JPH05126092A - Impeller with welded construction - Google Patents
Impeller with welded constructionInfo
- Publication number
- JPH05126092A JPH05126092A JP28600891A JP28600891A JPH05126092A JP H05126092 A JPH05126092 A JP H05126092A JP 28600891 A JP28600891 A JP 28600891A JP 28600891 A JP28600891 A JP 28600891A JP H05126092 A JPH05126092 A JP H05126092A
- Authority
- JP
- Japan
- Prior art keywords
- impeller
- blade
- welding
- welded
- split
- 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.)
- Withdrawn
Links
Landscapes
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
Description
【0001】[0001]
【産業上の利用分野】本発明は冷凍機等に適用される溶
接構造羽根車に関するものである。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a welded structure impeller applied to a refrigerator or the like.
【0002】[0002]
【従来の技術】図2は溶接構造羽根車を示してあり、主
板1と前横板2の間に複数の翼3を備えた構造となって
いる。翼3は入口部(回転中心部)から出口部(外周
部)に向かい湾曲しつつ放射状に形成されており、羽根
車が回転することにより送排風を行う。2. Description of the Related Art FIG. 2 shows a welded structure impeller having a structure in which a plurality of blades 3 are provided between a main plate 1 and a front transverse plate 2. The blades 3 are formed in a radial shape while curving from the inlet portion (center of rotation) toward the outlet portion (outer peripheral portion), and perform air supply and exhaust by rotating the impeller.
【0003】図3〜図6は溶接構造羽根車の従来の溶接
構造を示すものであり、図2のA−A’断面にあたる部
分を示している。このうち図3及び図4はポート幅Pが
狭い場合の溶接構造の例を示し、図5及び図6はポート
幅Pが広い場合の例を示している。3 to 6 show a conventional welding structure of a welded structure impeller, and show a portion corresponding to the AA 'cross section of FIG. Of these, FIGS. 3 and 4 show examples of welded structures when the port width P is narrow, and FIGS. 5 and 6 show examples when the port width P is wide.
【0004】図3,図4に示すようにポート幅Pが狭い
場合には、外面側から溶接施工をして溶接羽根車を製作
していた。4は溶接金属である。この溶接構造では、完
全溶込みの確保が困難で、かつ、翼付根部5に生じるノ
ッチを回避できなかった。When the port width P is narrow as shown in FIGS. 3 and 4, welding is performed from the outer surface side to manufacture a welding impeller. 4 is a weld metal. With this welded structure, it was difficult to ensure complete penetration, and the notch generated in the blade root part 5 could not be avoided.
【0005】ポート幅Pが広い場合には、図5に示すよ
うに、内側から翼3と前横板2を溶接したり、図6に示
すように、内側から翼3と前横板2、ならびに翼3と主
板1とを溶接したりして、溶接羽根車を製作していた。
4は溶接金属である。When the port width P is wide, as shown in FIG. 5, the blade 3 and the front horizontal plate 2 are welded from the inside, or as shown in FIG. 6, the blade 3 and the front horizontal plate 2 are welded from the inside. In addition, the blade 3 was welded to the main plate 1 to produce a welded impeller.
4 is a weld metal.
【0006】[0006]
【発明が解決しようとする課題】ところで図3及び図4
に示すように、ポート幅Pが狭い溶接構造羽根車の場
合、溶接は外面側から施工しているが、この溶接中に内
面側の翼付根部5への溶込みが適当な曲率になり、ノッ
チを形成しないように制御する技術は現在のところ有し
ておらず、また、これをカバーすることも困難であっ
た。このため多少の溶込み不足或いは内面側の翼付根部
5への曲率悪化は犠牲にせざるを得なかった。By the way, FIG. 3 and FIG.
In the case of a welded structure impeller having a narrow port width P, as shown in FIG. 2, welding is performed from the outer surface side, but during this welding, the penetration into the blade root portion 5 on the inner surface side has an appropriate curvature, Currently, there is no technique for controlling notch formation, and it is difficult to cover this. For this reason, there was no choice but to sacrifice a slight lack of penetration or deterioration of the curvature of the blade root portion 5 on the inner surface side.
