JP3106165B2 - Cross flow fan - Google Patents
Cross flow fanInfo
- Publication number
- JP3106165B2 JP3106165B2 JP04325651A JP32565192A JP3106165B2 JP 3106165 B2 JP3106165 B2 JP 3106165B2 JP 04325651 A JP04325651 A JP 04325651A JP 32565192 A JP32565192 A JP 32565192A JP 3106165 B2 JP3106165 B2 JP 3106165B2
- Authority
- JP
- Japan
- Prior art keywords
- blade
- partition plate
- impeller
- cross flow
- flow fan
- 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 - Fee Related
Links
Landscapes
- Structures Of Non-Positive Displacement Pumps (AREA)
Description
【0001】[0001]
【産業上の利用分野】本発明は、たとえば空気調和機を
構成する室内ユニット内に配置され、熱交換空気である
被空調室空気の送風作用をなす横流ファンに関する。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a cross flow fan arranged in an indoor unit constituting an air conditioner, for example, and for blowing air to be conditioned in a room to be conditioned.
【0002】[0002]
【従来の技術】空気調和機を構成する室内ユニット内に
は、室内側熱交換器とともに室内送風機が配置される。
最近の住宅事情から室内ユニットは、高さ寸法を抑制す
る要望が大であり、そのため上記室内側熱交換器とも幅
寸法を長くとる傾向にある。2. Description of the Related Art An indoor blower is arranged together with an indoor heat exchanger in an indoor unit constituting an air conditioner.
Due to recent housing circumstances, there is a great demand for suppressing the height of the indoor unit, and therefore the width of the indoor heat exchanger also tends to be long.
【0003】このような室内側熱交換器に対して被空調
室空気を送風する上記室内送風機は、熱交換器の均一な
熱交換効率を得るために、幅寸法とほとんど同長の送風
範囲が必要である。[0003] In order to obtain uniform heat exchange efficiency of the heat exchanger, the above-mentioned indoor blower for blowing the air to be conditioned to the indoor side heat exchanger has a blowing range almost the same length as the width. is necessary.
【0004】したがって、各種の送風機のうち、特に軸
方向長さが長く、広い送風範囲が得られる横流ファンが
最適である。[0004] Therefore, among various types of blowers, a cross flow fan which has a particularly long axial length and can obtain a wide range of blowing is most suitable.
【0005】図5(A)に、横流ファンの基本的な形状
構造を示す。FIG. 5A shows a basic configuration of a cross flow fan.
【0006】その中心部に軸部1aが設けられる両側板
1,1と、これら両側板1,1間に軸方向に所定間隔を
存して配置される仕切板2…と、両側板1,1と仕切板
2…との間に介在され、かつこの周端部に、周方向に沿
って複数配列される、それぞれが湾曲成されるブレード
3…とからなる。[0006] Both side plates 1, 1 provided with a shaft portion 1a at the center thereof, partition plates 2, ... arranged at predetermined intervals in the axial direction between these side plates 1, 1; 1 and a plurality of blades 3 interposed between the partition plates 2 and arranged along the circumferential direction at the peripheral end.
【0007】図5(B)に示すように、横流ファンの製
造にあたって、予め、仕切板2と、この仕切板2の一側
面に複数枚のブレード3…を、一体に突出してなる、多
翼型羽根車4を製作する。As shown in FIG. 5 (B), in the manufacture of a cross flow fan, a multi-blade is formed by previously projecting a partition plate 2 and a plurality of blades 3 on one side surface of the partition plate 2. The mold impeller 4 is manufactured.
【0008】この多翼型羽根車4を、軸方向に沿って積
み重ねる。すなわち、下部側多翼型羽根車4の仕切板2
上面に、上部側多翼型羽根車4のブレード3の先端縁が
載る状態となる。[0008] The multi-blade type impeller 4 is stacked along the axial direction. That is, the partition plate 2 of the lower multi-blade impeller 4
The top edge of the blade 3 of the upper multi-blade impeller 4 rests on the upper surface.
