsulation of the inert gas 8 (Tig welding), excess material 9 needed to seam the corner to the blade 2
Is supplied by the bottom wall of the formed groove 6 through the main plate 1 or the side plate 3, and the groove 6 is referred to as a closed slot that does not pass through the entire wall thickness of the main plate 1 or the side plate 3. In the filling pass, the filler metal is used in the same TIG welding, and the TIG method used in the first pass and the next filling pass is used to make the current, voltage, welding speed and position of the tungsten electrode 7 constant along the entire length of the closed slot. It is a method for arc welding the main plate 1 and the blades 2 of the side plates 3 of a rotary machine, which is characterized by being automated so that A known example similar to this type of manufacturing method is disclosed in JP-A-61-262465.
JP-A-62-28071, JP-A-62-107866, JP-A-SHO
62-46191, JP-A-62-187569, JP-A-55-40201
No. 5, JP-A-55-64193, JP-A-47-19442, JP-A-SHO
48-45448, JP-A-48-88039, JP-A-49-65951
JP-A 64-48682, JP-A 55-22471, JP-A 2
-121796, JP-A-63-26285, JP-A-63-26286
And JP-A-63-203286. The above-mentioned known examples include arc welding, electron beam welding, electroslag welding, brazing, etc. in addition to TIG welding, but it is considered that the basic manufacturing method plans are similar to each other. Hereinafter, these manufacturing methods are collectively referred to as a manufacturing method B.
【0009】その他、図3に示した羽根車を製作する方
法として製作方法Aおよび製作方法B以外に関連する公
知例は、特開昭55−78196 号公報がある。この公知例を
図8により説明する。主板,側板を対応させてそれぞれ
の翼片数に相応する扇型に分け、その扇型主板材11,
扇型側板材12,翼部13の三部をもって、羽根車を形
成すべき羽根車要素10を組立て、あるいはこのような
形状の羽根車要素10の所要数を成形作成して、この羽
根車要素10を円形に集めてその要素間を溶接する羽根
車の製作方法である。また、この種の製作方法に類似し
た公知例には特開昭54−83106 号公報がある。以下これ
らの製作方法をまとめて製作方法Cと称する。In addition, as a known method other than the manufacturing method A and the manufacturing method B as a method for manufacturing the impeller shown in FIG. 3, there is JP-A-55-78196. This known example will be described with reference to FIG. The main plate and side plates are made to correspond to each other and divided into fan-shaped parts corresponding to the number of wing pieces, and the fan-shaped main plate material 11,
With the three parts of the fan-shaped side plate material 12 and the blade portion 13, the impeller element 10 for forming the impeller is assembled, or the required number of impeller elements 10 having such a shape is formed and formed, and the impeller element is formed. This is a method of manufacturing an impeller in which 10 are collected in a circle and the elements are welded together. A known example similar to this type of manufacturing method is Japanese Patent Laid-Open No. 54-83106. Hereinafter, these manufacturing methods are collectively referred to as a manufacturing method C.
【0010】[0010]
【発明が解決しようとする課題】図6および、それに類
似した公知例における製作方法Aの従来技術では、製作
方法Bおよび製作方法Cに比べ、羽根車の製作方法は単
純でかつ製作工数も少ないが、主板1と側板3との間隙
16が非常に狭い場合や、翼2の曲線4が大きくなった
場合に溶接による接合が困難あるいは不可能となり、さ
らにこの羽根車形状では溶接の自動化も困難であるとい
う問題点があった。In the prior art of the manufacturing method A in FIG. 6 and a known example similar to FIG. 6, the manufacturing method of the impeller is simpler and the manufacturing man-hour is smaller than the manufacturing methods B and C. However, if the gap 16 between the main plate 1 and the side plate 3 is very narrow, or if the curve 4 of the blade 2 becomes large, it becomes difficult or impossible to join them by welding. Furthermore, with this impeller shape, it is also difficult to automate welding. There was a problem that was.
