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JPH0658116B2 - Blower - Google Patents
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JPH0658116B2 - Blower - Google Patents

Blower

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Publication number
JPH0658116B2
JPH0658116B2 JP18460686A JP18460686A JPH0658116B2 JP H0658116 B2 JPH0658116 B2 JP H0658116B2 JP 18460686 A JP18460686 A JP 18460686A JP 18460686 A JP18460686 A JP 18460686A JP H0658116 B2 JPH0658116 B2 JP H0658116B2
Authority
JP
Japan
Prior art keywords
hub
flow
impeller
blade
angle
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 - Lifetime
Application number
JP18460686A
Other languages
Japanese (ja)
Other versions
JPS6341698A (en
Inventor
輝彦 友広
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.)
Panasonic Holdings Corp
Original Assignee
Matsushita Electric Industrial 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 Matsushita Electric Industrial Co Ltd filed Critical Matsushita Electric Industrial Co Ltd
Priority to JP18460686A priority Critical patent/JPH0658116B2/en
Publication of JPS6341698A publication Critical patent/JPS6341698A/en
Publication of JPH0658116B2 publication Critical patent/JPH0658116B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Description

【発明の詳細な説明】 産業上の利用分野 本発明は、空気調和装置等に用いられている斜流羽根車
を使った送風装置に関するものである。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an air blower using a mixed flow impeller used in an air conditioner or the like.

従来の技術 従来、斜流羽根車にはハブの傾斜に沿った方向へ吐出さ
れる斜流ディフューザが用いられることが多く、羽根形
状はステパノフやフライデラらの示した線図や経験式を
用いて設計されてきた。その手順を図を用いて説明す
る。第5図に示すように、羽根1のメリディアン形状を
決定し、ハブ2からチップ3までの流路を等流量になる
ように、複数の流路に分割する。その等流量分割線4を
母線とし、中心軸まわりに回転して得られる円錐面を回
転流面と考え、この面上の2次元流れをもとにして羽根
の反り線を決定する。回転流面の展開図(第6図)を用
いて説明すると、入口では空気の流入角β′と羽根の
入口角βが大きくずれていると空気が羽根に沿って流
れず、乱れが大きくなり性能が低下する。したがって、
β′にほぼ一致するようにβを決めるのが一般的で
ある。普通、β′は羽根車の回転数、流量および入口
半径より推測される値を用いるので、βは半径rにに
よって第7図に示すよのにハブ側で大きく、チップ側で
小さくなるように変化する。
Conventional technology Conventionally, a mixed flow diffuser that discharges in the direction along the inclination of the hub is often used for mixed flow impellers, and the shape of the blades is determined using the diagrams and empirical formulas shown by Stepanov and Fredera. Has been designed. The procedure will be described with reference to the drawings. As shown in FIG. 5, the meridian shape of the blade 1 is determined, and the flow path from the hub 2 to the tip 3 is divided into a plurality of flow paths so that the flow rate becomes equal. The equal flow rate dividing line 4 is used as a generatrix, and a conical surface obtained by rotating around the central axis is considered as a rotating flow surface, and the warp line of the blade is determined based on the two-dimensional flow on this surface. To explain with reference to development of the rotating flow surfaces (Figure 6), when the inlet entrance angle beta 1 of inflow angle beta '1 and the blade of air greatly deviate the air does not flow along the blade, it is disturbed It becomes large and the performance deteriorates. Therefore,
It is general to determine β 1 so as to almost coincide with β ′ 1 . Normally, beta '1 is the rotational speed of the impeller, so using the values deduced from the flow rate and inlet radius, beta 1 is large at the hub side to by that shown in FIG. 7 by the radius r, smaller chip side To change.

一方、羽根の出口角βは必要とする全圧上昇を満たす
ように決定される。すなわち、第6図に示すような流れ
を生じている場合、全圧ヘッドΔHtは ただし、η…効率 g…重力加速度(m/sec2) Cu2…絶対速度の周方向成分(m/sec) U…外周の周速度(m/sec) で与えられる。ここで、Cuは次式で表わされる。
On the other hand, the blade outlet angle β 2 is determined so as to satisfy the required total pressure increase. That is, when the flow shown in FIG. 6 is generated, the total pressure head ΔHt is However, η ... Efficiency g ... Gravitational acceleration (m / sec 2 ), Cu2 ... Circumferential component of absolute velocity (m / sec) U 2, ... Here, Cu 2 is represented by the following equation.

