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JPS5937135B2 - Manufacturing method of curved rotary impeller - Google Patents
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JPS5937135B2 - Manufacturing method of curved rotary impeller - Google Patents

Manufacturing method of curved rotary impeller

Info

Publication number
JPS5937135B2
JPS5937135B2 JP55077139A JP7713980A JPS5937135B2 JP S5937135 B2 JPS5937135 B2 JP S5937135B2 JP 55077139 A JP55077139 A JP 55077139A JP 7713980 A JP7713980 A JP 7713980A JP S5937135 B2 JPS5937135 B2 JP S5937135B2
Authority
JP
Japan
Prior art keywords
rotary impeller
curved
blade
straight
manufacturing
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
Application number
JP55077139A
Other languages
Japanese (ja)
Other versions
JPS574337A (en
Inventor
俊輔 鈴木
武 宮田
昭 佐藤
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Nissan Motor Co Ltd
Original Assignee
Nissan Motor Co Ltd
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 by Nissan Motor Co Ltd filed Critical Nissan Motor Co Ltd
Priority to JP55077139A priority Critical patent/JPS5937135B2/en
Publication of JPS574337A publication Critical patent/JPS574337A/en
Publication of JPS5937135B2 publication Critical patent/JPS5937135B2/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2250/00Geometry
    • F05B2250/70Shape
    • F05B2250/71Shape curved
    • 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
    • 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
    • Y02E10/70Wind energy
    • Y02E10/72Wind turbines with rotation axis in wind direction
    • 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
    • Y02PCLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P70/00Climate change mitigation technologies in the production process for final industrial or consumer products
    • Y02P70/50Manufacturing or production processes characterised by the final manufactured product

Landscapes

  • Wind Motors (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Hydraulic Turbines (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Description

【発明の詳細な説明】 本発明は羽根形状が彎曲面を呈する曲翼回転羽根車の製
造方法に関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a method for manufacturing a curved rotary impeller whose blades have a curved surface.

第1図に示すような彎曲面1を有する曲翼回転羽根車I
は、従来よりロストワツクス法、あるいは分割金型を用
いて製造するダイカスト法等の精密鋳造法によつて製造
していた。
A curved rotary impeller I having a curved surface 1 as shown in FIG.
have traditionally been manufactured by a precision casting method such as a lost wax method or a die casting method using a split mold.

しかしながら、前記いずれの鋳造法を用いても彎曲面1
を有する羽根部Rの形状に合致したキャビティを形成し
なければならないため、複雑な形状、構造等をもつた鋳
型、鋳造装置を製作しなければならず、前記鋳型、鋳造
装置等の製作費を含む設備費の増大を招き、その結果こ
れらの鋳造法では曲翼回転羽根車Iの製造コストが著し
く高くなるという欠点があつた。
However, no matter which casting method is used, the curved surface 1
Since it is necessary to form a cavity that matches the shape of the blade portion R, it is necessary to manufacture molds and casting equipment with complicated shapes and structures, and the manufacturing costs of the molds, casting equipment, etc. are reduced. As a result, these casting methods have the disadvantage that the production cost of the curved rotary impeller I increases significantly.

また、分割金型を用いての鋳造後、分割金型を半径方向
に移動させた時に、羽根形状に干渉するような羽根車は
、この方法では鋳造できないという問題もあつた。本発
明は、このような問題点に着目してなされたもので、そ
の目的とするところは複雑な彎曲キャビティを有する高
価な鋳型、鋳造装置等を用いることなく、先づ放射状に
配列された直状翼を有する回転羽根車を鋳造し、ついで
この直状翼を曲げ加工して曲翼回転羽根車を製造する方
法を提供するにある。
Another problem was that impellers that would interfere with the shape of the blades when the split mold was moved in the radial direction after casting using the split mold could not be cast using this method. The present invention has been made in view of these problems, and its purpose is to first produce straight lines arranged radially without using expensive molds or casting equipment having complicated curved cavities. The present invention provides a method for manufacturing a curved rotary impeller by casting a rotary impeller having shaped blades and then bending the straight blades.

