JPH094598A - Manufacture of impeller for centrifugal blower having aerofoil blade - Google Patents

Manufacture of impeller for centrifugal blower having aerofoil blade

Info

Publication number
JPH094598A
JPH094598A JP17802495A JP17802495A JPH094598A JP H094598 A JPH094598 A JP H094598A JP 17802495 A JP17802495 A JP 17802495A JP 17802495 A JP17802495 A JP 17802495A JP H094598 A JPH094598 A JP H094598A
Authority
JP
Japan
Prior art keywords
blade
blades
main plate
shroud
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.)
Granted
Application number
JP17802495A
Other languages
Japanese (ja)
Other versions
JP3291167B2 (en
Inventor
Hiroshi Gomi
弘 五味
Takaki Yoshida
隆紀 吉田
Yuichi Misawa
雄一 三澤
Takuya Shirai
琢也 白井
Tomoyoshi Noda
知義 野田
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.)
Takasago Thermal Engineering Co Ltd
Original Assignee
Takasago Thermal Engineering 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 Takasago Thermal Engineering Co Ltd filed Critical Takasago Thermal Engineering Co Ltd
Priority to JP17802495A priority Critical patent/JP3291167B2/en
Publication of JPH094598A publication Critical patent/JPH094598A/en
Application granted granted Critical
Publication of JP3291167B2 publication Critical patent/JP3291167B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/28Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
    • F04D29/281Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for fans or blowers
    • F04D29/282Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for fans or blowers the leading edge of each vane being substantially parallel to the rotation axis

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

PURPOSE: To precisely and easily manufacture an impeller for a centrifugal blower having a hollow aerofoil blade. CONSTITUTION: A shroud 1 and blades F1 -F8 are integrated by the aluminum die casting. A recessed part 3 which is open to the lower end face is formed in the blades F1 -F8 . A preliminarily pressed main plate 11 is abutted on the lower end part of the blades F1 -F8 , and a rivet 15 is passed through the recessed part 3 to fix the shroud 1 to the main plate 11. Positioning of the blades and the three dimensional machining of an upper end part are unnecessary, and the recessed part 3 forms a hollow part.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】本発明は、羽根の形が流線型の翼
形を有している遠心送風機用羽根車(ファンランナ)の
製造方法に関するものである。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a method for manufacturing an impeller (fan runner) for a centrifugal blower in which the blade has a streamlined blade shape.

【0002】[0002]

【従来の技術】遠心送風機は、複数の羽根を固定した羽
根車をケーシング内で回転させて、回転軸の中心方向か
ら吸い込んだ空気を、径方向に吹き出す構成を持った送
風機であり、羽根車とケーシングの形態等によって、多
翼送風機、ターボ送風機、翼型送風機などの種類がある
が、その中でも羽根の形が厚みを持って航空機の翼の形
を有しているいわゆる翼形送風機は、効率が良く騒音も
少ない。
2. Description of the Related Art A centrifugal blower is a blower having a structure in which an impeller having a plurality of fixed blades is rotated in a casing and air sucked in from the center of a rotating shaft is blown out in a radial direction. There are types such as a multi-blade blower, a turbo blower, and a wing blower depending on the form of the casing and the like, and among them, a so-called wing blower having a blade shape having a thickness and an aircraft wing shape is High efficiency and low noise.

【0003】図12に示した従来の一般的な翼形送風機
101に基づいて詳述すると、ケーシング102内に回
転自在に収容されているファンランナ103は、適宜の
回転駆動軸104によって回転し、軸方向に形成された
吸込口105から吸い込んだ空気を、径方向にある吐出
口106から吹き出すようになっている。
Explaining in detail based on the conventional general airfoil blower 101 shown in FIG. 12, a fan runner 103 rotatably housed in a casing 102 is rotated by an appropriate rotary drive shaft 104, Air sucked from the suction port 105 formed in the axial direction is blown out from the discharge port 106 in the radial direction.

【0004】そしてファンランナ103自体は、吸込口
105側の側板となるシュラウド107と、主板108
との間に固定されている複数の羽根109によって構成
されており、送風機の効率を上げるためにその全体の形
状は、回転中心からのいずれの距離における断面でも風
速がほぼ等しくなるように、シュラウド107において
通常は、円周方向に勾配がつけられている。即ち前記シ
ュラウド107は略円錐形状に成形されている。また各
羽根109は、図13に示したように、航空機の翼のよ
うに厚みをもった流線型の形状を有している。従って、
シュラウド107と羽根109との交点(接触部)は、
三次元の曲面になっている。
The fan runner 103 itself has a shroud 107 serving as a side plate on the suction port 105 side and a main plate 108.
And a plurality of blades 109 that are fixed between the shroud and the shroud so that the wind speed is almost the same at any distance from the center of rotation in order to increase the efficiency of the blower. At 107, there is usually a circumferential gradient. That is, the shroud 107 is formed in a substantially conical shape. In addition, each blade 109 has a streamlined shape having a thickness like an aircraft wing, as shown in FIG. Therefore,
The intersection (contact portion) between the shroud 107 and the blade 109 is
It has a three-dimensional curved surface.