【0009】ついで、上部側羽根車4の仕切板2上面に
超音波溶着手段を構成するホーンHを当て、超音波エネ
ルギを付与する。超音波エネルギは、図中破線矢印に示
すように、この仕切板2を介して一体のブレード3先端
縁に集中するところとなり、超音波振動をなす。Next, a horn H constituting ultrasonic welding means is applied to the upper surface of the partition plate 2 of the upper impeller 4 to apply ultrasonic energy. The ultrasonic energy is concentrated on the leading edge of the integral blade 3 via the partition plate 2 as shown by the dashed arrow in the drawing, and generates ultrasonic vibration.
【0010】このブレード3先端縁は下部側仕切板2
と、単なる当接状態にあり、ブレード3先端縁が超音波
振動することによって、これと下部側仕切板2との間に
摩擦熱が発生する。所定時間継続して、超音波エネルギ
を供給すれば、上部ブレード3先端部と下部側仕切板2
の当接部位とが溶着し、上下部羽根車4,4相互が一体
化する。The leading edge of the blade 3 is located on the lower partition plate 2.
When the blade 3 is ultrasonically vibrated at its leading edge, frictional heat is generated between the blade 3 and the lower partition plate 2. If ultrasonic energy is supplied continuously for a predetermined time, the tip of the upper blade 3 and the lower partition plate 2
And the upper and lower impellers 4 and 4 are integrated with each other.
【0011】また、従来より、送風効率の向上を図るた
め、および送風騒音を低減させるために、特に、上記ブ
レード3を対象とする多くの工夫がなされている。Conventionally, many attempts have been made to improve the blowing efficiency and to reduce the blowing noise, especially for the blade 3.
【0012】特開昭60−17296号公報には、図6
に示すようになブレード構造が開示される。Japanese Patent Application Laid-Open No. Sho 60-17296 discloses FIG.
A blade structure is disclosed as shown in FIG.
【0013】それぞれのブレード3…は、弦長や曲率半
径等の形状構造を同一とするも、互いに隣接するブレー
ド3,3相互間と中心点Oとでなす角度θが、互いに異
なる(θ1 ≠θ 2≠θ3 …)よう設定され、ブレード3
の周方向に沿う配列ピッチが、不等である。Each of the blades 3 has the same shape and structure such as a chord length and a radius of curvature, but the angles θ between the adjacent blades 3 and 3 and the center point O are different from each other (θ 1). ≠ θ 2 ≠ θ 3 …) and blade 3
Are unequal in arrangement pitch along the circumferential direction.
【0014】このような構造は、結局、ブレード3の周
方向に沿う配列を非対称となすことが特徴であるので、
回転軸とファンとの重心が異なることになり、回転時の
アンバランスが増大する。Such a structure is characterized in that the arrangement of the blades 3 along the circumferential direction is asymmetrical.
Since the center of gravity of the rotating shaft and the center of gravity of the fan are different, imbalance during rotation increases.
【0015】したがって、バランス調整のための錘(お
もり)が必要となるが、別部品である錘を取り付けるに
は、手間がかかって面倒であり、材料費および取付け工
数が増大する不具合を招く。Therefore, a weight (weight) for adjusting the balance is required. However, mounting the weight as a separate component is troublesome and troublesome, and causes a problem that the material cost and the number of mounting steps are increased.
【0016】特開平4−164195号公報には、図7
(A),(B)に示すような、上述した不具合を除去す
るための構成が開示されている。Japanese Patent Application Laid-Open No. 4-164195 discloses FIG.
A configuration for removing the above-described disadvantages as shown in (A) and (B) is disclosed.
【0017】すなわち、仕切板2の一側面にブレード3
を一体成形する多翼型羽根車4の製造段階で、ブレード
3が突設された側面と反対側の側面に一体に偏肉部5を
設け、錘の代用としてのバランサ機能を有するようにな
っている。That is, the blade 3 is provided on one side of the partition plate 2.
In the manufacturing stage of the multi-blade impeller 4 in which the blade 3 is formed integrally, the uneven thickness portion 5 is provided integrally on the side surface opposite to the side surface on which the blade 3 is projected, so that it has a balancer function as a substitute for the weight. ing.