以下、本発明の一実施例を第1図ないし第5図に基づい
て説明する。
An embodiment of the present invention will be described below with reference to FIGS. 1 to 5.

第2図は、本発明の道具鋳造工程によつて得られる羽根
部R’が軸部2に対して放射状に延びた複数の平板状直
状翼にを有する回転羽根車I’を示す。
FIG. 2 shows a rotary impeller I' in which the blade portion R' obtained by the tool casting process of the present invention has a plurality of flat straight blades extending radially with respect to the shaft portion 2.

この回転羽根車工′を製造するには、従来公知の方法例
えば、前記口ストワックス法あるいはダイカスト鋳造法
等を採用できるが、生産性を重視する場合にはダイカス
ト鋳造法によるのが望ましい。このダイカスト鋳造法に
よつて第2図に示す道具回転羽根車I’を鋳造する際に
用いる分割金型装置はたとえば第3図イ、口に示す構造
を備えている。すなわち、前記羽根車I’の軸部2及び
羽根部R’の形状に対応したキャビティにを形成し得る
金型3、すなわち道具形状に対応する刻設面3a’が刻
設された羽根枚数と同数の分割金型3aを集合してなる
金型3をもつている。そしてこれらの分割金型3aは上
下部型枠4、5及び側枠6で形成される空間内に配置さ
れている。J これらの分割金型3aは、それぞれ保持
体7を介して駆動シリンダ8に連結されて放射方向に進
退可能になつており、これらの駆動シリンダ8の作動に
より多数の分割金型3aが最も前進した位置で型閉状態
が保たれ、前記羽根車I’のギヤビア; イにを形成で
きるようになつている。
In order to manufacture this rotary impeller machine, conventionally known methods such as the above-mentioned stow wax method or die casting method can be used, but when emphasis is placed on productivity, it is preferable to use the die casting method. A split mold device used when casting the tool rotary impeller I' shown in FIG. 2 by this die casting method has, for example, the structure shown in FIG. 3A. That is, the mold 3 is capable of forming a cavity corresponding to the shape of the shaft portion 2 and the blade portion R' of the impeller I', that is, the number of blades on which the carved surface 3a' corresponding to the tool shape is engraved. It has a mold 3 made up of a set of the same number of split molds 3a. These split molds 3a are arranged in a space formed by the upper and lower mold frames 4 and 5 and the side frames 6. J These divided molds 3a are each connected to a drive cylinder 8 via a holder 7, so that they can move forward and backward in the radial direction. At this position, the mold is kept closed, and the gear via of the impeller I' can be formed.

そして、このキャビティに内にプランジャ−機構(詳細
図示は省略してあるが、下部型枠5の中央、下方に二点
鎖線をもつて示したプランシャー内蔵のシリンダP等)
により溶融金属を圧入し、硬化させた後、駆動シリンダ
8を矢印M方向に作動させ、各分割金型3aの型開きを
行い、第2図に示すような直翼回転羽根車『を鋳造する
ものである。
Inside this cavity is a plunger mechanism (detailed illustration is omitted, but there is a cylinder P with a built-in plunger shown in the center of the lower formwork 5 with a two-dot chain line at the bottom, etc.)
After press-fitting the molten metal and hardening it, the drive cylinder 8 is operated in the direction of arrow M to open each split mold 3a, and a straight-blade rotary impeller as shown in FIG. 2 is cast. It is something.

金型3aは第3図イ,口に示すように、その刻設面3a
′が彎曲面ではないので金型3aの加工はフライス、研
削等の通例の機械加工により容易に製作可能であり、彎
曲面を有する刻設面を具備した金型に比べてその製作工
数、及び費用を著しく低減することができると共に、金
型の損耗による修理が簡単であるという利点を有する。
The mold 3a has its engraved surface 3a as shown in FIG.
′ is not a curved surface, the mold 3a can be easily manufactured by conventional machining such as milling and grinding, and the manufacturing man-hours and This method has the advantage that costs can be significantly reduced and repairs due to wear and tear on the mold are easy.

