JPS6133963B2 - - Google Patents
Info
- Publication number
- JPS6133963B2 JPS6133963B2 JP5528781A JP5528781A JPS6133963B2 JP S6133963 B2 JPS6133963 B2 JP S6133963B2 JP 5528781 A JP5528781 A JP 5528781A JP 5528781 A JP5528781 A JP 5528781A JP S6133963 B2 JPS6133963 B2 JP S6133963B2
- Authority
- JP
- Japan
- Prior art keywords
- blade
- shroud
- impeller
- shape
- pressure
- 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
Links
- 238000000034 method Methods 0.000 claims description 14
- 238000005266 casting Methods 0.000 claims description 13
- 238000004519 manufacturing process Methods 0.000 claims description 8
- 230000004048 modification Effects 0.000 claims description 6
- 238000012986 modification Methods 0.000 claims description 6
- 239000000956 alloy Substances 0.000 description 6
- 229910045601 alloy Inorganic materials 0.000 description 4
- 229910000914 Mn alloy Inorganic materials 0.000 description 3
- 238000005452 bending Methods 0.000 description 3
- 238000012545 processing Methods 0.000 description 3
- 229910000838 Al alloy Inorganic materials 0.000 description 2
- 230000000994 depressogenic effect Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 239000011505 plaster Substances 0.000 description 2
- 238000007493 shaping process Methods 0.000 description 2
- 229910001297 Zn alloy Inorganic materials 0.000 description 1
- 238000003483 aging Methods 0.000 description 1
- 238000012937 correction Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 238000003672 processing method Methods 0.000 description 1
- 238000010791 quenching Methods 0.000 description 1
- 230000000171 quenching effect Effects 0.000 description 1
- 239000004576 sand Substances 0.000 description 1
- 230000008719 thickening Effects 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/04—Blade-carrying members, e.g. rotors for radial-flow machines or engines
- F01D5/043—Blade-carrying members, e.g. rotors for radial-flow machines or engines of the axial inlet- radial outlet, or vice versa, type
- F01D5/048—Form or construction
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Description
【発明の詳細な説明】
本発明は遠心圧縮機、ラジアルタービン等に使
用される羽根車の製造方法に関する。DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a method for manufacturing impellers used in centrifugal compressors, radial turbines, and the like.
この種の羽根車は一般に第1図に示す如く背面
シユラウド1および羽根2を有するが、羽根2が
彎曲して配向された羽根車の場合には所要の配向
状態にてダイキヤストすなわち加圧鋳造法で鋳造
できない場合が多い。このため従来は石膏型、砂
型、ロストワツクス型等を使用した鋳造技術が採
用され、作業性や精度等の面で大きな問題を残し
ていた。 This type of impeller generally has a back shroud 1 and blades 2 as shown in FIG. In many cases, it cannot be cast. For this reason, conventional casting techniques using plaster molds, sand molds, lost wax molds, etc. have been adopted, but these have left major problems in terms of workability and accuracy.
これを解決する方法として、本出願人はそのま
まの形状では加圧鋳造不可能な羽根の彎曲、折曲
ならびに羽根高さの変化状態を有する羽根車を、
加圧鋳造可能な形状に先ず加圧鋳造し、然る後所
要の形状となす製造方法を提供(特願昭55―
178992号)した。この方法では、羽根とシユラウ
ドとの接合基部に沿う所要部分の片側に肉盛部を
形成しておき、他側に肉盛部の形成と同時もしく
は後工程で切込みを形成した後その部分の羽根を
高さ方向へ起し、これにより肉盛部が羽根基部を
形成するようになして羽根の配向を修正すること
を特徴とした。 As a way to solve this problem, the present applicant has created an impeller with curved and bent blades, as well as changes in blade height, which cannot be pressure-cast in its original shape.
Provides a manufacturing method in which pressure casting is first performed into a shape that can be pressure cast, and then the desired shape is formed (patent application filed in 1982).
No. 178992). In this method, a built-up part is formed on one side of the required part along the base of the connection between the blade and the shroud, and a notch is formed on the other side at the same time as the built-up part or in a later process, and then the blade in that part is formed. The blade is raised in the height direction so that the built-up part forms the blade base, thereby correcting the orientation of the blade.
本発明はこのように加圧鋳造の採用を可能とし
た羽根車の製造方法をさらに改良することを目的
とする。 The object of the present invention is to further improve the method for manufacturing an impeller that makes it possible to employ pressure casting as described above.