【0011】図7およびそれに類似した公知例における
製作方法Bの従来技術では、主板1と側板3との間隙1
6が非常に狭い場合や、翼2の曲線4が大きくなった場
合にも溶接による接合が可能であり、溶接の自動化も容
易となる。しかしこの従来技術は、主板1あるいは側板
3に溝6を切削によって施す際に切削用エンドミルを溝
形状に合わせた特殊形状にしなければならず、また側板
3と翼2との位置ずれが生じると良好な接合ができなく
なるため、その位置精度をきわめて精度良く切削しなけ
ればならない。従って切削工数に多大な時間を要してい
る。さらに、この製作方法Bは溝6を集中的に溶接によ
って主板1の一部を形成しなければならないため、溶接
による歪、および、各溝の溶着金属量のばらつきによっ
て回転体である羽根車の動バランスが乱れやすくなる等
の問題があった。In the prior art of the manufacturing method B in FIG. 7 and a known example similar thereto, in the gap 1 between the main plate 1 and the side plate 3.
Even when 6 is very narrow, or when the curve 4 of the blade 2 is large, welding can be performed and the welding can be automated easily. However, according to this conventional technique, when the groove 6 is formed in the main plate 1 or the side plate 3 by cutting, the cutting end mill has to have a special shape in accordance with the groove shape, and when the side plate 3 and the blade 2 are displaced from each other, a positional deviation occurs. Since good joining cannot be achieved, the positional accuracy must be cut with extremely high accuracy. Therefore, a lot of time is required for cutting man-hours. Furthermore, in this manufacturing method B, since the groove 6 must be intensively welded to form a part of the main plate 1, distortion of the welding and variations in the amount of deposited metal in each groove cause the impeller, which is a rotor, to rotate. There was a problem that the dynamic balance was easily disturbed.
【0012】図8および、それに類似した公知例におけ
る製作方法Cの従来技術では、製作方法Aの問題点を解
決することが可能であるが製作方法Bと同様に羽根車の
動バランスが乱れやすくなる問題点がある。さらに、製
作方法Cは、翼部13の数量分羽根車要素10を製作し
それぞれの羽根車要素10を円形に集めてその要素間を
溶接する構造であるため、翼の数が多くなるほど溶接す
る主板接合部14,側板接合部15の数も多くなってく
る。また、翼部13の曲線4が大きくなると羽根車要素
10の主板材接合部14,側板材接合部15の接合面を
直線加工することができなくなり、羽根車要素10の製
作に多大な時間を要する。8 and the related art of the manufacturing method C in a known example similar to that can solve the problem of the manufacturing method A, but like the manufacturing method B, the dynamic balance of the impeller is easily disturbed. There is a problem that becomes. Furthermore, since the manufacturing method C is a structure in which the number of blade portions 13 is the number of the impeller elements 10, the impeller elements 10 are collected in a circular shape, and the elements are welded together, welding is performed as the number of blades increases. The number of main plate joints 14 and side plate joints 15 also increases. Further, when the curved line 4 of the blade portion 13 becomes large, it becomes impossible to perform straight-line processing on the joint surfaces of the main plate material joint portion 14 and the side plate material joint portion 15 of the impeller element 10, and it takes a lot of time to manufacture the impeller element 10. It costs.
【0013】[0013]
【課題を解決するための手段】以上のような問題点を解
決するには、羽根車の製作時間を低減できるように極力
自動化できる構造とし、かつ製作後の動的バランスが乱
れにくくする必要がある。In order to solve the above problems, it is necessary to have a structure that can be automated as much as possible so as to reduce the manufacturing time of the impeller and to prevent the dynamic balance after manufacturing from being disturbed. is there.
【0014】本発明の請求項1に記載の発明では、主板
と翼の製作は従来技術の製作方法Aおよび、製作方法B
と同様であるが、側板をドーナツ形円板状に内輪部と外
輪部に分割した形状とし、特殊な機械加工を要すること
なく製作できるようにした。According to the first aspect of the present invention, the main plate and the blade are manufactured by the conventional manufacturing method A and manufacturing method B.
Same as the above, but the side plate has a donut-shaped disc shape divided into an inner ring part and an outer ring part so that it can be manufactured without special machining.
【0015】本発明の請求項2に記載の発明では、請求
項1に記載の主板および翼の部片と、側板内輪部とを製
作方法Aと同様に翼付根部を溶接することによって接合
できるようにし、かつ側板外輪部と側板内輪部との接合
部を羽根車の外側から溶接できるようにした。In the invention described in claim 2 of the present invention, the main plate and the blade piece described in claim 1 and the side plate inner ring portion can be joined by welding the blade root as in the manufacturing method A. In addition, the joint between the outer ring portion of the side plate and the inner ring portion of the side plate can be welded from the outside of the impeller.