すなわち、金型に彎曲面加工を施すにはモデルを使用す
る倣い加工機やNC工作機のような高価な精密工作機械
を使用しなければならず、このことが延いては金型の製
作費用の増大を招くという欠点が生じていたのである。
In other words, to machine a mold with a curved surface, it is necessary to use an expensive precision machine tool such as a copying machine that uses a model or an NC machine, which in turn increases the manufacturing cost of the mold. The disadvantage was that it led to an increase in

次に、前記工程で得られた直翼回転羽根車『(第2図参
照)を曲げ加工する曲翼加工工程につき説明する。
Next, a curved blade processing step of bending the straight blade rotary impeller (see FIG. 2) obtained in the above process will be described.

第4図、第5図はこの曲翼加工工程に用いる曲翼曲げ加
工装置の一実施例を示すものである。
FIGS. 4 and 5 show an embodiment of a curved wing bending device used in this curved wing processing step.

各図において、第2図に示したものと同様に、『は直翼
回転羽根車、2はこの直翼回転羽根車の軸部、yは平板
状の直状翼、Bは前記軸部2基部に形成した方形状のビ
スゲット部(このビスゲット部は最終的には切断されて
製品とはならない)である。10は中央に前記ビスゲッ
ト部Bに嵌合するよう座ぐり加工された受け面11を有
する基盤、12はこの基盤10上に設けた回転羽根車『
を固定する手段で、複数の溝13とこの溝13に嵌合し
、一端に前記ビスゲット部Bと係止する係合部14aを
有するクランプ部材14と、ボルト15とから成る。
In each figure, similarly to what is shown in FIG. This is a rectangular screw-get part formed at the base (this screw-get part will eventually be cut and will not become a product). Reference numeral 10 denotes a base having a receiving surface 11 at the center which is counterbore-processed to fit into the screw-get portion B, and 12 represents a rotary impeller provided on the base 10.
The clamping member 14 is a means for fixing the clamp member 14, and is comprised of a plurality of grooves 13, a clamp member 14 that fits into the grooves 13, and has an engaging portion 14a at one end that engages with the screw-get portion B, and a bolt 15.

16は各直状翼Yの曲げ加工を行う回動部材であり、こ
の回動部材16の内側にはその軸線方向に刻設した、羽
根枚数と同数の彎曲面18をもつた溝部19を有する。
Reference numeral 16 denotes a rotary member for bending each straight blade Y, and the rotary member 16 has a groove 19 carved in the axial direction inside the rotary member 16 and having the same number of curved surfaces 18 as the number of blades. .

20は前記回動部材16の回転を支承する受部で、この
実施例においては、前記各クランプ部材14上に立設し
た突片によつて構成されている。
Reference numeral 20 denotes a receiving portion for supporting the rotation of the rotating member 16, and in this embodiment, it is constituted by a projecting piece erected on each of the clamping members 14.

22は前記回動部材16の回動手段で、回動部材16の
上部外周壁面の一部に刻設したピニオン23とこのピニ
オン23と噛合するラツク24と、ラツク24を移動さ
せるための駆動シリンダ25とより構成される。
Reference numeral 22 denotes a rotating means for the rotating member 16, which includes a pinion 23 carved in a part of the upper outer peripheral wall surface of the rotating member 16, a rack 24 that meshes with the pinion 23, and a drive cylinder for moving the rack 24. 25.

26はラツク24の軸受である。26 is a bearing of the rack 24.