【0005】このようなファンランナ103を製作する
場合、従来はファンランナ103全体を一体でアルミダ
イカスト等で製造したり、アルミ押し出し型材を三次元
切削加工した形成した羽根109を、1枚ずつシュラウ
ド107と主板108にビス等で固定したりしていた。
When manufacturing such a fan runner 103, conventionally, the entire fan runner 103 is integrally manufactured by aluminum die casting or the like, or the blades 109 formed by three-dimensionally cutting an aluminum extrusion die material are shrouded one by one. It was fixed to 107 and the main plate 108 with screws or the like.

【0006】[0006]

【発明が解決しようとする課題】しかしながら、前記し
たアルミダイカスト等でファンランナ103全体を一体
に製造する方法では、羽根109の内部を中空にできな
いので重量が増加してしまうという問題があった。また
一品ごとの生産となるために価格も高価であった。これ
に対し、羽根109をアルミ押し出し型材の三次元切削
加工によって構成した場合には、等断面で羽根の内部を
中空にできるので軽量化は図れるが、羽根109を1枚
毎に三次元切削加工するため非常に時間、手間がかか
り、しかも加工費が高いものとなっていた。さらに羽根
109を1枚ずつ、シュラウド107と主板108にビ
スで固定する作業であるから、位置決めが難しく精度及
び作業性も好ましいものではなかったのである。
However, in the method of integrally manufacturing the entire fan runner 103 by the above-mentioned aluminum die casting or the like, there is a problem that the inside of the blade 109 cannot be made hollow and the weight increases. In addition, the price was high because each product was manufactured. On the other hand, when the blades 109 are formed by three-dimensional cutting of an aluminum extruded die material, the inside of the blades can be hollow with an equal cross section so that the weight can be reduced, but each blade 109 is three-dimensionally cut. Therefore, it takes much time and labor, and the processing cost is high. Further, since it is the work of fixing the blades 109 to the shroud 107 and the main plate 108 one by one, it is difficult to perform positioning, and the accuracy and workability are not preferable either.

【0007】本発明はかかる点に鑑みてなされたもので
あり、羽根の中空部を形成することが容易で、かつ各羽
根の位置決めを行う必要がない、翼形羽根を有する遠心
送風機用羽根車の製造方法を提供して、前記問題の解決
を図ることを目的とする。
The present invention has been made in view of the above points, and it is easy to form the hollow portion of the blade and it is not necessary to position each blade. It is an object of the present invention to provide a method for manufacturing the above and solve the above problems.

【0008】[0008]

【課題を解決するための手段】前記目的を達成するた
め、請求項1によれば、一端部が主板に、他端部が吸込
口側の側板に位置する羽根の外形が、厚みのある翼形を
有している遠心送風機用羽根車を、造する方法であっ
て、側板と羽根とを、溶融材料の金型への圧力注入方法
によって一体成形して、この羽根の一端部側からは凹部
を形成し、予め加工した主板と前記羽根の一端部とを接
合して固定することを特徴とする、翼形羽根を有する遠
心送風機用羽根車の製造方法が提供される。
In order to achieve the above object, according to claim 1, a blade whose one end is located on the main plate and the other end is located on the side plate on the suction port side has a thick outer shape. A method for manufacturing an impeller for a centrifugal blower having a shape, in which a side plate and a blade are integrally molded by a method of injecting a molten material into a mold, and from one end side of this blade. A method for manufacturing an impeller for a centrifugal blower having an airfoil blade, characterized in that a concave portion is formed, and a preprocessed main plate and one end portion of the blade are joined and fixed.

【0009】また請求項2によれば、一端部が主板に、
他端部が吸込口側の側板に位置する羽根の外形が、厚み
のある翼形を有している遠心送風機用羽根車を、製造す
る方法であって、側板及び羽根の他端部寄りの部分を溶
融材料の金型への圧力注入方法によって一体成形して、
前記羽根の残りの部分を中空構造にして別途製造し、前
記羽根の残りの部分の他端部側を前記他端部寄りの部分
に嵌合し、予め加工した主板と前記羽根の残りの部分の
一端部側とを接合して固定することを特徴とする、翼形
羽根を有する遠心送風機用羽根車の製造方法が提供され
る。
According to a second aspect, one end portion of the main plate,
A method for manufacturing an impeller for a centrifugal blower, wherein the other end of the blade positioned on the side plate on the suction port side has a thick airfoil, which is closer to the other end of the side plate and the blade. The part is integrally molded by the method of pressure injection of the molten material into the mold,
The remaining portion of the blade is manufactured separately with a hollow structure, the other end side of the remaining portion of the blade is fitted to the portion near the other end, and the main plate preprocessed and the remaining portion of the blade A method for manufacturing an impeller for a centrifugal blower having airfoil blades, the method including joining and fixing one end side thereof.