Cu=U−Cm/tanβ ただし、Cm…絶対速度の半径方向成分(m/sec) したがって、流量、回転数、全圧ヘッドおよび半径位置
が決まればηを適当に仮定することによってβが求め
られる。このβも前述のβと同様に一般の斜流羽根
車ではハブ側で大きく、チップ側で小さく変化する。
Cu 2 = U 2 −Cm 2 / tan β 2 However, Cm 2 ... Radial direction component of absolute velocity (m / sec) Therefore, if flow rate, rotation speed, total pressure head and radial position are determined, η should be properly assumed. Yields β 2 . Similar to β 1 described above, β 2 is also large on the hub side and small on the tip side in a general mixed flow impeller.

次に展開面上においいて、上記のβ、βを満足する
ように入口側と出口側を一円孤でつなぎ、これを羽根の
反り線とする。
Next, on the developed surface, the inlet side and the outlet side are connected by a single arc so as to satisfy the above β 1 and β 2 , and this is used as the warp line of the blade.

以上のようにして、1つの回転流面上で決定される羽根
反り線の形状をハブからチップまでの各々の回転流面上
において求め、それらをなめらかにつなぐことによって
羽根の形状を定めていた。
As described above, the shape of the blade warp line determined on one rotating flow surface was determined on each rotating flow surface from the hub to the tip, and the blade shape was determined by connecting them smoothly. .

発明が解決しようとする問題点 しかしながら、流れを半径方向に吐出する遠心ディフュ
ーザを用いた場合、翼間全体の流れがチップ側により、
流れの半径方向成分が増加するため、前述のように斜流
ディフューザに合わせて設計された斜流羽根車では十分
な性能が発揮できなかった。すなわち、遠心ディフュー
ザを用いると、羽根車のハブ側を流れる流量が減少し、
チップ側の流量が増加する傾向がある。したがって、ハ
ブ側では流れの剥離が生じやすくなり、チップ側では有
効なヘッドが得られずに性能が低下するという問題を有
していた。
DISCLOSURE OF THE INVENTION Problems to be Solved by the Invention However, when a centrifugal diffuser that discharges a flow in a radial direction is used, the entire flow between blades is more
As the radial component of the flow increases, the mixed flow impeller designed for the mixed flow diffuser as described above could not exhibit sufficient performance. That is, using a centrifugal diffuser reduces the flow rate on the hub side of the impeller,
The flow rate on the tip side tends to increase. Therefore, there is a problem that flow separation is likely to occur on the hub side, and an effective head cannot be obtained on the chip side, resulting in deterioration of performance.

本発明はかかる従来の問題を解消するもので、遠心ディ
フューザと組み合せた場合に最適な性能を示す斜流羽根
車を提供することを目的とする。
The present invention solves such a conventional problem, and an object of the present invention is to provide a mixed flow impeller that exhibits optimum performance when combined with a centrifugal diffuser.

問題点を解決するための手段 上記問題点を解決するために本発明の送風装置は、略円
錐台形のハブとそのハブの斜面上に設けられた複数枚の
羽根を備え、その羽根の入口角はハブ側からチップ側へ
いくに従って小さくし、出口角はハブ側からチップ側ま
でほぼ一定とし、かつ、羽根の前縁から後縁までの反り
線を一円弧曲線とした斜流羽根車と流れを半径方向に吐
出する遠心ディフューザを組み合せた構成をとってい
る。
Means for Solving the Problems In order to solve the above problems, a blower device of the present invention includes a substantially frustoconical hub and a plurality of blades provided on an inclined surface of the hub, and an inlet angle of the blade. Is smaller from the hub side to the tip side, the exit angle is almost constant from the hub side to the tip side, and the flow line from the mixed flow impeller with the curved line from the leading edge to the trailing edge of the blade is a circular arc curve. The centrifugal diffuser which discharges in the radial direction is combined.