尚、前記ピニオン23、ラツク24及び駆動シリンダ2
5に代えてウオーム、ウオームギャ、及びウオームを回
動駆動させるモーターを使用し、これらをもつて回動部
材16の回動手段とすることも可能である。次に以上の
構成に基づき、この曲翼加工工程における作用につき説
明する。
In addition, the pinion 23, rack 24 and drive cylinder 2
It is also possible to use a worm, a worm gear, and a motor for rotationally driving the worm in place of 5, and use these as the means for rotating the rotating member 16. Next, based on the above configuration, the operation in this curved blade processing step will be explained.

まず、第4図及び第5図に示すように直翼回転羽根車『
のビスゲット部Bを基盤10の受け面11上に載置する
First, as shown in Figs. 4 and 5, a straight-blade rotary impeller ``
The screwget part B of is placed on the receiving surface 11 of the base plate 10.

次にボルト15を用いてクランプ部材14の係合部14
aをビスゲット部Bに押しつけることにより、前記回転
羽根車『を基盤10上に確固に固定する。その後、回動
部材16をその外周に設けてあるピニオン23をラツク
24に噛合させながら回転羽根車1′の上方から挿通さ
せて各クランプ部材14の各受部20の内側に載置する
。このようにして回転羽根車1″及び回動部材16の組
み込みを終了する。そして、駆動シリンダ25を矢符Y
方向へ作動させると、ラツク24がY方向へ移動し、こ
れによつて受部20に回転可能に支承された回動部材1
6が矢符X方向へ回動することになる。
Next, use the bolt 15 to tighten the engaging portion 14 of the clamp member 14.
By pressing the rotary impeller ``a'' against the screwget part B, the rotary impeller ``is firmly fixed on the base 10. Thereafter, the rotating member 16 is inserted from above the rotary impeller 1' while engaging the pinion 23 provided on its outer periphery with the rack 24, and placed inside each receiving portion 20 of each clamp member 14. In this way, the assembly of the rotary impeller 1'' and the rotating member 16 is completed.Then, move the drive cylinder 25 to the arrow Y.
When the rack 24 is operated in the Y direction, the rack 24 moves in the Y direction, thereby causing the rotating member 1 rotatably supported on the receiving portion 20 to move in the Y direction.
6 will rotate in the direction of arrow X.

すると、回動部材16の各彎曲面18が回転羽根車『の
直状翼yのそれぞれと当接し、これに曲げ加工を施す。
Then, each curved surface 18 of the rotary member 16 comes into contact with each of the straight blades y of the rotary impeller, and bends them.

そして更に回動部材16を回動し前記直状翼yが第4図
鎖線に示す如く彎曲面18の曲率とほぼ同じ曲率に曲げ
加工された時、今度は駆動シリンダ25を逆向き(矢符
Yと反対方向)に作動させて回動部材16を元の位置1
1C:復帰させる。このようにして第2図に示した直翼
回転羽根車1″は、第1図に示すように各翼が一定の曲
率でもつて曲げ加工されて曲翼回転羽根車1となる。こ
の後、ビスゲット部Bと軸部2との境界付近、例えば第
1図の2点鎖線Sのところで切断してビスゲット部を取
除く。以上、述べたように本発明は放射状の直状翼を有
する回転羽根車を鋳造する直翼鋳造工程と、この直翼鋳
造工程で得られた回転羽根車の直状翼に一定の曲げ加工
を行なう曲翼加工工程との二工程とから成り、直翼鋳造
工程では彎曲面を刻設した高価な鋳型を用いることなく
、製作の容易で簡単な直状翼の鋳造可能な鋳型を用いれ
ばよいので、鋳造工程は従来に比し格段と安価にでき、
また曲翼の形成加工は機械的曲げ加工で行えるので簡単
かつ迅速である。
Then, when the rotating member 16 is further rotated and the straight blade y is bent to a curvature that is almost the same as the curvature of the curved surface 18 as shown by the chain line in FIG. (in the opposite direction to Y) to return the rotating member 16 to its original position 1.
1C: Return. In this way, the straight-blade rotary impeller 1'' shown in FIG. 2 is bent into a curved-blade rotary impeller 1 by bending each blade with a constant curvature as shown in FIG. 1. After this, The screwget part is removed by cutting near the boundary between the screwget part B and the shaft part 2, for example at the two-dot chain line S in FIG. The straight blade casting process consists of two processes: a straight blade casting process in which the car is cast, and a curved blade processing process in which the straight blades of the rotary impeller obtained in this straight blade casting process are subjected to a certain bending process. Instead of using an expensive mold with a curved surface, it is sufficient to use a mold that can cast straight blades, which is easy to manufacture, so the casting process can be made much cheaper than in the past.
Furthermore, the curved blades can be formed easily and quickly by mechanical bending.