【0016】本発明の請求項3に記載の発明では、請求
項1に記載の側板内輪部と外輪部のそれぞれを、さらに
ドーナツ形円板状に複数分割した形状であり、特殊な機
械加工を要することなく製作できるようにした。According to a third aspect of the present invention, each of the side plate inner ring portion and the outer ring portion of the first aspect is further divided into a donut-shaped disc shape, and special machining is performed. I made it possible to produce without needing.
【0017】本発明の請求項4に記載の発明では、請求
項1,2,3に記載の羽根車において側板内輪部と外輪
部あるいは、複数分割した側板内輪部および外輪部の接
合部に、特殊な機械加工を要することなくインロー部を
加工すると同時に、この接合部を羽根車の外側よりの溶
接が可能となる溶接開先加工を施すことができる。According to a fourth aspect of the present invention, in the impeller of the first, second, and third aspects, the side plate inner ring portion and the outer ring portion, or a plurality of divided side plate inner ring portions and outer ring portions are joined, The spigot portion can be processed without requiring special machining, and at the same time, the weld groove can be processed so that the joint portion can be welded from the outside of the impeller.
【0018】請求項5に記載の発明では主板と翼の接合
部である翼付根部および、請求項4に記載の側板内輪部
と外輪部の接合部あるいは、複数枚に分割した側板内輪
部と外輪部の接合部に自動溶接装置あるいは、電子ビー
ム溶接法等を適用できる構造とし、接合溶接の自動化を
図る。In a fifth aspect of the present invention, there is provided a blade root portion which is a joint portion between the main plate and the blade, and a joint portion between the side plate inner ring portion and the outer ring portion according to claim 4, or a side plate inner ring portion which is divided into a plurality of sheets. The welding of the outer ring will be automated by applying an automatic welding device or an electron beam welding method.
【0019】[0019]
【作用】本発明の請求項1に記載の発明では、側板をド
ーナツ形円板状に内輪部と外輪部に分割したことによっ
て、従来技術の製作方法Bのような特殊な機械加工が不
要となるため、製作工数が低減できる。In the invention according to claim 1 of the present invention, the side plate is divided into an inner ring part and an outer ring part in the shape of a donut-shaped disc, so that special machining such as the manufacturing method B of the prior art is unnecessary. Therefore, the number of manufacturing steps can be reduced.
【0020】請求項2に記載の発明では、側板を内輪部
と外輪部に分割したことによって、翼の曲率が大きくな
った場合や、羽根出口幅が狭くなった場合でも、従来技
術の製作方法Aに記載の翼と側板の溶接接合法が適用可
能となり、溶接工数が従来技術の製作方法Bおよび、製
作方法Cに比べて低減することができ、さらに側板内輪
部と外輪部の接合部を羽根車の外側から、羽根車の周方
向に溶接する構造であるため羽根車製作後の動的バラン
スが乱れにくくなる。According to the second aspect of the present invention, by dividing the side plate into the inner ring portion and the outer ring portion, even if the curvature of the blade becomes large or the blade outlet width becomes narrow, the manufacturing method of the prior art. The welding joining method of the blade and the side plate described in A can be applied, the welding man-hour can be reduced as compared with the manufacturing method B and the manufacturing method C of the prior art, and further, the joint portion of the side plate inner ring portion and the outer ring portion can be Since the structure is such that the impeller is welded in the circumferential direction from the outside, the dynamic balance after manufacturing the impeller is less likely to be disturbed.
【0021】請求項3に記載の発明では、請求項1に記
載の側板内輪部と外輪部の2分割において、翼の曲率が
さらに大きくなった場合や、羽根車の主板と側板との間
隙が狭くなった場合等の理由により、従来技術の製作方
法Aに記載の翼との側板の溶接が困難となる場合でも、
側板内輪部と外輪部をさらにドーナツ形円板状に複数分
割することによって、その溶接が可能となる。According to the third aspect of the invention, when the inner ring portion and the outer ring portion of the side plate according to the first aspect are divided into two parts, the curvature of the blade is further increased, or the gap between the main plate and the side plate of the impeller is increased. Even if it becomes difficult to weld the side plate to the blade described in the manufacturing method A of the prior art due to a reason such as narrowing,
The inner ring portion and the outer ring portion of the side plate can be welded by further dividing into a donut-shaped disc shape.