作 用 本発明の羽根車においては、羽根の出口角をハブからチ
ップまでほぼ一定にしたため、従来の出口角と比べると
ハブ側で小さく、チップ側で大きくなっている。一方、
遠心ディフューザを用いたときの翼間の流量分布はハブ
側で少なく、チップ側で多くなる傾向がある。したがっ
て、流量の減ったところで出口角が小さくなり、流量の
増えたところで出口角が大きくなるので、有効なヘッド
はあまり変化することなく、高性能が得られる。
Operation In the impeller of the present invention, the outlet angle of the blade is substantially constant from the hub to the tip, so that it is smaller on the hub side and larger on the tip side than the conventional outlet angle. on the other hand,
When a centrifugal diffuser is used, the flow rate distribution between blades tends to be small on the hub side and large on the tip side. Therefore, the outlet angle becomes smaller when the flow rate decreases and becomes larger when the flow rate increases, so that the effective head does not change much and high performance can be obtained.

実施例 以下、本発明の実施例を添付図面にもとづいて説明す
る。第1図において、5は斜流羽根車で、6がハブ、7
が羽根である。斜流羽根車がモータ8によって駆動され
ると、矢印aで示すように吸込口9より空気が流入し、
斜流羽根車5を通過した後遠心ディフューザ部10を半
径方向に曲げられて外部へ吐出される。
Embodiments Embodiments of the present invention will be described below with reference to the accompanying drawings. In FIG. 1, 5 is a mixed flow impeller, 6 is a hub, and 7
Is a feather. When the mixed flow impeller is driven by the motor 8, air flows in through the suction port 9 as indicated by the arrow a,
After passing through the mixed flow impeller 5, the centrifugal diffuser portion 10 is bent in the radial direction and discharged to the outside.

第2図は本発明の斜流羽根車の出口角と従来の斜流羽根
車の出口角の半径Rによる変化を比較したものである。
本発明における出口角はハブ側からチップ側までほぼ一
定となっているので、従来例と比較するとハブ側で小さ
く、チップ側で大きくなっている。これらの角度変化と
翼間の流量変化の関係について、第3図(a)(b)を用いて
説明する。まず、ハブ側についてみると、遠心ディフュ
ーザを用いることによって流量が減少するのでCm
に変化する。ところが、出口角βもβ*と小さくし
てあるため、絶対速度の周方向成分Cuはほとんど変
化なく、最適な流れ状態が保たれる。一方、第3図(b)
に示したチップ側についてみると、遠心ディフューザに
よってチップ側の流量が増加するので、CmがCm
*と増加するのに合わせて出口角βもβ*と大きく
なっているので、やはりCuはあまり変化なく、最適
な流れが保たれることになる。
FIG. 2 compares the exit angle of the mixed flow impeller of the present invention and the exit angle of the conventional mixed flow impeller with the radius R.
Since the outlet angle in the present invention is almost constant from the hub side to the tip side, it is smaller on the hub side and larger on the tip side as compared with the conventional example. The relationship between these angle changes and the flow rate changes between the blades will be described with reference to FIGS. 3 (a) and 3 (b). First, looking at the hub side, the flow rate is reduced by using a centrifugal diffuser, so Cm 2 *
Changes to. However, since the outlet angle β 2 is also as small as β 2 *, the circumferential component Cu 2 of the absolute velocity hardly changes and the optimum flow state is maintained. On the other hand, FIG. 3 (b)
As for the tip side shown in Fig. 2 , since the flow rate on the tip side is increased by the centrifugal diffuser, Cm 2 is equal to Cm 2
Since the outlet angle β 2 also increases to β 2 * as it increases with *, Cu 2 does not change so much, and the optimum flow is maintained.

第4図に本発明の斜流羽根車実線と従来の斜流羽根車破
線の特性を比較したグラフを示す。この図によれば、全
流量域において、本発明の斜流羽根車が従来と同程度以
上の性能を示していることがわかる。
FIG. 4 shows a graph comparing the characteristics of the solid line of the mixed flow impeller of the present invention and the broken line of the conventional mixed flow impeller. According to this figure, it is understood that the mixed flow impeller of the present invention exhibits the same or higher performance as the conventional one in the entire flow rate range.