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

第1図は、ビスゲット部を含んだ曲翼回転羽根車の斜視
図、第2図はビスゲット部を含んだ直翼回転羽根車の斜
視図、第3図イは第2図に示す直翼回転羽根車を鋳造す
る分割金型装置の側断面図、第3図叫ま第3図イの口〜
口線に沿う断面図、第4図、第5図は本発明に使用する
曲翼曲げ加工装置の平面図及び縦断面図である。 『・・・・・・直翼回転羽根車、F′・・・・・・直状
翼、B・・・・・・ビスゲット部、I・・・・・・曲翼
回転羽根車、12・・・・・・回転羽根車1′を固定す
る手段、16・・・・・・回動部材、18・・・・・・
彎曲面、20・・・・・・回動部材16の受部、22・
・・・・・回動部材16の回動手段。
Figure 1 is a perspective view of a curved rotary impeller including a screwget part, Figure 2 is a perspective view of a straight blade rotary impeller including a screwget part, and Figure 3A is a straight blade rotary impeller shown in Figure 2. A side sectional view of the split mold device for casting impellers, Figure 3.
A sectional view taken along the mouth line, FIGS. 4 and 5 are a plan view and a longitudinal sectional view of the curved blade bending apparatus used in the present invention. ``...Straight-blade rotary impeller, F'...straight blade, B...visget part, I...curved-blade rotary impeller, 12. ...Means for fixing the rotary impeller 1', 16...Rotating member, 18...
Curved surface, 20... Receiving portion of rotating member 16, 22.
...Rotating means for the rotating member 16.

Claims (1)

【特許請求の範囲】[Claims] 1 放射状に配列された直状翼を有する回転羽根車を鋳
造する直翼鋳造工程と、この直翼鋳造工程にて得られた
回転羽根車の直状翼に所定方向の曲げ加工を施す曲翼加
工工程とよりなることを特徴とする曲翼回転羽根車の製
造方法。
1. A straight blade casting process in which a rotary impeller having straight blades arranged radially is cast, and a curved blade in which the straight blades of the rotary impeller obtained in this straight blade casting process are bent in a predetermined direction. A method for manufacturing a curved blade rotary impeller, comprising a processing step.
JP55077139A 1980-06-10 1980-06-10 Manufacturing method of curved rotary impeller Expired JPS5937135B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP55077139A JPS5937135B2 (en) 1980-06-10 1980-06-10 Manufacturing method of curved rotary impeller

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP55077139A JPS5937135B2 (en) 1980-06-10 1980-06-10 Manufacturing method of curved rotary impeller

Publications (2)

Publication Number Publication Date
JPS574337A JPS574337A (en) 1982-01-09
JPS5937135B2 true JPS5937135B2 (en) 1984-09-07

Family

ID=13625463

Family Applications (1)

Application Number Title Priority Date Filing Date
JP55077139A Expired JPS5937135B2 (en) 1980-06-10 1980-06-10 Manufacturing method of curved rotary impeller

Country Status (1)

Country Link
JP (1) JPS5937135B2 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH02248689A (en) * 1989-12-06 1990-10-04 Sanko Gosei Jushi Kk Integral form method of cross flow fan
CN108886259A (en) 2016-04-13 2018-11-23 三菱电机株式会社 Charge and discharge electric appliance

Also Published As

Publication number Publication date
JPS574337A (en) 1982-01-09

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