【0018】[0018]
【発明が解決しようとする課題】図8に示すように、こ
のようなファンでは、ブレード3が位置する側面と反対
側の側面に偏肉部5が設けられることになり、この側面
には、また、超音波溶着手段としてのホーンHが当てら
れる。As shown in FIG. 8, in such a fan, an uneven thickness portion 5 is provided on the side opposite to the side where the blade 3 is located. Further, a horn H as an ultrasonic welding means is applied.
【0019】したがって、偏肉部5に対してホーンHが
接触し易く、超音波エネルギが必要な溶着部分に伝達し
ない可能性が大である。Therefore, the horn H easily comes into contact with the uneven thickness portion 5, and there is a large possibility that the ultrasonic energy is not transmitted to the necessary welding portion.
【0020】ホーンHの接触から確実に避けるように、
偏肉部5の位置を選択する考えもあるが、超音波エネル
ギをブレード3先端部に効率よく供給するためには、ホ
ーンHを、ブレード3が設けられる仕切板2周端部に当
てがわなければならず、必然的に、偏肉部5は回転中心
軸OL寄りの位置に選択されてしまう。In order to reliably avoid contact with the horn H,
Although there is a method of selecting the position of the uneven thickness portion 5, in order to efficiently supply ultrasonic energy to the tip of the blade 3, the horn H is applied to the peripheral end of the partition plate 2 on which the blade 3 is provided. Therefore, the uneven thickness portion 5 is necessarily selected at a position near the rotation center axis OL.
【0021】しかるに、アンバランス修正量の大きさ
は、偏肉部5の重量Wと、偏肉部5重心から回転中心軸
OLに至る距離Lbとの積(W×Lb)で決定される。However, the magnitude of the unbalance correction amount is determined by the product (W × Lb) of the weight W of the uneven thickness portion 5 and the distance Lb from the center of gravity of the uneven thickness portion 5 to the rotation center axis OL.
【0022】上述したように、回転中心軸OL近傍に偏
肉部5を備えると、偏肉部5重心と回転中心軸OLとの
距離Lbが必然的に小さくなり、その分、偏肉部5の重
量Wを大にしなければならない。したがって、材料コス
トの増大を招き、成形が困難になる不具合がともなわれ
る。As described above, when the uneven thickness portion 5 is provided near the rotation center axis OL, the distance Lb between the center of gravity of the uneven thickness portion 5 and the rotation center axis OL is inevitably reduced. Must be large. Therefore, there is a problem that the material cost is increased and molding is difficult.
【0023】また、回転中心軸OL近傍に偏肉部5を設
けるため、仕切板2を中空構造にすることができず、必
要以上にファン重量が増加し、材料費の増大、ファン回
転の慣性モーメントの増大およびファン回転に必要なエ
ネルギが増大する。併せて、送風効率の悪化と、送風時
における仕切板2壁面の粘性による圧力損失の増大およ
び風量の低下につながってしまう。Further, since the uneven thickness portion 5 is provided in the vicinity of the rotation center axis OL, the partition plate 2 cannot be formed in a hollow structure, so that the fan weight increases more than necessary, the material cost increases, and the inertia of the fan rotation increases. The energy required for the increase of the moment and the rotation of the fan increases. At the same time, the ventilation efficiency is deteriorated, the pressure loss due to the viscosity of the partition plate 2 wall surface at the time of ventilation is increased, and the air volume is reduced.
【0024】本発明は、このような事情によりなされた
ものであり、その目的とするところは、偏肉部を仕切板
と一体に備えるという基本構成を変えずに、偏肉部が超
音波溶着手段としてのホーンと全く接触せず、偏肉量を
小さくすることが可能であり、仕切板を中空構造にで
き、必要以上の重量増加を防止して、材料費の削減およ
び送風効率の向上を図れる横流ファンを提供しようとす
るものである。The present invention has been made in view of such circumstances, and it is an object of the present invention to provide an ultrasonic welding method without changing the basic structure in which the uneven thickness portion is provided integrally with the partition plate. No contact with the horn as a means, it is possible to reduce the thickness unevenness, the partition plate can be hollow structure, prevent unnecessary weight increase, reduce material costs and improve air blowing efficiency It is intended to provide a cross flow fan that can be achieved.