すなわち本発明は、前述の如く修正することに
より羽根基部の各側に充分なアール面が形成され
て強度向上が保証されるようになすことを主眼と
し、このために羽根基部の各側に肉盛部および切
込みを形成するという概念に替えて羽根基部の間
のシユラウド面を修正後にアール面を呈する如く
付形することを特徴とする。すなわちシユラウド
面をこのように付形することによつて、先の方法
における肉盛部および切込みの作用を得ることに
加えてアール面の形成効果も併せて得るものであ
る。 In other words, the present invention aims to ensure that sufficient radiused surfaces are formed on each side of the blade base by the above-mentioned modification to ensure strength improvement, and for this purpose, thickening is provided on each side of the blade base. Instead of the concept of forming a raised part and a notch, the shroud surface between the blade bases is shaped so as to exhibit a rounded surface after modification. That is, by shaping the shroud surface in this manner, in addition to obtaining the effects of the built-up portion and notch in the previous method, the effect of forming a rounded surface can also be obtained.
本発面の製造方法は主にアルミニウム合金材で
羽根車を作る場合を主眼とし、このような加圧鋳
造後の羽根修正を可能にするAl―Si―Fe―Mg―
Mn系合金、Al―Si―Cu―Mg―Mn系合金および
Al―Mg―Zn系合金が本出願人によつて開発され
たことで実現可能となつたのである。すなわちこ
のようなアルミニウム合金材は特開昭51―86011
号公報により開示され“Dx30合金”として市販
されているAl―Si―Mg―Mn系合金およびこれに
Cuを0.5〜1.5重量%加えたAl―Si―Cu―Mg―
Mn系合金ならびに特公昭45―32808号公報に開示
されているもの、および“Cx―2A合金”として
市販されているAl―Mg―Zn系合金である。 The manufacturing method developed in this invention is mainly focused on making impellers from aluminum alloy materials, and uses Al-Si-Fe-Mg- which makes it possible to modify the impellers after pressure casting.
Mn alloy, Al-Si-Cu-Mg-Mn alloy and
This became possible due to the development of Al--Mg--Zn alloy by the applicant. In other words, this kind of aluminum alloy material is
Al--Si--Mg--Mn alloy disclosed in the publication and commercially available as "Dx30 alloy" and this
Al―Si―Cu―Mg― with Cu added 0.5 to 1.5% by weight
These include Mn-based alloys, those disclosed in Japanese Patent Publication No. 45-32808, and Al--Mg--Zn-based alloys commercially available as "Cx-2A alloys."
以下に第2図〜第5図にもとづいて本発明を説
明する。 The present invention will be explained below based on FIGS. 2 to 5.
第2図は本発明の方法における特徴を図解する
もので、この方法においては実線で示す如く加圧
鋳造可能な形状にて羽根車全体を加圧鋳造し、然
る後羽根2の所要範囲について起すことで二点鎖
線で示す羽根2′の位置へ修正することを基本と
する。 FIG. 2 illustrates the features of the method of the present invention. In this method, the entire impeller is pressure cast in a shape that can be pressure cast as shown by the solid line, and the required range of the rear blade 2 is Basically, the blade 2' is corrected to the position shown by the two-dot chain line by raising the blade 2'.
ここで修正を加える羽根2の範囲(羽根2とシ
ユラウド1との接合部に沿う方向の範囲)にわた
り、シユラウド面には第2図および第3図に示す
如く曲面10が形成される。この曲面10は羽根
2を起した際に羽根2の各側面A,Bとシユラウ
ド1の表面との接合部に充分な大きさのアール面
20A,20Bが形成されるのを目的とする。こ
のために曲面10は、羽根2の起し方向(矢印方
向)にて前面となる側面Aの基部付近が比較的大
きな曲率半径の凹面10Aにてシユラウド1の基
準表面Nに連続されるように付形される。また後
面となる側面Bの基部付近は基準表面Nよりも小
さな半径位置N′まで凹面10Bによりシユラウ
ド面が陥没され、この最下位置から隣りの羽根2
の側面Aの基部に形成された凹面10Aまで滑ら
かな曲面または平面で結ばれる。この曲面10は
金型で付形されるようになつており、従つて加圧
鋳造時に同時に形成される。 As shown in FIGS. 2 and 3, a curved surface 10 is formed on the shroud surface over the range of the blade 2 to be modified here (the range in the direction along the joint between the blade 2 and the shroud 1). The purpose of this curved surface 10 is to form rounded surfaces 20A and 20B of sufficient size at the joints between the side surfaces A and B of the blade 2 and the surface of the shroud 1 when the blade 2 is raised. For this purpose, the curved surface 10 is designed so that the vicinity of the base of the side surface A, which is the front surface in the raising direction (arrow direction) of the blade 2, is continuous with the reference surface N of the shroud 1 at a concave surface 10A having a relatively large radius of curvature. Shaped. In addition, near the base of the side surface B, which is the rear surface, the shroud surface is depressed by the concave surface 10B to a radius position N' smaller than the reference surface N.