発明の効果 以上のように本発明の斜流送風装置では羽根出口角をほ
ぼ一定にしたことによって、遠心ディフューザを用いて
ハブ側の流量が減少し、チップ側の流量が減少した場合
にも最適な流れ状態を保つことができるので、羽根車の
性能が十分に発揮されるという効果が得られる。
Effect of the Invention As described above, in the mixed-flow fan of the present invention, by making the blade outlet angle almost constant, the flow rate on the hub side is reduced by using the centrifugal diffuser, and it is optimal even when the flow rate on the tip side is reduced. Since such a flow state can be maintained, the effect that the performance of the impeller is sufficiently exhibited is obtained.

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

第1図は本発明の一実施例における送風装置の断面図、
第2図は本発明の斜流羽根車の出口角と従来例の出口角
の半径Rによる変化を比較して示した特性図、第3図
(a)はハブ側における流量と出口角の変化の特性図、第
3図(b)はチップ側における同特性図、第4図は本発明
の送風装置と従来の送風装置の特性を比較した特性図、
第5図は斜流羽根車のメリディアン図、第6図は羽根の
反り線形状の決定方法を説明する回転流面の展開図、第
7図は入口角の半径Rによる変化を示す特性図である。 5……斜流羽根車、6……ハブ、7……羽根、 9……吸込口、10……遠心ディフューザ部、
FIG. 1 is a sectional view of an air blower according to an embodiment of the present invention,
FIG. 2 is a characteristic diagram showing a comparison between the exit angle of the mixed flow impeller of the present invention and the exit angle of the conventional example depending on the radius R, and FIG.
(a) is a characteristic diagram of changes in the flow rate and outlet angle on the hub side, FIG. 3 (b) is the same characteristic diagram on the tip side, and FIG. 4 compares the characteristics of the air blower of the present invention and the conventional air blower. Characteristic diagram,
FIG. 5 is a meridian diagram of a mixed flow impeller, FIG. 6 is a development diagram of a rotating flow surface for explaining a method of determining a curved line of a blade, and FIG. 7 is a characteristic diagram showing a change of an inlet angle with a radius R. is there. 5 ... Mixed flow impeller, 6 ... Hub, 7 ... Blade, 9 ... Suction port, 10 ... Centrifugal diffuser part,

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】略円錐台形のハブとこのハブの斜面上に設
けられた複数枚の羽根を備え、この羽根の入口角はハブ
側からチップ側へいくに従って小さくし、出口角はハブ
側からチップ側までほぼ一定とし、かつ、羽根の前縁か
ら後縁までの反り線を一円弧曲線とした斜流羽根車の吸
込側に吸込口を設け、吐出側には、軸方向に流入した流
れを半径方向に曲げて吐出する遠心ディフューザ部を有
する送風装置。
1. A hub having a substantially frusto-conical shape and a plurality of blades provided on the slope of the hub. The inlet angle of the blade is reduced from the hub side toward the tip side, and the outlet angle is measured from the hub side. A suction port is provided on the suction side of the mixed flow impeller with the curvature line from the front edge to the rear edge of the vane being one arc curve, and on the discharge side, the flow that flows in the axial direction. An air blower having a centrifugal diffuser portion that bends and discharges air.
JP18460686A 1986-08-06 1986-08-06 Blower Expired - Lifetime JPH0658116B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP18460686A JPH0658116B2 (en) 1986-08-06 1986-08-06 Blower

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP18460686A JPH0658116B2 (en) 1986-08-06 1986-08-06 Blower

Publications (2)

Publication Number Publication Date
JPS6341698A JPS6341698A (en) 1988-02-22
JPH0658116B2 true JPH0658116B2 (en) 1994-08-03

Family

ID=16156159

Family Applications (1)

Application Number Title Priority Date Filing Date
JP18460686A Expired - Lifetime JPH0658116B2 (en) 1986-08-06 1986-08-06 Blower

Country Status (1)

Country Link
JP (1) JPH0658116B2 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH01160197U (en) * 1988-04-19 1989-11-07
JP2544454B2 (en) * 1988-09-14 1996-10-16 株式会社日立製作所 Turbo compressor
JPH07103874B2 (en) * 1990-03-14 1995-11-08 株式会社日立製作所 Mixed flow compressor

Also Published As

Publication number Publication date
JPS6341698A (en) 1988-02-22

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