【0025】[0025]
【課題を解決するための手段】上記目的を達成するため
本発明は、軸方向に所定間隔を存して複数枚の仕切板を
配置し、これら仕切板間に、かつ仕切板の周端部で、こ
の周方向に沿って、互いの配列ピッチが複数種の長さの
組み合わせに設定されたブレードを介在し、上記仕切板
の一側面に上記ブレードが一体に突設される多翼型羽根
車を、複数個備え、一方の多翼型羽根車の仕切板に他方
の多翼型羽根車のブレードを当接するとともに、超音波
溶着手段によって互いの多翼型羽根車を連結固定して構
成される横流ファンにおいて、上記多翼型羽根車の仕切
板で、かつブレードが位置する側面と同一の側面部位
に、回転軸回りのアンバランスを吸収するための偏肉部
を設けたことを特徴とする横流ファンである。SUMMARY OF THE INVENTION In order to achieve the above object, the present invention comprises a plurality of partition plates arranged at predetermined intervals in an axial direction, and between the partition plates and at the peripheral end of the partition plate. In this circumferential direction, a multi-blade type blade is provided in which blades whose arrangement pitch is set to a combination of a plurality of lengths are interposed, and the blade is integrally provided on one side surface of the partition plate. A plurality of wheels are provided, and the blades of the other blade are brought into contact with the partition plate of one blade, and the blades of the blade are connected and fixed by ultrasonic welding means. The cross flow fan is characterized in that an uneven thickness portion for absorbing imbalance around the rotation axis is provided on a partition plate of the multi-blade type impeller and on the same side surface as the side surface where the blade is located. It is a cross flow fan.
【0026】[0026]
【作用】偏肉部を、仕切板の、ブレードが位置する側面
と同一の側面部位に設けたので、多翼型羽根車相互を超
音波溶着する際に、ホーンが偏肉部に接触しない。Since the uneven thickness portion is provided on the same side surface of the partition plate as the side surface on which the blade is located, the horn does not contact the uneven thickness portion when the multi-blade impellers are ultrasonically welded to each other.
【0027】したがって、偏肉部は、ブレード寄りの周
端部に近い位置を選択することができ、回転中心軸との
距離を大きくとれる。偏肉量を小さくできて、アンバラ
ンス調整工数が低減する。Therefore, the position of the uneven thickness portion can be selected at a position close to the peripheral end near the blade, and the distance from the rotation center axis can be increased. The thickness deviation can be reduced, and the number of man-hours for unbalance adjustment is reduced.
【0028】偏肉部がブレード寄りになるから、仕切板
を中空構造にすることができ、ファン全体の重量削減に
つなげられる。Since the uneven thickness portion is closer to the blade, the partition plate can have a hollow structure, which leads to a reduction in the weight of the entire fan.
【0029】[0029]
【実施例】以下、本発明の一実施例を図面にもとづいて
説明する。An embodiment of the present invention will be described below with reference to the drawings.
【0030】横流ファンの基本的な形状構成は、先に図
5(A)で説明した通りである。The basic configuration of the cross flow fan is as described above with reference to FIG.
【0031】そしてまた、先に図6で説明したように、
各ブレード3…は、弦長や曲率半径等の形状構造が同一
であるが、互いに隣接するブレード3,3相互間と中心
点Oとでなす角度θが、互いに異なる(θ1 ≠θ 2≠θ
3 …)よう設定され、ブレード3の周方向に沿う配列ピ
ッチが、不等であることを前提とする。Further, as described above with reference to FIG.
Each blade 3 has the same shape and structure, such as a chord length and a radius of curvature, but the angles θ formed between the adjacent blades 3 and 3 and the center point O are different from each other (θ 1 ≠ θ 2 ≠). θ
3 ...) And the arrangement pitch along the circumferential direction of the blade 3 is assumed to be unequal.