The concave surface 10A formed at the base of the side surface A is connected to the concave surface 10A by a smooth curved surface or flat surface. This curved surface 10 is designed to be shaped using a mold, and therefore is formed simultaneously during pressure casting.
このように曲面10を有する羽根車を加圧鋳造
した後、所要の羽根範囲につき修正を行うと、第
2図に示す如く側面Aとシユラウド1の表面とは
凹面10Aが縮減されて凹面20Aで結ばれるこ
とになる。従つて凹面の曲率半径を予め大きく設
定することで充分に大きなアール面を得ることが
できる。一方側面Bとシユラウド1の表面とは凹
面10Bによつて陥没されているので、凹面10
Bが伸ばされてより大きな曲率半径を有する凹面
20Bで結ばれることになる。従つて凹面10B
の曲率を予め適当に設定しておくことで充分に大
きなアール面を得られる。 After press-casting the impeller having the curved surface 10 in this way, if the required blade range is modified, the concave surface 10A is reduced and the concave surface 20A is formed between the side surface A and the surface of the shroud 1, as shown in FIG. They will be tied together. Therefore, by setting the radius of curvature of the concave surface large in advance, a sufficiently large rounded surface can be obtained. On the other hand, since the side surface B and the surface of the shroud 1 are depressed by the concave surface 10B, the concave surface 10
B are stretched and connected by a concave surface 20B having a larger radius of curvature. Therefore, the concave surface 10B
By setting the curvature appropriately in advance, a sufficiently large radius surface can be obtained.
このような曲面10は羽根2の基部の位置の修
正量が大きくなる方向に伴つて第3図に示す如く
曲面幅Wが大体比例的に大きくなる。従つて第3
図に示すように修正の起点付近では曲面幅Wも小
さくなり、引続き滑らかにシユラウドの基準表面
に連接されることが好ましい。第4図および第5
図では曲面10を羽根車の正面および断面にて示
したが、これらから判る如く修正範囲においてシ
ユラウド表面に曲面10による陥没部が形成され
ることになるが、この陥没部は修正起点付近から
始まつて滑かに拡がるのであつて、しかも加圧鋳
造にて表面精度も良いことから流れを阻害する等
の問題は充分に抑えることができる。 In such a curved surface 10, as the amount of correction of the position of the base of the blade 2 increases, the curved surface width W increases approximately proportionally as shown in FIG. Therefore, the third
As shown in the figure, it is preferable that the curved surface width W also becomes smaller near the starting point of the modification, and that it continues to be smoothly connected to the reference surface of the shroud. Figures 4 and 5
In the figure, the curved surface 10 is shown in front and in cross section of the impeller, but as can be seen from these figures, a depression is formed on the shroud surface in the modification range, and this depression starts near the modification starting point. Furthermore, since it spreads smoothly and has good surface precision due to pressure casting, problems such as flow obstruction can be sufficiently suppressed.
このように本発明によれば先ず加圧鋳造した後
所要部分の羽根の修正を行う。然る後必要に応じ
て熱処理およびさらに他の加工を行うことで羽根
車が完成される。熱処理としては溶体化処理
(480〜530℃)し、焼入れ後温間曲げ加工を行な
い、次いで時効硬化(140〜200℃)させることに
より曲げ加工を容易にするとともに製品強度の向
上を図ることが出来る。従つて完成形状のものの
加圧鋳造が出来ない羽根車に対しても加圧鋳造工
程の採用が可能となり、特にこの加圧鋳造におい
てシユラウド面にアール面を付形のための曲面を
形成することで羽根修正後の肉厚の保持を確実化
し、しかも曲面付形の金型部分が比較的大きくな
つて正確度が向上される他石コウ型等を使用した
鋳造に比べて内部組織がちみつで、健全なものが
得られると共に、高速回転する羽根車にとつて重
要な重量バランスが極めて良好なものが製造で
き、また加圧鋳造後の加工法として曲げ加工を採
用したのでプレス加工等による他法よりも寸法精
度の良好なものが得られる等の利点がある。 As described above, according to the present invention, after pressure casting is performed, required portions of the blade are modified. Thereafter, the impeller is completed by performing heat treatment and other processing as necessary. Heat treatment includes solution treatment (480 to 530℃), quenching followed by warm bending, and then age hardening (140 to 200℃) to facilitate bending and improve product strength. I can do it. Therefore, the pressure casting process can be used even for impellers that have a completed shape but cannot be pressure cast, and in particular, in this pressure casting, it is possible to form a curved surface on the shroud surface for shaping the rounded surface. This ensures that the wall thickness is maintained after the blade is modified, and the curved mold part is relatively large, improving accuracy.In addition, the internal structure is less dense compared to casting using a plaster mold, etc. In addition to obtaining a sound product, it was also possible to manufacture a product with extremely good weight balance, which is important for impellers that rotate at high speed.Also, since we adopted bending processing as the processing method after pressure casting, it was possible to manufacture products using other methods such as press processing. This method has advantages such as being able to obtain products with better dimensional accuracy than the method.