【0007】また、図5及び図6に示すように、ポート
幅Pが広い溶接構造羽根車の場合は、主板1と翼3、ま
たは前横板2と翼3を溶接しているが、主板1,前横板
2及び翼3で制限された空間で、しかもその溶接継手線
が曲線のため、その溶接には熟練を要し多くの工数を必
要としていた。Further, as shown in FIGS. 5 and 6, in the case of a welded structure impeller having a wide port width P, the main plate 1 and the blades 3, or the front transverse plate 2 and the blades 3 are welded. 1. In the space limited by the front horizontal plate 2 and the blades 3, and because the weld joint line is a curve, the welding requires skill and many man-hours.
【0008】本発明は、上記従来技術に鑑み、溶接作業
が簡単で且つ確実な溶接がされた溶接構造羽根車を提供
することを目的とする。The present invention has been made in view of the above prior art, and an object thereof is to provide a welded structure impeller in which welding work is simple and reliable welding is performed.
【0009】[0009]
【課題を解決するための手段】溶接構造羽根車の性能を
左右する製作上の主要因子は、前記のように完全溶込み
と翼付根部の適正な曲率確保である。完全溶込みが確保
しやすいのは、I型突合せ継手を深溶込み溶接法(電子
ビーム溶接,レーザ溶接,プラズマ溶接等)で施工する
場合であることから、継手形状はI型を採用した。一
方、翼付根部の適正曲率は、溶接金属で確保することは
極めて難しいことから、機械加工或いは鋳造,鍛造等に
より素材の段階で確保することにした。ここで最も考慮
したのは溶接継手の位置である。上記のように完全溶込
みが得られ且つ機械加工等で確保している適正曲率を損
なわない溶接構造とするために、翼の板厚中央部に、翼
厚さに直角方向に溶接継手を設ける構造とした。As described above, the main factors affecting the performance of the welded structure impeller are the complete penetration and the proper curvature of the blade root. Since it is easy to ensure complete penetration when the I-type butt joint is constructed by the deep penetration welding method (electron beam welding, laser welding, plasma welding, etc.), the I-type joint shape was adopted. On the other hand, since it is extremely difficult to secure the proper curvature of the root portion of the blade with weld metal, we decided to secure it at the material stage by machining, casting, forging, or the like. The most important consideration here is the position of the weld joint. A welded joint is provided in the blade thickness center part in the direction perpendicular to the blade thickness in order to obtain a welded structure that achieves complete penetration as described above and does not impair the proper curvature secured by machining, etc. With the structure.
【0010】[0010]
【作用】前記のような溶接構造とすることによって、両
側或いは片側からの深溶込溶接法によって完全溶込み溶
接が可能であり、且つ、翼付根部に設けた適正曲率を損
なうことなく溶接組立が可能になる。With the welding structure as described above, complete penetration welding can be performed by deep penetration welding from both sides or one side, and welding assembly can be performed without impairing the proper curvature provided at the blade root. Will be possible.
【0011】[0011]
【実施例】以下、本発明の好適な実施例を図面に基づき
詳細に説明する。図1は本発明の実施例を示す断面図で
あり、図2のA−A’断面にあたる部分を示している。
分割羽根車部材10は、図2に示す羽根車を、周方向に
沿う複数箇所で且つ翼3の板厚中央部で分割した形状を
なしている。そして周方向に沿う複数箇所で分割された
主板1,前横板2,翼3でなる個々の分割羽根車部材1
0は、機械加工,鋳造または鍛造等により一体に形成さ
れている。そしてこの素材である一体形成した各々の分
割羽根車部材10には、翼付根部5に適正な曲率の曲面
をあらかじめ形成してある。DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT A preferred embodiment of the present invention will now be described in detail with reference to the drawings. FIG. 1 is a cross-sectional view showing an embodiment of the present invention, showing a portion corresponding to the AA 'cross section of FIG.
