JPH048630B2 - - Google Patents

Info

Publication number
JPH048630B2
JPH048630B2 JP57163872A JP16387282A JPH048630B2 JP H048630 B2 JPH048630 B2 JP H048630B2 JP 57163872 A JP57163872 A JP 57163872A JP 16387282 A JP16387282 A JP 16387282A JP H048630 B2 JPH048630 B2 JP H048630B2
Authority
JP
Japan
Prior art keywords
blade
welding
piece
impeller
welded
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.)
Expired - Lifetime
Application number
JP57163872A
Other languages
Japanese (ja)
Other versions
JPS5954776A (en
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed filed Critical
Priority to JP57163872A priority Critical patent/JPS5954776A/en
Publication of JPS5954776A publication Critical patent/JPS5954776A/en
Publication of JPH048630B2 publication Critical patent/JPH048630B2/ja
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03BMACHINES OR ENGINES FOR LIQUIDS
    • F03B3/00Machines or engines of reaction type; Parts or details peculiar thereto
    • F03B3/12Blades; Blade-carrying rotors
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Hydraulic Turbines (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Description

【発明の詳細な説明】 〔産業上の利用分野〕 本発明はコンプレツサ,ブロワ,フアン,ポン
プなどのターボ流体機械の主要部品の一つである
羽根車の製法に係るもので、更に詳しくは溶接羽
根車の製法に関するものである。
[Detailed Description of the Invention] [Field of Industrial Application] The present invention relates to a method for manufacturing an impeller, which is one of the main parts of turbo fluid machines such as compressors, blowers, fans, and pumps. This relates to the manufacturing method of impellers.

〔従来の技術〕[Conventional technology]

羽根車の構造を第1図に示す。第1図の−
線矢視図を第2図に示す。羽根車の製法には、溶
接,鋳造,放電加工などの方法があるが、鋳造は
型の製作費が高い上に、鋳物欠陥が避けられない
ため、強度上の制限がある。また、放電加工は加
工時間が非常に長い上に、電極の移動方向に制限
があるため、羽根車の流路形状に制限を受ける。
このため、流路形状に制限を受けず製作費も比較
的安価な溶接による羽根車の製法が広く採用され
ている。
The structure of the impeller is shown in Figure 1. Figure 1 -
A line arrow view is shown in Fig. 2. Impellers can be manufactured using methods such as welding, casting, and electrical discharge machining, but casting has limitations in terms of strength because the manufacturing cost of the mold is high and casting defects are inevitable. In addition, electric discharge machining requires a very long machining time and there are restrictions on the direction of movement of the electrode, so there are restrictions on the shape of the flow path of the impeller.
For this reason, impeller manufacturing methods by welding, which are not limited by the flow path shape and are relatively inexpensive to manufacture, have been widely adopted.

従来の溶接羽根車の構造を第1図,第2図によ
り説明する。心板1、側板2、羽根3はそれぞ
れ、心板1と羽根3同志、あるいは側板2と羽根
3同志で溶接接合されて一体構造に構成されてい
る。第2図に溶接ビードの状況を示す。溶接作
業,溶接ビード4の仕上作業は羽根3入口先端を
除いて、羽根3出口から溶接棒あるいはカツター
を挿入して行なわれる。一点鎖線で示すX,Yは
溶接棒あるいはカツターの挿入状態を示す。第2
図に示す羽根の出口角度βは、羽根車の流体性能
に影響を及ぼす因子の一つで、従来の溶接羽根車
ではβの値は比較的大きく、図に示すように溶接
棒は羽根の入口先端部まで楽に届き、溶接作業お
よびビード仕上作業に支障はなかつた。なお、こ
の図において、5は羽根入口、6は羽根出口であ
る。
The structure of a conventional welded impeller will be explained with reference to FIGS. 1 and 2. The core plate 1, the side plates 2, and the blades 3 are each formed into an integral structure by welding the core plate 1 and the blades 3 together, or the side plates 2 and the blades 3 together. Figure 2 shows the condition of the weld bead. The welding work and the finishing work of the weld bead 4 are performed by inserting a welding rod or a cutter from the exit of the blade 3, except for the tip of the entrance of the blade 3. X and Y indicated by dashed dotted lines indicate the inserted state of the welding rod or cutter. Second
The exit angle β of the blade shown in the figure is one of the factors that affects the fluid performance of the impeller. In the conventional welded impeller, the value of β is relatively large, and the welding rod is at the entrance of the blade as shown in the figure. It was easy to reach the tip and there was no problem with welding and bead finishing work. In this figure, 5 is a blade inlet, and 6 is a blade outlet.