【0010】前記各製造方法において、主板と羽根の一
端部、あるいは主板と羽根の一端部寄りの部分とを固定
するにあたっては、請求項3に記載したように、主板と
側板との間で羽根の中空部を貫通する部材、例えばビ
ス、リベット、通しボルトなどで固定するようにしても
よい。
In each of the above manufacturing methods, when fixing the main plate and one end of the blade, or the part of the main plate near the one end of the blade, as described in claim 3, the blade is provided between the main plate and the side plate. It may be fixed by a member penetrating the hollow part of the device, such as a screw, a rivet, or a through bolt.

【0011】前記各製造方法における溶融材料の金型へ
の圧力注入方法の例としては、材料が金属の場合には、
いわゆるダイカスト法が挙げられ、プラスチックを始め
とする合成樹脂が材料の場合には、射出成形法が挙げら
れる。いずれにしてもこれら各方法は、精密な成形加工
が可能である。
As an example of the method for injecting the molten material into the mold in each of the above manufacturing methods, when the material is a metal,
A so-called die casting method can be used, and when a synthetic resin such as plastic is used as a material, an injection molding method can be used. In any case, each of these methods enables precise molding.

【0012】[0012]

【作用】請求項1によれば、側板と羽根とを、溶融材料
の金型への圧力注入方法によって一体成形するが、羽根
の内部に一端部側からの凹部を形成することはもちろん
容易である。そして予め例えばプレス加工した主板と前
記羽根の一端部とを接合して固定すると、前記凹部はそ
のまま中空部となる。従って、羽根の中空部を形成する
ことが容易である。また羽根は、側板と一体に成形され
るので、羽根の位置決めを行う必要はない。
According to the first aspect of the present invention, the side plate and the blade are integrally formed by the method of injecting the molten material into the mold. However, it is of course easy to form the recess from the one end side inside the blade. is there. Then, for example, when the main plate that has been pressed in advance and one end of the blade are joined and fixed, the recess becomes a hollow part as it is. Therefore, it is easy to form the hollow portion of the blade. Further, since the blade is formed integrally with the side plate, it is not necessary to position the blade.

【0013】請求項2の製造方法の場合には、前記のよ
うに羽根の全てを側板と一体成形するのではなく、その
一部、即ち羽根の他端部寄りの部分を側板とを一体成形
するようになっている。次いで別途製造した中空構造の
羽根の残りの部分を前記他端部寄りの部分に嵌合するの
で、やはり羽根の位置決めの必要はない。この中空構造
の羽根の残りの部分は、例えば押し出し成形によって容
易に製造することができる。そして最後に予め加工した
主板と前記羽根の一端部寄りの部分とを接合して固定す
るようにしたので、羽根の中空部の形成は容易となって
いる。
In the manufacturing method according to the second aspect, not all the blades are integrally formed with the side plate as described above, but a part thereof, that is, a portion near the other end of the blade is integrally formed with the side plate. It is supposed to do. Then, since the remaining portion of the separately manufactured hollow blade is fitted to the portion near the other end, it is not necessary to position the blade. The rest of the hollow structure of the vanes can easily be manufactured, for example by extrusion. Finally, since the pre-processed main plate and the portion near the one end of the blade are joined and fixed, it is easy to form the hollow portion of the blade.

【0014】請求項3に記載したように、主板と側板と
の間で羽根の中空部を貫通する部材、例えばビス、リベ
ット、通しボルトなどで、羽根の一端部と主板、羽根の
一端部よりの部分と主板とを固定すれば、固定作業は容
易であり、しかも羽根は主板に対して強固に固定され
る。
As described in claim 3, a member penetrating the hollow portion of the blade between the main plate and the side plate, such as a screw, a rivet, or a through bolt, is used to remove the blade from one end of the blade and the main plate or one end of the blade. By fixing the portion and the main plate, the fixing work is easy and the blades are firmly fixed to the main plate.

【0015】[0015]

【実施例】以下、本発明の実施例を図面に基づき説明す
れば、まず図1に示したシュラウド1をアルミダイカス
トで製造する。図1は該シュラウド1の平面を示してお
り、その外形は略切頭円錐形状をなし、中央部には円形
の吸込口2が形成されている。
EXAMPLE An example of the present invention will be described below with reference to the drawings. First, the shroud 1 shown in FIG. 1 is manufactured by aluminum die casting. FIG. 1 shows a plan view of the shroud 1, the outer shape of which is substantially frustoconical, and a circular suction port 2 is formed in the central portion.

【0016】このシュラウド1の内側には、8枚の羽根
F1〜F8が一体に成形されている。各羽根F1〜F8は同
形同大であり、その上端部がシュラウド1の内側面と一
体になっている。また各羽根F1〜F8の下端部は、図2
に示したように、平坦に成形されている。さらに各羽根
F1〜F8の内部には、この下端部側に開口した凹部3が
同時に成形され、これら各凹部3の天井壁は、シュラウ
ド1の内側面によって構成されている。
Inside the shroud 1, eight blades F1 to F8 are integrally formed. Each of the blades F1 to F8 has the same shape and size, and the upper end portion thereof is integrated with the inner side surface of the shroud 1. The lower end of each blade F1 to F8 is shown in FIG.
As shown in, it is molded flat. Further, inside each of the blades F1 to F8, a recess 3 that opens to the lower end side is formed at the same time, and the ceiling wall of each recess 3 is formed by the inner side surface of the shroud 1.