The divided impeller member 10 has a shape obtained by dividing the impeller shown in FIG. 2 at a plurality of locations along the circumferential direction and at the plate thickness center portion of the blade 3. Then, an individual divided impeller member 1 composed of a main plate 1, a front lateral plate 2, and a blade 3 divided at a plurality of locations along the circumferential direction
0 is integrally formed by machining, casting or forging. In each of the integrally formed divided impeller members 10 made of this material, a curved surface having an appropriate curvature is previously formed on the blade root portion 5.
【0012】複数の分割羽根車部材10は周方向に配列
されており、隣接する部材10どうしは、分割された翼
3どうしで、深溶込溶接法(電子ビーム溶接,レーザ溶
接,プラズマ溶接等)により溶接されている。4は溶接
金属であり、溶接前では、相対向する翼3,3間がI型
開先部となる。A plurality of divided impeller members 10 are arranged in the circumferential direction. Adjacent members 10 are divided into blades 3 by deep penetration welding (electron beam welding, laser welding, plasma welding, etc.). ) Are welded together. Reference numeral 4 denotes a weld metal, and before welding, the I-shaped groove portion is formed between the blades 3 and 3 facing each other.
【0013】図1には、両側溶接の場合を示している
が、ポート幅の小さい溶接羽根車では片側溶接で行なう
ことができる。また、図示していないが、溶接中に翼3
の外表面が酸化することを防ぐため、その部分をガスシ
ールドしたり、銅当金等で冷却する場合もある。FIG. 1 shows a case of welding on both sides, but a welding impeller having a small port width can perform welding on one side. Although not shown, the blade 3 is
In order to prevent the outer surface of the product from being oxidized, the part may be gas-shielded or may be cooled with a copper metal or the like.
【0014】[0014]
【発明の効果】本発明によれば、適正な曲率の翼付根部
形状を有する分割羽根車部材同志を、翼厚さ中央部で突
合せ溶接することによって、完全溶込みとノッチのない
適正な溶接継手が確保できる。本発明の溶接構造の場
合、溶接は外側からのみ施行するが、深溶込み溶接法
(電子ビーム溶接,レーザ溶接,プラズマ溶接等)を適
用することによって現状の羽根車ではポート幅に関係な
く適用できる。このようにすれば、図3及び図4に示す
ポート幅の狭い従来構造の場合のように、前横板側翼付
根部のノッチを形成することはない。According to the present invention, the divided impeller members having a blade root portion shape with an appropriate curvature are butt-welded at the blade thickness central portion, so that proper welding without complete penetration and notch is achieved. A joint can be secured. In the case of the welded structure of the present invention, the welding is performed only from the outside, but by applying the deep penetration welding method (electron beam welding, laser welding, plasma welding, etc.), the present impeller is applied regardless of the port width. it can. In this way, the notch of the front blade side wing root portion is not formed unlike the conventional structure having a narrow port width shown in FIGS. 3 and 4.
【0015】なお、突合せ継手は全翼に設けても良い
が、何枚か毎に継手ができるような翼付ブロックを組立
てる工法をとれば更に溶接歪も軽減される。Although the butt joints may be provided on all the blades, welding distortion can be further reduced by adopting the method of assembling the winged blocks capable of forming joints for every several blades.
【図1】本発明の実施例における溶接構造を示す断面図
である。FIG. 1 is a cross-sectional view showing a welded structure in an embodiment of the present invention.
【図2】溶接構造羽根車を示す構成図である。FIG. 2 is a configuration diagram showing a welded structure impeller.
【図3】従来技術における溶接構造を示す断面図であ
る。FIG. 3 is a cross-sectional view showing a welding structure in the conventional technique.
【図4】従来技術における溶接構造を示す断面図であ
る。FIG. 4 is a cross-sectional view showing a welding structure according to a conventional technique.
【図5】従来技術における溶接構造を示す断面図であ
る。FIG. 5 is a cross-sectional view showing a welded structure in the related art.
【図6】従来技術における溶接構造を示す断面図であ
る。FIG. 6 is a cross-sectional view showing a welding structure in the conventional technique.