【0032】図1に示すように、横流ファン製造工程に
あたって、予め、仕切板2Aと、この仕切板2Aの一側
面に複数枚のブレード3…を、一体に突出してなる、多
翼型羽根車4Aを製作する。As shown in FIG. 1, in the process of manufacturing the cross flow fan, a multi-blade type impeller in which a partition plate 2A and a plurality of blades 3 are integrally protruded on one side surface of the partition plate 2A in advance. Build 4A.
【0033】ここで、上記仕切板2Aは、後述する理由
から中空構造をなす。Here, the partition plate 2A has a hollow structure for the reason described later.
【0034】さらに、仕切板2Aのブレード3が突設さ
れる面と同一の側面には、バランサとしての偏肉部5A
が一体に設けられる。Further, on the same side surface as the surface on which the blade 3 of the partition plate 2A protrudes, an uneven thickness portion 5A as a balancer is provided.
Are provided integrally.
【0035】換言すれば、ブレード3の近傍に偏肉部5
Aが設けられており、この偏肉部5Aの重心と多翼型羽
根車4Aの回転中心軸OLとの距離Laを、可能な限り
大にとることができる。In other words, the uneven thickness portion 5 is located near the blade 3.
A is provided, and the distance La between the center of gravity of the uneven thickness portion 5A and the rotation center axis OL of the multi-blade impeller 4A can be made as large as possible.
【0036】アンバランス修正量の大きさは、偏肉部5
Aの重量Wと、偏肉部5A重心から回転中心軸OLに至
る距離Laとの積(W×La)で決定される。The magnitude of the unbalance correction amount depends on the uneven thickness 5
It is determined by the product (W × La) of the weight W of A and the distance La from the center of gravity of the uneven thickness portion 5A to the rotation center axis OL.
【0037】本発明構成では、偏肉部5A重心と回転中
心軸OLとの距離Laを可能な限り大したので、その結
果、偏肉量を小さくすることができ、アンバランス修正
量が小さくてすむ。In the structure of the present invention, the distance La between the center of gravity of the uneven thickness portion 5A and the rotation center axis OL is made as large as possible. As a result, the thickness unevenness can be reduced, and the unbalance correction amount can be reduced. Yes.
【0038】また、偏肉部5Aをブレード3近傍の周端
部寄りの位置に設けるので、仕切板2Aの中心軸部分は
特に板部を必要としない。すなわち、中空部10を有す
る中空構造にできる。偏肉部5Aの重量が小さくなると
ともに、仕切板2Aを中空構造にしたので、ファン全体
の重量の低減が得られる。Further, since the uneven thickness portion 5A is provided at a position near the peripheral end near the blade 3, the central axis portion of the partition plate 2A does not need any particular plate portion. That is, a hollow structure having the hollow portion 10 can be obtained. Since the weight of the uneven thickness portion 5A is reduced and the partition plate 2A has a hollow structure, the weight of the entire fan can be reduced.
【0039】横流ファンの製造に当たって、多翼型羽根
車4Aを上下に積み重ね、超音波溶着手段としてのホー
ンHを上部側羽根車4Aの仕切板2に当接して、超音波
エネルギを付与する。先に、図5(B)で説明したのと
同一の作業をなす。In manufacturing the cross flow fan, the multi-blade type impellers 4A are stacked up and down, and a horn H as an ultrasonic welding means is brought into contact with the partition plate 2 of the upper side impeller 4A to apply ultrasonic energy. First, the same operation as described with reference to FIG.
【0040】超音波エネルギは、上部ブレード3の先端
縁と、下部仕切板2Aとの当接部に集中し、互いの超音
波溶着がなされるわけだが、このとき、偏肉部5Aがホ
ーンHの当接側に設けられていないから、偏肉部5Aが
ホーンHの邪魔にならない。超音波エネルギが偏肉部5
Aに集中することがなく、所定の必要箇所に確実に集中
する。The ultrasonic energy is concentrated on the contact portion between the tip edge of the upper blade 3 and the lower partition plate 2A, and the ultrasonic welding is performed. At this time, the uneven thickness portion 5A has the horn H The uneven thickness portion 5A does not interfere with the horn H. Ultrasonic energy is uneven part 5
Instead of concentrating on A, it is surely concentrated on a predetermined necessary place.