【0017】シュラウド1における各羽根F1〜F8の凹
部3に対応した箇所には、それぞれ凹部3内に貫通する
透孔4、5が形成されている。これら透孔4、5を含め
て前記シュラウド1は、各羽根F1〜F8と共に、一体に
アルミダイカストで製造されたものである。
Through holes 4, 5 are formed in the shroud 1 at positions corresponding to the recesses 3 of the blades F1 to F8, respectively, which penetrate into the recesses 3. The shroud 1 including the through holes 4 and 5 is integrally manufactured by aluminum die casting together with the blades F1 to F8.

【0018】さらに図3に示した主板11を別途製造し
ておく。図3はこの主板11の平面を示しており、図4
に示したように、その中央部11aは、上側に凸となる
ように円錐台形状に成形され、その中心には、貫通孔1
2aを有する駆動用シャフト固定ボス12が設けられて
いる。また主板11の平坦部分には、前記シュラウド1
に形成した透孔4、5と対応する透孔13、14がそれ
ぞれ同心円状に穿設されている。
Further, the main plate 11 shown in FIG. 3 is manufactured separately. FIG. 3 shows a plane of the main plate 11, and FIG.
As shown in FIG. 3, the central portion 11a is formed in a truncated cone shape so as to be convex upward, and the through hole 1 is formed at the center thereof.
A drive shaft fixing boss 12 having 2a is provided. The shroud 1 is provided on the flat portion of the main plate 11.
Through holes 13 and 14 corresponding to the through holes 4 and 5 formed in the above are respectively concentrically formed.

【0019】即ち図3に示したように、シュラウド1と
主板11とを対向して組み合わせて各羽根F1〜F8の下
端部を主板11の上面に当接させた際(そのときの各羽
根F1〜F8の下端部の位置は図3中の二点鎖線で示
す)、シュラウド1の透孔4、5に対向して透孔13、
14が、各羽根F1〜F8の凹部3内に位置するように、
前記各透孔13、14は形成されている。前記駆動用シ
ャフト固定ボス12と主板11はプレス加工によって一
体に成形されたものである。
That is, as shown in FIG. 3, when the shroud 1 and the main plate 11 are combined facing each other and the lower end portions of the respective blades F1 to F8 are brought into contact with the upper surface of the main plate 11 (each blade F1 at that time). (The position of the lower end of F8 is indicated by a chain double-dashed line in FIG. 3), the through hole 13 is provided so as to face the through holes 4, 5 of the shroud 1,
14 so as to be located in the concave portion 3 of each of the blades F1 to F8,
The through holes 13 and 14 are formed. The drive shaft fixing boss 12 and the main plate 11 are integrally formed by press working.

【0020】次いで図5に示したように、前記構成のシ
ュラウド1と主板11とを対向して組み合わせて、各羽
根F1〜F8の下端部を主板11の上面に当接させる。そ
うすると各羽根F1〜F8の凹部3は、ちようど主板11
の上面で蓋をされた格好となり、各凹部3は、そのまま
各羽根F1〜F8の中空部を形成することになる。
Next, as shown in FIG. 5, the shroud 1 and the main plate 11 having the above-described structure are combined so as to face each other, and the lower ends of the blades F1 to F8 are brought into contact with the upper surface of the main plate 11. Then, the concave portion 3 of each of the blades F1 to F8 will have the chiodo main plate 11
The upper surface of the blade 3 is covered with a lid, and the recesses 3 form the hollow portions of the blades F1 to F8 as they are.

【0021】後は図6に示したように、シュラウド1に
形成した透孔4、5と、これら透孔4、5と対応する主
板11の透孔13、14との間を貫通する固定部材、例
えば図6に示したようなリベット材15などを用いて、
シュラウド1と主板11とを固定する。即ちリベット材
15をシュラウド1側から各羽根F1〜F8の中空部内に
入れ、主板11側底面においてその突出端部を強固にか
しめる。これによってシュラウド1と主板11とは強固
に固定され、また前記したリベット材15は、各羽根F
1〜F8の中空部内に入っているから、シュラウド1、主
板11及び各羽根F1〜F8の一体性は、極めて強固にな
っている。もちろん前記したリベット材15に代えて、
通しボルトやビスなどを用いても良い。
After that, as shown in FIG. 6, a fixing member penetrating between the through holes 4 and 5 formed in the shroud 1 and the through holes 13 and 14 of the main plate 11 corresponding to these through holes 4 and 5, respectively. , For example, using the rivet material 15 as shown in FIG.
The shroud 1 and the main plate 11 are fixed. That is, the rivet material 15 is put into the hollow portions of the blades F1 to F8 from the shroud 1 side, and the projecting end portion thereof is firmly caulked on the bottom surface of the main plate 11 side. As a result, the shroud 1 and the main plate 11 are firmly fixed to each other, and the rivet material 15 described above has the blades F
Since the shroud 1, the main plate 11, and the blades F1 to F8 are contained in the hollow portion 1 to F8, the integrity is extremely strong. Of course, instead of the rivet material 15 described above,
Through bolts or screws may be used.