第1図は一般的な羽根車の斜視図。第2図は本
発明の方法における特徴を図解する説明図。第3
図は本発明の方法で作られた羽根車の斜視図。第
4図および第5図は第3図の羽根車のそれぞれ平
面図および断面図。
1……シユラウド、2……羽根、10……曲
面、10A,10B……凹面、20A,20B…
…アール面。
Figure 1 is a perspective view of a typical impeller. FIG. 2 is an explanatory diagram illustrating the features of the method of the present invention. Third
The figure is a perspective view of an impeller made by the method of the present invention. 4 and 5 are a plan view and a sectional view, respectively, of the impeller of FIG. 3. 1...Shroud, 2...Blade, 10...Curved surface, 10A, 10B...Concave surface, 20A, 20B...
...R side.
Claims (1)
を、加圧鋳造可能な形状にて加圧鋳造した後、羽
根の所要部分を起して羽根形状を修正して完成形
状を得る製造方法であつて、羽根の引起し方向に
見て前面となる羽根側面に基準シユラウド面に連
接する比較的曲率半径の大きな凹面を、後面とな
る羽根の側面に基準シユラウド面より小さい半径
の面に連接する陥没せる凹面をそれぞれ前記羽根
形状の修正範囲にわたつて羽根基部に加圧鋳造に
より一体的に形成することを特徴とする羽根車の
製造方法。1. A manufacturing method in which an impeller that cannot be pressure cast in its completed shape is pressure cast into a shape that can be pressure cast, and then the required part of the blade is raised to correct the blade shape to obtain the completed shape. A concave surface with a relatively large radius of curvature connected to the reference shroud surface is formed on the side surface of the blade, which is the front side when viewed in the direction in which the blade is raised, and a recessed surface connected to a surface with a smaller radius than the reference shroud surface is formed on the side surface of the blade, which is the rear surface. A method for manufacturing an impeller, characterized in that concave surfaces are integrally formed on the blade base by pressure casting over the modification range of the blade shape.
Priority Applications (6)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP5528781A JPS57171004A (en) | 1981-04-13 | 1981-04-13 | Manufacture of impeller |
| CA000392340A CA1183675A (en) | 1980-12-19 | 1981-12-15 | Method for producing profiled product having fins |
| US06/331,177 US4520541A (en) | 1980-12-19 | 1981-12-16 | Method for producing profiled product having fins |
| FR8123602A FR2496528A1 (en) | 1980-12-19 | 1981-12-17 | METHOD FOR MANUFACTURING A PROFILE PRODUCT COMPRISING FINS |
| GB8138181A GB2091137B (en) | 1980-12-19 | 1981-12-18 | Method for producing profiled finned product |
| DE19813150553 DE3150553A1 (en) | 1980-12-19 | 1981-12-21 | METHOD FOR PRODUCING PROFILE PARTS WITH RIBS |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP5528781A JPS57171004A (en) | 1981-04-13 | 1981-04-13 | Manufacture of impeller |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS57171004A JPS57171004A (en) | 1982-10-21 |
| JPS6133963B2 true JPS6133963B2 (en) | 1986-08-05 |
Family
ID=12994362
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP5528781A Granted JPS57171004A (en) | 1980-12-19 | 1981-04-13 | Manufacture of impeller |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS57171004A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1999036701A1 (en) * | 1998-01-14 | 1999-07-22 | Ebara Corporation | Centrifugal turbomachinery |
| US6338610B1 (en) | 1998-01-14 | 2002-01-15 | Ebara Corporation | Centrifugal turbomachinery |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2006090701A1 (en) | 2005-02-22 | 2006-08-31 | Hitachi Metals Precision, Ltd. | Impeller for supercharger and method of manufacturing the same |
| CN107428049B (en) | 2015-03-06 | 2019-11-01 | 本田技研工业株式会社 | Method for manufacturing impeller |
-
1981
- 1981-04-13 JP JP5528781A patent/JPS57171004A/en active Granted
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1999036701A1 (en) * | 1998-01-14 | 1999-07-22 | Ebara Corporation | Centrifugal turbomachinery |
| US6338610B1 (en) | 1998-01-14 | 2002-01-15 | Ebara Corporation | Centrifugal turbomachinery |
Also Published As
| Publication number | Publication date |
|---|---|
| JPS57171004A (en) | 1982-10-21 |
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