【0022】請求項4に記載の発明では、ドーナツ形円
板状に分割した側板を組み合わせる際に、その組合わせ
接合部にインロー加工を施しておくことによって組合わ
せ作業を精度良くかつ、迅速に行うことができる。ま
た、インロー加工と同時に溶接開先加工が従来技術の製
作方法Bのような特殊加工を要することなく可能とな
り、製作工数を低減することができる。According to the fourth aspect of the present invention, when the side plates divided into the donut-shaped disc shape are assembled, the combination work is performed with a spigot, so that the combination work can be performed accurately and quickly. It can be carried out. Further, the welding groove working can be performed simultaneously with the inlay working without requiring special working as in the manufacturing method B of the prior art, and the number of manufacturing steps can be reduced.
【0023】請求項5に記載の発明では、接合部の溶接
を自動化することによって、溶接工数を低減する。In the invention described in claim 5, the welding man-hour is reduced by automating the welding of the joint portion.
【0024】[0024]
【実施例】本発明の一実施例を図1,図2を用いて説明
する。図1は、本発明を適用した回転機械用羽根車の概
要を示したものである。ドーナツ形の円板である主板1
および、一定の曲線4を描きつつ主板1の中心部から外
周部へ放射状に複数枚取り付けられる、あるいは主板1
と一体となった翼2および、主板1と対称位置に間隙を
介して翼2に取り付けられるドーナツ形の円板である側
板内輪部3aで構成されている。DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS An embodiment of the present invention will be described with reference to FIGS. FIG. 1 shows an outline of an impeller for a rotary machine to which the present invention is applied. Main plate 1 which is a donut-shaped disc
A plurality of main plates 1 are attached radially from the central portion to the outer peripheral portion while drawing a constant curve 4, or the main plate 1
And a side plate inner ring portion 3a which is a donut-shaped disc attached to the blade 2 at a position symmetrical to the main plate 1 with a gap therebetween.
【0025】羽根車の製作方法は次のようである。主板
1に複数枚の翼2を配置した後、翼2の付根部を溶接に
よって接合する。あるいは、主板1の材料の状態から機
械加工によって翼2を削り出す。また、この製作作業と
は別に、機械加工によって側板内輪部3aおよび、側板
外輪部3bの接合部となる部分にインロー加工部7、お
よび溶接開先加工部18を施工する。The method of manufacturing the impeller is as follows. After arranging a plurality of blades 2 on the main plate 1, the roots of the blades 2 are joined by welding. Alternatively, the blade 2 is machined from the material state of the main plate 1 by machining. Separately from this manufacturing work, the spigot processing part 7 and the welding groove processing part 18 are applied to the part which becomes the joint part of the side plate inner ring part 3a and the side plate outer ring part 3b by machining.
【0026】主板1と翼2を溶接によって接合した部
材、あるいは主板1の材料の状態から翼2を削り出した
部材に、側板内輪部3aの主板1の対称位置に取り付け
る。取り付け後、翼2との合わせ部、即ち、翼2の付根
部を溶接によって接合する。接合後、側板外輪部3bを
側板内輪部3aのインローに合わせて取り付け、翼2と
の合わせ部を溶接する。最後に側板内輪部3aと側板外
輪部3bとの合わせ部に形成された溶接開先18を溶接
によって接合する。主板1と翼2の溶接および、側板内
輪部3aと側板外輪部3bの溶接は羽根車の外側より溶
接可能であるため自動溶接が可能となる。また、特に側
板内輪部3aと側板内輪部3bの接合部の溶接は電子ビ
ーム溶接法を適用することも可能である。A member obtained by joining the main plate 1 and the blade 2 by welding, or a member obtained by cutting the blade 2 from the material state of the main plate 1 is attached to the side plate inner ring portion 3a at a symmetrical position of the main plate 1. After the attachment, the joint with the blade 2, that is, the root of the blade 2 is joined by welding. After the joining, the side plate outer ring portion 3b is attached according to the spigot of the side plate inner ring portion 3a, and the joining portion with the blade 2 is welded. Finally, the welding groove 18 formed at the joint between the side plate inner ring portion 3a and the side plate outer ring portion 3b is joined by welding. Since the main plate 1 and the blade 2 can be welded and the side plate inner ring portion 3a and the side plate outer ring portion 3b can be welded from the outside of the impeller, automatic welding can be performed. Further, in particular, the welding of the joint between the side plate inner ring portion 3a and the side plate inner ring portion 3b can be performed by applying the electron beam welding method.