【0022】以上の製造プロセスでも明らかなように、
従来のファンランナ全体をアルミダイカストで製造する
方法と比べると、本発明に従って製造されたファンラン
ナは、各羽根F1〜F8の内部に中空部が形成されてお
り、従来よりも重量が低減している。
As is clear from the above manufacturing process,
Compared with the conventional method of manufacturing the entire fan runner by aluminum die casting, the fan runner manufactured according to the present invention has a hollow portion formed inside each of the blades F1 to F8, and the weight is reduced as compared with the conventional method. There is.

【0023】また従来の押し出し成形によって製作した
羽根を1枚ずつ取り付ける方法と比べれば、羽根の位置
決めが不要であって、しかも羽根の上端部とシュラウド
内面との接合部の三次元加工も不要である。従って作業
が極めて容易で品質も向上している。
Further, compared with the conventional method of mounting the blades manufactured by extrusion molding one by one, the positioning of the blades is not required, and the three-dimensional processing of the joint between the upper end of the blade and the inner surface of the shroud is also unnecessary. is there. Therefore, the work is extremely easy and the quality is improved.

【0024】さらに前記実施例では、シュラウド1に形
成した固定用の透孔4、5はシュラウド1と各羽根F1
〜F8の一体成形時に形成されるため、例えばプレス加
工した後に曲面に穿孔する方法と比べると、透孔の形成
位置の精度が高く、また工数も低減している。
Further, in the above embodiment, the fixing through holes 4 and 5 formed in the shroud 1 are the shroud 1 and each blade F1.
Since they are formed during the integral molding of F8 to F8, the accuracy of the position of forming the through holes is higher and the man-hours are reduced as compared with, for example, a method of punching a curved surface after pressing.

【0025】なお各羽根F1〜F8の下端部は、平坦に成
形したものでよいから、例えば各羽根F1〜F8の上下方
向の長さを任意に設定でき、種々の翼高さを有するファ
ンランナーを製造することができる。
Since the lower ends of the blades F1 to F8 may be molded flat, for example, the vertical lengths of the blades F1 to F8 can be arbitrarily set, and fan runners having various blade heights can be set. Can be manufactured.

【0026】前記実施例では、シュラウド1と羽根F1
〜F8の全部を一体成形し、その後に主板11を接合し
て、固定するというプロセスを経ていたが、これに代え
て羽根の一部だけをシュラウドと一体に成形し、その後
当該一部に羽根の残りの部分を取り付けてから主板を最
後に接合固定するようにしてもよい。
In the above embodiment, the shroud 1 and the blade F1
The entire process of ~ F8 was integrally molded, and then the main plate 11 was joined and fixed. However, instead of this, only a part of the blade was integrally molded with the shroud, and then the blade was formed on the part. The main plate may be finally joined and fixed after the rest of the above is attached.

【0027】図7〜図11はそのような他の実施例のプ
ロセスを示しており、図7に示したシュラウド21はそ
の内側面に羽根の上端部UF1〜UF8(但し図面の都合
上、羽根の上端部UF4、UF5、UF6は省略してい
る)を一体にアルミダイカストで製造したものである。
FIGS. 7-11 show the process of such an alternative embodiment, wherein the shroud 21 shown in FIG. 7 has on its inner surface the upper ends UF1 to UF8 of the blades (however, for convenience of the drawings, the blades are not shown). The upper end portions UF4, UF5 and UF6 are omitted) and are integrally manufactured by aluminum die casting.

【0028】各羽根の上端部UF1〜UF8内には、それ
ぞれ下側に開口した凹部22が形成されており、さらに
各凹部22の周縁部には、その外周が羽根の上端部より
も僅かに小さい突部23が形成されている。なお24は
吸込口、25は各凹部内に開口した透孔であり、この透
孔25の外周にも前記実施例と同様、他の透孔が形成さ
れている。
In the upper end portions UF1 to UF8 of the blades, there are formed recesses 22 that open downward, and the outer circumference of each recess 22 is slightly smaller than the upper end portion of the blade. A small protrusion 23 is formed. In addition, 24 is a suction port, and 25 is a through hole opened in each recess, and another through hole is formed on the outer periphery of this through hole 25 as in the above embodiment.

【0029】一方図8、図9に示した羽根の残部DF1
〜DF8(但し図面の都合上、羽根の残部DF4、DF
5、DF6は省略している)を、例えばアルミ押し出し成
形によって製造しておく。これら各羽根の残部DF1〜
DF8は同形同大であって、かつその上下端面は平坦で
あり、その内部には、上下端面に開口した中空部26を
有している。従って、これら羽根の残部DF1〜DF8は
押し出し成形が容易な形状であって、適宜一定長さ毎に
直角に切断することによって、同一物を安価に量産でき
るものとなっている。
On the other hand, the remaining portion DF1 of the blade shown in FIGS.
~ DF8 (However, for convenience of drawing, the remaining blades DF4, DF
5 and DF6 are omitted) are manufactured by, for example, aluminum extrusion molding. Remaining part of each of these blades DF1 ~
The DF8 has the same shape and the same size, its upper and lower end faces are flat, and has a hollow portion 26 open to the upper and lower end faces therein. Therefore, the remaining portions DF1 to DF8 of these blades have a shape that can be easily extruded, and can be mass-produced at the same cost at a low cost by appropriately cutting the blades at a right angle at regular intervals.