〔発明が解決しようとする課題〕[Problem to be solved by the invention]

一方、少ない流量を取扱う羽根車としては、出
口角度βの値を小さくする方が流体性能が向上す
ることが知られていたが、この場合の羽根車の断
面形状では第3図に示すようにαが小さくなつた
ために同一外径の羽根車とした場合羽根の長さが
長くなる。このため、溶接で羽根車を製作しよう
とすると、溶接棒の位置は、X,Yの位置となる
から、図に示すように羽根の入口側A〜B間が死
角となり、溶接作業,ビード仕上作業ができな
い。従つて、従来の溶接による製法では、出口角
度βの小さい羽根車の製作はできなかつた。
On the other hand, it has been known that for an impeller that handles a small flow rate, the fluid performance is improved by decreasing the value of the outlet angle β, but in this case, the cross-sectional shape of the impeller is as shown in Figure 3. Since α becomes smaller, the length of the blade becomes longer when the impeller has the same outer diameter. For this reason, when trying to manufacture an impeller by welding, the welding rods are placed in the X and Y positions, so the area between A and B on the inlet side of the blade becomes a blind spot as shown in the figure, and the welding work and bead finishing are difficult. I can't work. Therefore, it has not been possible to manufacture an impeller with a small exit angle β using the conventional welding method.

本発明の目的は、羽根の出口角度が小さく、少
ない流量を取扱う羽根車であつても羽根車の流路
形状に制限を受けずに高い流体性能の得られる溶
接羽根車の製法を得ることにある。
An object of the present invention is to obtain a manufacturing method of a welded impeller that can obtain high fluid performance without being restricted by the flow path shape of the impeller even if the impeller has a small exit angle of the blades and handles a small flow rate. be.

〔課題を解決するための手段〕[Means to solve the problem]

上記目的を達成するため本発明は、心板,側板
および羽根を溶接により一体に構成して製作され
る羽根車において、前記側板を径方向に少なくと
も2以上の同心円体状に分割された側板片に製作
すると共に、前記羽根も長手方向に少なくとも2
以上に分割された羽根片に製作し、先ず、心板に
内径側の羽根片を溶接した後、該内径側羽根片に
内径側の側板片を溶接し、次に外径側の羽根片を
前記心板及び前記内径側羽根片に溶接し、最後に
外径側の側板片を前記内径側側板片及び外径側羽
根片に溶接することを特徴とするものである。
To achieve the above object, the present invention provides an impeller manufactured by integrally constructing a core plate, a side plate, and a blade by welding, in which the side plate is divided into at least two concentric circular pieces in the radial direction. At the same time, the blades also have at least two holes in the longitudinal direction.
The blade pieces divided into the above are manufactured. First, the inner diameter side blade piece is welded to the core plate, the inner diameter side side plate piece is welded to the inner diameter side blade piece, and then the outer diameter side blade piece is welded to the inner diameter side blade piece. The core plate and the inner blade piece are welded, and finally the outer side plate piece is welded to the inner diameter side plate piece and the outer diameter side blade piece.

〔作用〕[Effect]

本発明によれば、上記構成としたことにより、
羽根車の溶接作業時に、溶接棒の死角となる部分
をなくすことができるので、小出口角度で羽根長
さの長い羽根車を製作する場合であつても溶接作
業やビード仕上作業を容易に行うことが可能とな
る。
According to the present invention, by having the above configuration,
When welding an impeller, it is possible to eliminate the blind spot of the welding rod, so welding and bead finishing work can be easily performed even when manufacturing an impeller with a small exit angle and a long blade length. becomes possible.

〔実施例〕〔Example〕

従来の製法では小出口角度、すなわち羽根長さ
の長い羽根車を溶接により製作する場合、羽根入
口側に溶接作業およびビード仕上作業の死角がで
きるために溶接が不可能であつた。本発明では、
この死角を無くすために、羽根および側板あるい
は心板を分割し、各片を順次溶接により接合して
羽根車を製作するようにしたものである。
In conventional manufacturing methods, when manufacturing an impeller with a small exit angle, that is, a long blade length, by welding, welding is impossible because a blind spot is created on the blade inlet side for welding work and bead finishing work. In the present invention,
In order to eliminate this blind spot, the impeller is manufactured by dividing the blades and side plates or core plate, and sequentially joining each piece by welding.

以下、本発明の具体的一実施例を第4図〜第7
図により説明する。この実施例は、側板および羽
根を二分割した場合の製法を示すものである。
A specific embodiment of the present invention will be described below in Figures 4 to 7.
This will be explained using figures. This example shows a manufacturing method in which the side plate and the blade are divided into two parts.