【0041】図3(A)に、このような構造の仕切板2
Aを有する横流ファンを回転駆動した際の、吹出側に形
成される風速ベクトルを示す。これは、仕切板2Aに中
空部10を有することにより得られる結果であり、送風
量が極めて大であることが分かる。FIG. 3A shows a partition plate 2 having such a structure.
7 shows a wind speed vector formed on the blow-out side when the cross flow fan having A is rotationally driven. This is a result obtained by having the hollow portion 10 in the partition plate 2A, and it can be seen that the blowing amount is extremely large.
【0042】図3(B)は、従来の、中空構造を採用で
きない、1枚ものの仕切板2を備えた横流ファンにおけ
る風速ベクトルを示す。本発明構造のファンと比較し
て、送風量が小であることが分かる。FIG. 3B shows a wind velocity vector in a conventional cross flow fan provided with one partition plate 2 which cannot employ a hollow structure. It can be seen that the air volume is smaller than that of the fan of the present invention.
【0043】図4(A)は、ファン直径Daφが小さい
場合の、多翼型羽根車4Aa相互を超音波溶着する状態
を示す。FIG. 4A shows a state in which the multi-blade impellers 4Aa are ultrasonically welded to each other when the fan diameter Da φ is small.
【0044】図4(B)は、ファン直径Dbφが大きい
場合の、多翼型羽根車4Ab相互を超音波溶着する状態
を示す。[0044] FIG. 4 (B) shows the case where the fan diameter Db phi is large, the multi-blade impeller 4Ab mutual state of ultrasonic welding.
【0045】いずれのファン直径Daφ,Dbφのもの
であっても、必要な偏肉部5Aa,5Abはブレード3
a,3b側に一体に設けられており、ホーンHがあてが
われる仕切板2Aa,2Ab側にはないので、全く同一
のホーンHを使っての超音波溶着が可能である。Regardless of the fan diameter Da φ , Db φ , the necessary uneven thickness portions 5Aa, 5Ab
Since the horns H are provided integrally and are not provided on the partition plates 2Aa and 2Ab sides to which the horns H are applied, ultrasonic welding using the same horns H is possible.
【0046】[0046]
【発明の効果】以上説明したように本発明によれば、多
翼型羽根車の仕切板で、ブレードが位置する側面と同一
の側面部位に、回転軸回りのアンバランスを吸収するた
めの偏肉部を設けたから、偏肉部を仕切板と一体に備え
るという基本構成を変えることなく、偏肉部が超音波溶
着手段としてのホーンと全く接触せずにすむ。As described above, according to the present invention, in the partition plate of the multi-blade type impeller, an unbalanced portion for absorbing imbalance around the rotation axis is provided on the same side surface as the side surface where the blade is located. Since the thick portion is provided, the uneven thickness portion does not need to contact the horn as the ultrasonic welding means at all without changing the basic configuration of integrally providing the uneven thickness portion with the partition plate.
【0047】したがって、偏肉部の重量を小さくできる
とともに、仕切板を中空構造にでき、ファンとして必要
以上の重量増加を防止し、材料費の削減および送風効率
の向上を図れるなどの効果を奏する。Therefore, the weight of the uneven thickness portion can be reduced, and the partition plate can have a hollow structure, so that the weight of the fan can be prevented from increasing more than necessary, and the effects such as reduction of material costs and improvement of blowing efficiency can be achieved. .
【図面の簡単な説明】[Brief description of the drawings]
【図1】本発明の一実施例を示す、横流ファンを構成す
る多翼型羽根車の斜視図。FIG. 1 is a perspective view of a multi-blade impeller constituting a cross flow fan according to an embodiment of the present invention.
【図2】(A)は、同実施例を示す、多翼型羽根車の縦
断面図。(B)は、多翼型羽根車の概略の底面図。FIG. 2A is a longitudinal sectional view of the multi-blade impeller, showing the embodiment. (B) is a schematic bottom view of the multi-blade impeller.