【0030】そして図8、図9に示したように、各羽根
の上端部UF1〜UF8の突部23を、各羽根の残部DF
1〜DF8の中空部内に嵌入させて、両者を嵌合させ、各
羽根の上端部UF1〜UF8と各羽根の残部DF1〜DF8
とを一体化させれば、8枚の羽根が構成される。
Then, as shown in FIGS. 8 and 9, the projections 23 of the upper end portions UF1 to UF8 of the respective blades are replaced by the remaining portions DF of the respective blades.
1 to DF8 are fitted into the hollow portion, both are fitted to each other, and the upper ends UF1 to UF8 of each blade and the remaining portions DF1 to DF8 of each blade
Eight blades are formed by integrating and.

【0031】後は前記実施例と同様、図10に示したよ
うに、主板11の上面を各羽根の残部DF1〜DF8の下
端面に当接させるようにして、シュラウド21と主板1
1とを対向して組み合わせる。そうすると各羽根の上端
部UF1〜UF8の凹部22と、各羽根の残部DF1〜D
F8の中空部26とで、羽根の中空部が形成される。
After that, as in the case of the above-described embodiment, as shown in FIG. 10, the upper surface of the main plate 11 is brought into contact with the lower end surfaces of the remaining portions DF1 to DF8 of the blades, and the shroud 21 and the main plate 1 are made.
1 and face each other and combine. Then, the concave portions 22 of the upper end portions UF1 to UF8 of the respective blades and the remaining portions DF1 to D of the respective blades.
With the hollow portion 26 of F8, the hollow portion of the blade is formed.

【0032】次いで図11に示したように、シュラウド
21に形成した透孔25と、それに対応する主板11の
透孔13、14との間を、例えばボルト27、ナット2
8で締め付け固定してシュラウド21、各羽根の残部D
F1〜DF8及び主板11とを一体に固定すればよい。
Next, as shown in FIG. 11, between the through hole 25 formed in the shroud 21 and the corresponding through holes 13 and 14 of the main plate 11, for example, the bolt 27 and the nut 2 are provided.
Tighten and fix with 8 to shroud 21 and the rest of each blade D
The F1 to DF8 and the main plate 11 may be integrally fixed.

【0033】この実施例では、羽根の一部、即ち羽根の
上端部UF1〜UF8とシュラウド21とを一体成形し、
次いで各羽根の残部DF1〜DF8を各羽根の上端部UF
1〜UF8と嵌合し、その後主板11を固定するようにし
ており、やはり前記実施例と同様、従来よりも簡単にか
つ精度よくファンランナを製造することができ、しかも
羽根の内部に中空部が形成された軽量のファンランナを
製作することができる。また各羽根の残部DF1〜DF8
の上下方向の長さを変えることにより、種々の翼高さを
有するファンランナを製造することも可能である。
In this embodiment, a part of the blade, that is, the upper end portions UF1 to UF8 of the blade and the shroud 21 are integrally molded,
Then, set the remaining parts DF1 to DF8 of each blade to the upper end UF of each blade.
1 to UF8 are fitted, and then the main plate 11 is fixed. Again, like the above-mentioned embodiment, the fan runner can be manufactured more easily and more accurately than before, and the hollow portion is formed inside the blade. It is possible to manufacture a lightweight fan runner in which the above is formed. Also, the remaining parts of each blade DF1 to DF8
It is also possible to manufacture fan runners having various blade heights by changing the vertical length of the fan runner.

【0034】[0034]

【発明の効果】請求項1〜3に記載の発明によれば、中
空部を持った羽根を有する羽根車の製造が容易であり、
軽量の羽根車を提供することができる。そのうえ製造の
際に、羽根の位置決めをする必要はない。また請求項1
では、羽根の全部を側板と一体成形し、次いで主板を固
定するというプロセスを採っているので、製造作業は容
易でかつコストも低廉に抑えることができる。請求項2
でも、羽根の一部と側板とを一体成形しているので、製
造が容易であり、その分コストが低廉である。請求項3
の発明によれば、固定作業は容易であり、しかも羽根は
主板に対して強固に固定されるという効果が得られる。
According to the invention described in claims 1 to 3, it is easy to manufacture an impeller having a blade having a hollow portion,
A lightweight impeller can be provided. Moreover, it is not necessary to position the vanes during manufacture. Claim 1
In this case, since the process of integrally forming all of the blades with the side plate and then fixing the main plate is adopted, the manufacturing work can be facilitated and the cost can be kept low. Claim 2
However, since a part of the blade and the side plate are integrally molded, the manufacturing is easy and the cost is correspondingly low. Claim 3
According to the invention, the fixing work is easy, and the blade is firmly fixed to the main plate.