羽根入口5と出口6の中間付近で側板2を内径
側側板片2aと外径側側板片2bとに二分割し、
また羽根3を内径側羽根片3aと外径側羽根片3
bとに二分割する。
The side plate 2 is divided into two parts near the middle between the blade inlet 5 and the outlet 6 into an inner diameter side plate piece 2a and an outer diameter side plate piece 2b,
In addition, the blade 3 is connected to the inner diameter side blade piece 3a and the outer diameter side blade piece 3.
Divide into two parts.

製作手順は先ず第4図に示すように心板1に羽
根3aを溶接し、次にこの羽根片3aに側板片2
aを溶接する。第4図の−線矢視図を第5図
に示す。この状態では羽根3の長さは全長の半分
程度であるので溶接棒の位置は一点鎖線で示す
X,Yの位置になり羽根入口5側の先端まで溶接
可能である。この状態で溶接した後に溶接ビード
4の仕上および非破壊検査を実施する。
The manufacturing procedure is to first weld the blade 3a to the core plate 1 as shown in Figure 4, and then attach the side plate piece 2 to this blade piece 3a.
Weld a. FIG. 5 shows a view taken along the - line in FIG. 4. In this state, the length of the blade 3 is about half of the total length, so the welding rod is positioned at the X and Y positions indicated by the dashed line, and welding can be performed up to the tip on the blade inlet 5 side. After welding in this state, the weld bead 4 is finished and non-destructively inspected.

次の製作ステツプを第6図,第7図に示す。先
ず心板1に羽根片3bを溶接すると共に羽根片3
aと羽根片3b同志を溶接する。溶接ビードの仕
方および非破壊検査を実施した後、側板片2aと
側板片2b同志を溶接し、次に羽根片3bと側板
片2bを溶接する。この場合、溶接棒の位置は第
7図に一点鎖線で示すX,Yの位置になるから、
溶接すべき全ての部分が溶接可能となる。次に、
羽根片3bと側板片2b,側板片2aと側板片2
bとの溶接部のビード仕上,非破壊検査を実施す
れば全溶接作業を完了する。
The next manufacturing steps are shown in Figures 6 and 7. First, the blade piece 3b is welded to the core plate 1, and the blade piece 3b is welded to the core plate 1.
A and blade piece 3b are welded together. After welding bead formation and non-destructive testing, the side plate pieces 2a and 2b are welded together, and then the blade pieces 3b and side plate pieces 2b are welded together. In this case, the position of the welding rod is at the X and Y positions shown by the dashed line in Fig. 7, so
All parts to be welded can be welded. next,
Blade piece 3b and side plate piece 2b, side plate piece 2a and side plate piece 2
The entire welding work is completed by finishing the bead of the weld with b and performing a non-destructive inspection.

以上の製作手順をまとめると次のようになる。 The above manufacturing steps are summarized as follows.

心板1と羽根片3aとの溶接 羽根片3aと側板片2aとの溶接 ,溶接部のビード仕上および検査 心板1と羽根片3bとの溶接 羽根片3aと羽根片3bとの溶接 ,溶接部のビード仕上および検査 側板片2aと側板片2bとの溶接 側板片2aと羽根片3bとの溶接 ,溶接部のビード仕上および検査 以上説明したように、本実施例によれば、溶接
作業,ビード仕上作業の死角を作ることなく、完
全に溶接することが可能となり、小出口角度すな
わち羽根長さの長い羽根車も溶接により完全に製
作することが可能となる。
Welding of the core plate 1 and the blade piece 3a Welding of the blade piece 3a and the side plate piece 2a, Bead finishing and inspection of the welded part Welding of the core plate 1 and the blade piece 3b Welding of the blade piece 3a and the blade piece 3b, Welding Welding of the side plate piece 2a and the side plate piece 2b Welding of the side plate piece 2a and the blade piece 3b Bead finishing and inspection of the welded part As explained above, according to this embodiment, welding work, It becomes possible to completely weld without creating a blind spot during bead finishing work, and it is also possible to completely manufacture impellers with small exit angles, that is, long blade lengths, by welding.

したがつて、従来の製作法のように、羽根車の
流路形状に制限を受けたり(放電加工の場合)、
強度上の制限を受けたり(鋳造の場合)すること
がなくなり、安価で流体性能の良好な羽根車を得
ることができる。
Therefore, as with conventional manufacturing methods, there are restrictions on the flow path shape of the impeller (in the case of electric discharge machining),
There are no restrictions on strength (in the case of casting), and an impeller with good fluid performance can be obtained at low cost.