【図3】(A)は、同実施例の、横流ファンの風速ベク
トルを現す図。(B)は、従来構造の、横流ファンの風
速ベクトルを現す図。FIG. 3A is a diagram illustrating a wind speed vector of a cross flow fan according to the embodiment. (B) is a figure showing the wind velocity vector of a cross flow fan of a conventional structure.
【図4】(A),(B)は、互いに異なるファン直径の
多翼型羽根車相互を超音波溶着する説明図。FIGS. 4A and 4B are explanatory diagrams of ultrasonic welding of multi-blade impellers having different fan diameters from each other.
【図5】(A)は、一般的な横流ファンの斜視図。
(B)は、多翼型羽根車相互を超音波溶着する説明図。FIG. 5A is a perspective view of a general cross flow fan.
(B) is an explanatory view of ultrasonic welding of multi-blade type impellers.
【図6】横流ファンのブレードピッチを説明する図。FIG. 6 is a diagram illustrating a blade pitch of a cross flow fan.
【図7】(A)は、従来構造の、多翼型羽根車の縦断面
図。(B)は、多翼型羽根車の概略の底面図。FIG. 7A is a longitudinal sectional view of a conventional multi-blade impeller. (B) is a schematic bottom view of the multi-blade impeller.
【図8】従来構造の、多翼型羽根車相互を超音波溶着す
る説明図。FIG. 8 is an explanatory view of ultrasonic welding of a multi-blade type impeller of a conventional structure.
2A…仕切板、3…ブレード、4A…多翼型羽根車、H
…超音波溶着手段(ホーン)、5A…偏肉部。2A: partition plate, 3: blade, 4A: multi-blade impeller, H
... Ultrasonic welding means (horn), 5A.
Claims (1)
枚の仕切板と、これら仕切板間に介在され、かつ仕切板
の周端部で、この周方向に沿って、互いの配列ピッチが
複数種の長さの組み合わせに設定されたブレードとを具
備し、上記仕切板の一側面に上記ブレードが一体に突設
される多翼型羽根車を、複数個備え、一方の多翼型羽根
車の仕切板に他方の多翼型羽根車のブレードを当接する
とともに、超音波溶着手段によって互いの多翼型羽根車
を連結固定して構成される横流ファンにおいて、上記多
翼型羽根車の仕切板で、かつブレードが位置する側面と
同一の側面部位に、回転軸回りのアンバランスを吸収す
るための偏肉部を設けたことを特徴とする横流ファン。1. A plurality of partition plates disposed at predetermined intervals in an axial direction, and a plurality of partition plates interposed between the partition plates and at a peripheral end of the partition plates along the circumferential direction. A plurality of multi-blade type impellers, the arrangement pitch of which is set to a combination of a plurality of lengths; In the cross flow fan configured by abutting the blade of the other multi-blade impeller on the partition plate of the vane-type impeller and connecting and fixing the multi-blade impeller to each other by ultrasonic welding means, A cross flow fan, wherein an uneven wall portion for absorbing imbalance around a rotation axis is provided on a partition plate of an impeller and at the same side surface portion as a side surface where a blade is located.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP04325651A JP3106165B2 (en) | 1992-12-04 | 1992-12-04 | Cross flow fan |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP04325651A JP3106165B2 (en) | 1992-12-04 | 1992-12-04 | Cross flow fan |
Publications (2)
Publication Number | Publication Date |
---|---|
JPH06173885A JPH06173885A (en) | 1994-06-21 |
JP3106165B2 true JP3106165B2 (en) | 2000-11-06 |
Family
ID=18179204
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP04325651A Expired - Fee Related JP3106165B2 (en) | 1992-12-04 | 1992-12-04 | Cross flow fan |
Country Status (1)
Country | Link |
---|---|
JP (1) | JP3106165B2 (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP5704139B2 (en) * | 2012-09-04 | 2015-04-22 | ダイキン工業株式会社 | Cross flow fan |
-
1992
- 1992-12-04 JP JP04325651A patent/JP3106165B2/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
JPH06173885A (en) | 1994-06-21 |
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