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

【図1】本発明の実施例に用いたシュラウドの平面図で
ある。
FIG. 1 is a plan view of a shroud used in an embodiment of the present invention.

【図2】図1のA−A線断面図である。FIG. 2 is a sectional view taken along line AA of FIG.

【図3】本発明の実施例に用いた主板の平面図である。FIG. 3 is a plan view of a main plate used in an example of the present invention.

【図4】図1のB−B線断面図である。FIG. 4 is a sectional view taken along line BB of FIG. 1;

【図5】図1に示したシュラウドと図3に示した主板と
を組み合わせた状態を示す縦断面図である。
5 is a longitudinal sectional view showing a state in which the shroud shown in FIG. 1 and the main plate shown in FIG. 3 are combined.

【図6】リベット材を用いて図1のシュラウドと図3の
主板とを固定する状態を示す縦断面図である。
6 is a vertical cross-sectional view showing a state in which the shroud of FIG. 1 and the main plate of FIG. 3 are fixed to each other by using a rivet material.

【図7】他の実施例にかかるシュラウドの縦断面図であ
る。
FIG. 7 is a vertical cross-sectional view of a shroud according to another embodiment.

【図8】図7のシュラウドに羽根の残部を嵌合する様子
を示す縦断面図である。
8 is a vertical cross-sectional view showing how the remaining portion of the blade is fitted into the shroud of FIG.

【図9】羽根の上端部と羽根の残部とを嵌合する様子を
示す斜視図である。
FIG. 9 is a perspective view showing how the upper end of the blade and the rest of the blade are fitted together.

【図10】図7に示したシュラウドと図3に示した主板
とを組み合わせた状態を示す縦断面図である。
10 is a vertical cross-sectional view showing a state in which the shroud shown in FIG. 7 and the main plate shown in FIG. 3 are combined.

【図11】ボルト、ナットを用いて図7のシュラウドと
図3の主板とを固定する状態を示す縦断面図である。
11 is a vertical cross-sectional view showing a state in which the shroud of FIG. 7 and the main plate of FIG. 3 are fixed using bolts and nuts.

【図12】従来の方法によって製造されたシュラウドの
縦断面図である。
FIG. 12 is a vertical cross-sectional view of a shroud manufactured by a conventional method.

【図13】従来の方法によって製造されたシュラウドの
平面図である。
FIG. 13 is a plan view of a shroud manufactured by a conventional method.

【符号の説明】[Explanation of symbols]

1 シュラウド 2 吸込口 3 凹部 4、5 透孔 11 主板 13、14 透孔 15 リベット材 F1〜F8 羽根 1 Shroud 2 Suction Port 3 Recesses 4, 5 Through Hole 11 Main Plate 13, 14 Through Hole 15 Rivet Material F1 ~ F8 Blade

───────────────────────────────────────────────────── フロントページの続き (72)発明者 野田 知義 東京都多摩市永山4−4−13−903 ─────────────────────────────────────────────────── ─── Continuation of the front page (72) Inventor Tomoyoshi Noda 4-4-13-903 Nagayama, Tama City, Tokyo

Claims (3)

【特許請求の範囲】[Claims] 【請求項1】 一端部が主板に、他端部が吸込口側の側
板に位置する羽根の外形が、厚みのある翼形を有してい
る、遠心送風機用羽根車を製造する方法であって、側板
と羽根とを、溶融材料の金型への圧力注入方法によって
一体成形して、この羽根の一端部側から凹部を形成し、
予め加工した主板と前記羽根の一端部とを接合して固定
することを特徴とする、翼形羽根を有する遠心送風機用
羽根車の製造方法。
1. A method for manufacturing an impeller for a centrifugal blower, wherein one end of a blade is located at a main plate and the other end is located at a side plate on the suction port side, and the outer shape of the blade has a thick blade shape. Then, the side plate and the blade are integrally molded by a method of injecting the molten material into the mold to form a recess from one end side of the blade,
A method for manufacturing an impeller for a centrifugal blower having airfoil-shaped blades, characterized in that a preprocessed main plate and one end portion of the blades are joined and fixed.
【請求項2】 一端部が主板に、他端部が吸込口側の側
板に位置する羽根の外形が、厚みのある翼形を有してい
る、遠心送風機用羽根車を製造する方法であって、側板
及び羽根の他端部寄りの部分を溶融材料の金型への圧力
注入方法によって一体成形して、前記羽根の残りの部分
を中空構造にして別途製造し、前記羽根の残りの部分の
他端部側を前記他端部寄りの部分に嵌合し、予め加工し
た主板と前記羽根の残りの部分の一端部側とを接合して
固定することを特徴とする、翼形羽根を有する遠心送風
機用羽根車の製造方法。
2. A method for manufacturing an impeller for a centrifugal blower, wherein one end of the blade is located on the main plate and the other end is located on the suction side plate, and the outer shape of the blade has a thick airfoil. Then, the side plate and the portion near the other end of the blade are integrally molded by a method of injecting the molten material into the mold to form the remaining portion of the blade into a hollow structure and separately manufactured. The airfoil blade is characterized in that the other end side of the blade is fitted to a portion near the other end, and a preprocessed main plate and one end side of the remaining portion of the blade are joined and fixed. A method for manufacturing an impeller for a centrifugal blower having the same.
【請求項3】前記固定にあたっては、主板と側板との間
で羽根の中空部を貫通する部材で固定することを特徴と
する、請求項1又は2に記載の翼形羽根を有する遠心送
風機用羽根車の製造方法。
3. The centrifugal blower having airfoil blades according to claim 1, wherein the fixing is performed by a member penetrating the hollow portion of the blade between the main plate and the side plate. Impeller manufacturing method.
JP17802495A 1995-06-20 1995-06-20 Method of manufacturing impeller for centrifugal blower having airfoil blade Expired - Fee Related JP3291167B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP17802495A JP3291167B2 (en) 1995-06-20 1995-06-20 Method of manufacturing impeller for centrifugal blower having airfoil blade