【0027】図2は、図1に記載の側板内輪部3aと側
板外輪部3bをさらに分割した状態の側板の説明図であ
る。側板は側板内輪部3aと側板外輪部3bとの2分割
に限らず、図2に示すように4分割あるいは、さらに複
数分割して製作しても良い。この際分割した側板の合わ
せ部は、図1に記載のインロー加工と溶接開先加工を施
しておく。FIG. 2 is an explanatory view of the side plate in a state where the side plate inner ring portion 3a and the side plate outer ring portion 3b shown in FIG. 1 are further divided. The side plate is not limited to being divided into the side plate inner ring portion 3a and the side plate outer ring portion 3b, but may be divided into four as shown in FIG. At this time, the joint portion of the divided side plates is subjected to the spigot processing and the welding groove processing shown in FIG.
【0028】[0028]
【発明の効果】本発明によれば、従来の公知例であるス
ロット溶接法に比べて溝加工をインロー加工することに
よって、機械加工工数を低減することができる。また、
分割した側板の合わせ部を連続自動溶接化することがで
きるため、品質が向上し、工数も低減する。さらに、回
転体である羽根車の側板をドーナツ形円板状に分割する
ことにより、製作後の動的バランスが乱れにくい。特に
放射状に分割加工する従来公知技術と比べるときわだっ
た効果がある。さらに、翼と側板の接合後の仕上げ加工
についても接合部を治工具がとどく範囲に設けることが
できるため仕上作業,仕上効果が良好となる。According to the present invention, the number of machining steps can be reduced by spigot-grooving the groove as compared with the conventionally known slot welding method. Also,
Since the joined parts of the divided side plates can be continuously and automatically welded, the quality is improved and the man-hours are reduced. Furthermore, by dividing the side plate of the impeller, which is a rotating body, into a donut-shaped disc shape, the dynamic balance after manufacturing is less likely to be disturbed. In particular, it has a remarkable effect when compared with the conventionally known technique of radially dividing. Further, in the finishing process after joining the blade and the side plate, the joining portion can be provided within the range where the jig and tool reach, and the finishing work and the finishing effect are improved.
【図1】本発明の一実施例を示す羽根車の説明図。FIG. 1 is an explanatory view of an impeller showing an embodiment of the present invention.
【図2】図1の実施例の側板内輪部と側板外輪部をさら
に4分割した側板の説明図。FIG. 2 is an explanatory view of a side plate obtained by further dividing the side plate inner ring portion and the side plate outer ring portion of the embodiment of FIG. 1 into four parts.
【図3】従来の羽根車の構造の説明図。FIG. 3 is an explanatory view of a structure of a conventional impeller.
【図4】図3の従来羽根車の主板と翼を溶接によって接
合した場合の接合部の断面図。FIG. 4 is a cross-sectional view of a joint portion when the main plate and the blade of the conventional impeller of FIG. 3 are joined by welding.
【図5】図3の従来羽根車の翼を主板の材料から機械加
工によって削り出した後の、主板と翼が一体となった場
合の断面図。FIG. 5 is a cross-sectional view of a case where the main plate and the blade are integrated after the blade of the conventional impeller of FIG. 3 is machined from the material of the main plate by machining.
【図6】図3の従来羽根車を製作する際の、翼と側板を
溶接する従来技術を示す斜視図。FIG. 6 is a perspective view showing a conventional technique for welding a blade and a side plate when manufacturing the conventional impeller of FIG.
【図7】従来公知例の実施例の説明図。FIG. 7 is an explanatory diagram of an example of a conventionally known example.
【図8】従来公知例の実施例の説明図。FIG. 8 is an explanatory diagram of an example of a conventionally known example.