〔発明の効果〕〔Effect of the invention〕

本発明によれば、羽根の出口角度が小さく、少
ない流量を取扱う羽根車であつても、羽根車の流
路形状に制限を受けることなく、完全に溶接によ
り製作することができ、高い流体性能の溶接羽根
車を製作できる効果がある。
According to the present invention, even if the impeller has a small exit angle and handles a small flow rate, it can be manufactured completely by welding without being restricted by the flow path shape of the impeller, and has high fluid performance. This has the effect of making it possible to produce a welded impeller.

【図面の簡単な説明】[Brief explanation of drawings]

第1図および第2図は従来の羽根車の構造およ
び製法を示す図で、第1図は羽根車の縦断面図、
第2図は第1図の−線矢視図、第3図は羽根
出口角度が小さい場合の羽根車の構造を示す図
で、第2図に相当する図、第4図〜第7図は本発
明の溶接羽根車の製法ステツプの一例を説明する
図で、第4図,第6図はその羽根車の縦断面図、
第5図は第4図のV−V線矢視図、第7図は第6
図の−線矢視図である。 1……心板、2……側板、2a,2b……側板
片、3……羽根、3a,3b……羽根片、4……
溶接ビード、5……羽根入口、6……羽根出口。
Figures 1 and 2 are diagrams showing the structure and manufacturing method of a conventional impeller; Figure 1 is a longitudinal cross-sectional view of the impeller;
Figure 2 is a view taken along the - line arrow in Figure 1, Figure 3 is a diagram showing the structure of the impeller when the blade exit angle is small, and Figures 4 to 7 are views corresponding to Figure 2. 4 and 6 are longitudinal cross-sectional views of the impeller;
Fig. 5 is a view taken along the line V-V in Fig. 4, and Fig. 7 is a view taken along the line V-V in Fig. 4.
It is a - line arrow view of a figure. 1... core board, 2... side plate, 2a, 2b... side plate piece, 3... blade, 3a, 3b... blade piece, 4...
Welding bead, 5...blade inlet, 6...blade outlet.

Claims (1)

【特許請求の範囲】[Claims] 1 心板、側板および羽根を溶接により一体に構
成して製作される羽根車において、前記側板を径
方向に少なくとも2以上の同心円体状に分割され
た側板片に製作すると共に、前記羽根も長手方向
に少なくとも2以上に分割された羽根片に製作
し、先ず、心板に内径側の羽根片を溶接した後、
該内径側羽根片に内径側の側板片を溶接し、次に
外径側の羽根片を前記心板及び前記内径側羽根片
に溶接し、最後に外径側の側板片を前記内径側側
板片及び外径側羽根片に溶接することを特徴とす
る溶接羽根車の製法。
1. In an impeller manufactured by integrally constructing a core plate, side plates, and blades by welding, the side plate is manufactured into at least two or more concentric side plate pieces divided in the radial direction, and the blades are also longitudinally divided. The blade piece is divided into at least two parts in the direction, and after welding the inner diameter side blade piece to the core plate,
The inner diameter side plate piece is welded to the inner diameter side blade piece, then the outer diameter side blade piece is welded to the core plate and the inner diameter side blade piece, and finally the outer diameter side side plate piece is welded to the inner diameter side side plate. A method for manufacturing a welded impeller, characterized by welding to the blade pieces and the outer diameter side blade pieces.
JP57163872A 1982-09-22 1982-09-22 Manufacturing method of welded impeller Granted JPS5954776A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP57163872A JPS5954776A (en) 1982-09-22 1982-09-22 Manufacturing method of welded impeller

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP57163872A JPS5954776A (en) 1982-09-22 1982-09-22 Manufacturing method of welded impeller

Publications (2)

Publication Number Publication Date
JPS5954776A JPS5954776A (en) 1984-03-29
JPH048630B2 true JPH048630B2 (en) 1992-02-17

Family

ID=15782372

Family Applications (1)

Application Number Title Priority Date Filing Date
JP57163872A Granted JPS5954776A (en) 1982-09-22 1982-09-22 Manufacturing method of welded impeller

Country Status (1)

Country Link
JP (1) JPS5954776A (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108035833A (en) * 2017-12-08 2018-05-15 重庆水轮机厂有限责任公司 A kind of hydraulic turbine low specific-speed mixed-flow minor diameter manufacturing of runner method

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5133239A (en) * 1974-09-12 1976-03-22 Fuji Electric Co Ltd Furanshisugataranna no seisakuhoho
JPS5440945A (en) * 1977-09-02 1979-03-31 Tsurubosutoroenia Le Metaruric Method of manufacturing rotor wings of fluid machine
JPS5797073A (en) * 1980-12-08 1982-06-16 Toshiba Corp Production of francis type runner

Also Published As

Publication number Publication date
JPS5954776A (en) 1984-03-29

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