1 主板 2 前横板 3 翼 4 溶接金属 5 翼付根部 10 分割羽根車部材 P ポート幅 1 Main Plate 2 Front Horizontal Plate 3 Blade 4 Weld Metal 5 Blade Root 10 Split Impeller Member P Port Width
Claims (1)
翼を湾曲しつつ放射状に備えた羽根車であって、 前記羽根車を、周方向に沿う複数箇所で且つ翼の板厚中
央部の位置で分割した形状をなし、周方向に沿う複数箇
所で分割された主板と前横板と翼とが一体に形成され
て、翼付根部に適正な曲率の曲面を付けた複数の分割羽
根車部材を周方向に配列した状態で具備し、 隣接する分割羽根車部材どうしが、分割された翼どうし
で突合せ溶接してなることを特徴とする溶接構造羽根
車。1. An impeller having a plurality of blades that are curved and radially provided between a disc-shaped main plate and a front transverse plate, wherein the impeller is provided at a plurality of locations along a circumferential direction. It has a shape that is divided at the center of the plate thickness, and the main plate, the front horizontal plate, and the blade that are divided at multiple points along the circumferential direction are integrally formed, and a curved surface with an appropriate curvature is attached to the blade root. A welded structure impeller, comprising a plurality of divided impeller members arranged in a circumferential direction, wherein adjacent divided impeller members are butt-welded together by divided blades.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP28600891A JPH05126092A (en) | 1991-10-31 | 1991-10-31 | Impeller with welded construction |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP28600891A JPH05126092A (en) | 1991-10-31 | 1991-10-31 | Impeller with welded construction |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH05126092A true JPH05126092A (en) | 1993-05-21 |
Family
ID=17698809
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP28600891A Withdrawn JPH05126092A (en) | 1991-10-31 | 1991-10-31 | Impeller with welded construction |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH05126092A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2016098715A (en) * | 2014-11-20 | 2016-05-30 | 株式会社東芝 | Impeller and blower provided with the same |
-
1991
- 1991-10-31 JP JP28600891A patent/JPH05126092A/en not_active Withdrawn
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2016098715A (en) * | 2014-11-20 | 2016-05-30 | 株式会社東芝 | Impeller and blower provided with the same |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US7520055B2 (en) | Method for manufacturing a stator or rotor component | |
JP4155646B2 (en) | Method for joining a base of an airfoil and a disk and an assembly formed by this method | |
US7189064B2 (en) | Friction stir welded hollow airfoils and method therefor | |
KR100785543B1 (en) | Fluted blisk | |
US7200933B2 (en) | Method for manufacturing a stator component | |
KR101131198B1 (en) | Single-pass laser welding method of a T assembly of metallic parts | |
US7726938B2 (en) | Turbine blade and diaphragm construction | |
JP5557433B2 (en) | Welding nozzle assembly for steam turbine and associated assembly fixture | |
US20040146401A1 (en) | Turbine blade | |
GB2024959A (en) | Compressor rotor wheel for turbomachines | |
JPH0552101A (en) | Hollow fan moving blade of gas turbine | |
JPH0220802B2 (en) | ||
JP2005111561A (en) | Method of manufacturing or repairing monobloc bladed rotor disc | |
JP2002047944A (en) | High speed rotation type impeller | |
EP1540141B1 (en) | Method for manufacturing a stator or rotor component | |
JP4481822B2 (en) | Manufacturing method of stator blade component | |
JPH05126092A (en) | Impeller with welded construction | |
JPH08159088A (en) | Manufacture of impeller | |
JPS6326285A (en) | Welding and assembling method for impeller | |
JPS58143103A (en) | Manufacturing method of turbine nozzle diaphragm | |
JPH11148496A (en) | Impeller | |
JPS5963399A (en) | Impeller for pump | |
JP2017160875A (en) | Method for manufacturing impeller | |
JPH06117396A (en) | Manufacture of impeller | |
JPH02277997A (en) | Centrifugal impeller made of sheet metal |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
A300 | Withdrawal of application because of no request for examination |
Free format text: JAPANESE INTERMEDIATE CODE: A300 Effective date: 19990107 |