1…主板、2…翼、3a…側板内輪部、3b…側板外輪
部、4…曲線、5c…側板内輪部と側板外輪部の接合部
の溶着金属、17…インロー加工部、18…溶接開先加
工部。DESCRIPTION OF SYMBOLS 1 ... Main plate, 2 ... Wing, 3a ... Side plate inner ring part, 3b ... Side plate outer ring part, 4 ... Curve, 5c ... Weld metal of joint part of side plate inner ring part and side plate outer ring part, 17 ... Inlay processing part, 18 ... Welding opening Pre-processing section.
Claims (1)
の曲線を描きつつ前記主板の中心部から外周部へ放射状
に複数枚取付けられる、あるいは前記主板と一体となっ
た翼および、前記主板と対象位置に間隙を介して前記翼
に取り付けられる前記ドーナツ形の円板である側板で構
成される羽根車において、前記側板を前記ドーナツ形の
円板状に内輪部と外輪部に分割した形状にしたことを特
徴とする羽根車。1. A main plate which is a donut-shaped disc, and a plurality of blades which are radially attached from a central portion of the main plate to an outer peripheral portion while drawing a constant curve or which are integral with the main plate, and the main plate. And a side plate that is a donut-shaped disc that is attached to the blade via a gap at a target position, in which the side plate is divided into an inner ring portion and an outer ring portion into the donut-shaped disc shape. An impeller that is characterized by
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP13010294A JPH07332289A (en) | 1994-06-13 | 1994-06-13 | Impeller |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP13010294A JPH07332289A (en) | 1994-06-13 | 1994-06-13 | Impeller |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH07332289A true JPH07332289A (en) | 1995-12-22 |
Family
ID=15026000
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP13010294A Pending JPH07332289A (en) | 1994-06-13 | 1994-06-13 | Impeller |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH07332289A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112917110A (en) * | 2021-02-25 | 2021-06-08 | 南京中科神光科技有限公司 | Large-scale narrow flow passage closed impeller, manufacturing method and special welding equipment for blades |
-
1994
- 1994-06-13 JP JP13010294A patent/JPH07332289A/en active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112917110A (en) * | 2021-02-25 | 2021-06-08 | 南京中科神光科技有限公司 | Large-scale narrow flow passage closed impeller, manufacturing method and special welding equipment for blades |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US6095402A (en) | Method for the manufacture or repair of a blisk by linear friction welding | |
| US12090569B2 (en) | Method of manufacturing a component of a rotary machine and component manufactured using said method | |
| US7189064B2 (en) | Friction stir welded hollow airfoils and method therefor | |
| JP4155646B2 (en) | Method for joining a base of an airfoil and a disk and an assembly formed by this method | |
| JP4353981B2 (en) | Method of joining a blade to a blade root or rotor disk when manufacturing or repairing a gas turbine blade or blade-integrated gas turbine rotor | |
| US6969826B2 (en) | Welding process | |
| US7997860B2 (en) | Welded nozzle assembly for a steam turbine and related assembly fixtures | |
| US4985992A (en) | Method of making stator stages for compressors and turbines, and stator vanes and vane arrays produced thereby | |
| EP1808577B1 (en) | A welded nozzle assembly for a steam turbine | |
| US8702385B2 (en) | Welded nozzle assembly for a steam turbine and assembly fixtures | |
| EP1132166A1 (en) | A stator vane assembly for a turbine and methods for forming the assembly | |
| JP2004308647A (en) | Method of manufacturing impeller and impeller | |
| JP4648946B2 (en) | Component repair method and component manufacturing method | |
| JP4436661B2 (en) | Method for manufacturing a steam turbine nozzle box assembly | |
| JPS637873B2 (en) | ||
| GB2132512A (en) | Welded stator vane assemblies for turbomachines | |
| US8097831B2 (en) | Use of an activating flux for the TIG welding of metal parts | |
| JPH07332289A (en) | Impeller | |
| US6519849B2 (en) | Method for the manufacture of a welded rotor of a fluid-flow machine | |
| JPS6326285A (en) | Impeller welding assembly method | |
| CN119288722A (en) | Improvements involving the manufacture of water turbines | |
| JPS6330186A (en) | Electron beam welding method for rotor | |
| JP2006029198A (en) | Assembling the runner of a Francis hydraulic machine | |
| JPH0676763B2 (en) | Turbine vane stopper welding method | |
| JPS60216004A (en) | Turbine nozzle diaphragm |