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP17802495A JP3291167B2 (en) 1995-06-20 1995-06-20 Method of manufacturing impeller for centrifugal blower having airfoil blade

Publications (2)

Publication Number Publication Date
JPH094598A true JPH094598A (en) 1997-01-07
JP3291167B2 JP3291167B2 (en) 2002-06-10

Family

ID=16041255

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Application Number Title Priority Date Filing Date
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Country Status (1)

Country Link
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Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2005127176A (en) * 2003-10-22 2005-05-19 Matsushita Electric Ind Co Ltd Turbofan and manufacturing method for turbofan
JP2006291710A (en) * 2005-04-05 2006-10-26 Maruyama Mfg Co Ltd Wheel impeller for centrifugal blower
CN100453818C (en) * 2006-03-03 2009-01-21 山东大学 Technological process of making wing type centrifugal vane whell
JP2012526230A (en) * 2009-05-08 2012-10-25 ヌオーヴォ ピニォーネ ソシエタ ペル アチオニ Composite shroud and method of attaching shroud to multiple blades
CN104613006A (en) * 2014-12-10 2015-05-13 张凤荣 Wing sectional material combination type turbine centrifugal impeller
CN104653512A (en) * 2015-02-05 2015-05-27 冯桂超 Molding glass fiber reinforced plastic centrifugal fan impeller and preparation method thereof
US9797255B2 (en) 2011-12-14 2017-10-24 Nuovo Pignone S.P.A. Rotary machine including a machine rotor with a composite impeller portion and a metal shaft portion
US9810235B2 (en) 2009-11-23 2017-11-07 Massimo Giannozzi Mold for a centrifugal impeller, mold inserts and method for building a centrifugal impeller
EP2959172B1 (en) * 2013-02-25 2019-10-23 Greenheck Fan Corporation Methods of producing a fan wheel
US11162505B2 (en) 2013-12-17 2021-11-02 Nuovo Pignone Srl Impeller with protection elements and centrifugal compressor

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2005127176A (en) * 2003-10-22 2005-05-19 Matsushita Electric Ind Co Ltd Turbofan and manufacturing method for turbofan
JP2006291710A (en) * 2005-04-05 2006-10-26 Maruyama Mfg Co Ltd Wheel impeller for centrifugal blower
JP4504860B2 (en) * 2005-04-05 2010-07-14 株式会社丸山製作所 Impeller for centrifugal blower
CN100453818C (en) * 2006-03-03 2009-01-21 山东大学 Technological process of making wing type centrifugal vane whell
JP2012526230A (en) * 2009-05-08 2012-10-25 ヌオーヴォ ピニォーネ ソシエタ ペル アチオニ Composite shroud and method of attaching shroud to multiple blades
US8998581B2 (en) 2009-05-08 2015-04-07 Nuovo Pignone S.P.A. Composite shroud and methods for attaching the shroud to plural blades
US9810230B2 (en) 2009-05-08 2017-11-07 Nuovo Pignone Srl Impeller for a turbomachine and method for attaching a shroud to an impeller
US9810235B2 (en) 2009-11-23 2017-11-07 Massimo Giannozzi Mold for a centrifugal impeller, mold inserts and method for building a centrifugal impeller
US9797255B2 (en) 2011-12-14 2017-10-24 Nuovo Pignone S.P.A. Rotary machine including a machine rotor with a composite impeller portion and a metal shaft portion
EP2959172B1 (en) * 2013-02-25 2019-10-23 Greenheck Fan Corporation Methods of producing a fan wheel
US11162505B2 (en) 2013-12-17 2021-11-02 Nuovo Pignone Srl Impeller with protection elements and centrifugal compressor
CN104613006A (en) * 2014-12-10 2015-05-13 张凤荣 Wing sectional material combination type turbine centrifugal impeller
CN104653512B (en) * 2015-02-05 2017-01-18 冯桂超 Molding glass fiber reinforced plastic centrifugal fan impeller and preparation method thereof
CN104653512A (en) * 2015-02-05 2015-05-27 冯桂超 Molding glass fiber reinforced plastic centrifugal fan impeller and preparation method thereof

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