JPH045760Y2 - - Google Patents

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Publication number
JPH045760Y2
JPH045760Y2 JP1986068190U JP6819086U JPH045760Y2 JP H045760 Y2 JPH045760 Y2 JP H045760Y2 JP 1986068190 U JP1986068190 U JP 1986068190U JP 6819086 U JP6819086 U JP 6819086U JP H045760 Y2 JPH045760 Y2 JP H045760Y2
Authority
JP
Japan
Prior art keywords
fan
rotor blade
tip
stall
flow
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
JP1986068190U
Other languages
Japanese (ja)
Other versions
JPS62180700U (en
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 filed Critical
Priority to JP1986068190U priority Critical patent/JPH045760Y2/ja
Publication of JPS62180700U publication Critical patent/JPS62180700U/ja
Application granted granted Critical
Publication of JPH045760Y2 publication Critical patent/JPH045760Y2/ja
Expired legal-status Critical Current

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Description

【考案の詳細な説明】 産業上の利用分野 この考案は、軸流フアンの失速防止機構に関す
る。
[Detailed Description of the Invention] Industrial Application Field This invention relates to a stall prevention mechanism for an axial flow fan.

従来の技術 軸流フアンの失速防止機構の従来例に第3aお
よび3b図に図示するものがある。すなわち、回
動させられるハブ2に固設させてある軸流フアン
動翼1の外周に覆設したケーシング3において、
該動翼の先端に対向する前記ケーシングの部分に
動翼1の前縁先端付近から上流側に向けて凹所を
成形させて循環流路8を構成させ、該循環流路の
ほぼ中央部に多数の旋回防止ベーン5を突設させ
るとともに、該防止ベーンの内周側を夫々連結さ
せて円環7を固設させて前記防止ベーンの後流側
に後方キヤビテイ4を、また上流側に前方キヤビ
テイ6を形成させてなるものであつて、前記軸流
フアン動翼はその上流側から矢印Aの方向に空気
を送流させるとともに、前記循環流路内において
は動翼1の先端の流れの一部を点線図示の矢印B
の方向に循環させるようにしている。
BACKGROUND ART A conventional example of a stall prevention mechanism for an axial fan is shown in FIGS. 3a and 3b. That is, in the casing 3 covered around the outer periphery of the axial fan rotor blade 1 fixed to the hub 2 that is rotated,
A recess is formed in the part of the casing facing the tip of the rotor blade from near the tip of the leading edge of the rotor blade 1 toward the upstream side to form a circulation passage 8, and a recess is formed in the portion of the casing facing the tip of the rotor blade 1, and a recess is formed in the portion of the casing facing the tip of the rotor blade 1 to form a circulation passage 8. A large number of rotation prevention vanes 5 are provided protrudingly, and a ring 7 is fixedly installed by connecting the inner peripheral sides of the prevention vanes to form a rear cavity 4 on the downstream side of the prevention vanes, and a front cavity on the upstream side. The axial fan rotor blade sends air in the direction of arrow A from its upstream side, and in the circulation flow path, the flow at the tip of the rotor blade 1 is controlled. Arrow B partially shown in dotted line
I try to circulate it in the direction of.

前述した従来軸流フアンの失速防止機構の作用
は、前記循環流路内の循環流を安定的に生起させ
ることにより、フアン失速点の近傍において動翼
1の先端に蓄積される低エネルギ流れが逆流を起
こすようにさせて、フアン特性の劣化を防いでフ
アン失速を防止するものである。
The effect of the conventional axial fan stall prevention mechanism described above is to stably generate a circulating flow in the circulating flow path, thereby preventing the low-energy flow accumulated at the tip of the rotor blade 1 in the vicinity of the fan stall point. This prevents deterioration of fan characteristics and stalls the fan by causing backflow.

いま、従来失速防止機構をもつた軸流フアンの
失速防止状況を実験した結果を第4図において説
述すると、なお、該防止機構を備えないフアンの
結果をも併せて図示してあるが、その記号につい
てまず説明すれば、 Φを流量係数、Ψを圧力係数、Qをフアン流
量、Δpをフアン圧力上昇、Dをフアン直径、u
をフアン周速、ρを気流密度 であり、 Φ=Q/(π/4)・D2・u Ψ=Δp/(ρ/2)・u2 となるが、この係数による表示法では、フアンの
回転数の影響があらわれず、回転数を変化させて
取得したデータも一本の曲線で図示できて便利で
ある。同図によれば、従来失速防止機構を備えな
いフアンの性能曲線11は、失速点で圧力が急激
に低下するという欠点があることが知られるが、
他の曲線群12,13および14は、装備したフ
アンに係る性能曲線であつて、フアン回転数を低
速、中速および高速に順次上昇させると、失速改
善部分の特性が前記曲線12,13,14の順で
変化し、高速になるほど失速防止量が減少する、
すなわち失速が早くなる現象があり、その原因
は、明確ではないが、低速では装備した前記防止
機構のセパレータ内に流れが穏やかに流入して所
期の企図が達成されるのに、高速では乱れが大き
くなつて効果が減殺されるものと考えられるが、
フアンの計画時に、どの程度の失速マージンを考
慮すればよいか、解明するべき問題である。
Now, the results of an experiment on the stall prevention situation of an axial flow fan with a conventional stall prevention mechanism will be explained in Fig. 4.The results of a fan without the stall prevention mechanism are also shown. To explain the symbols first, Φ is the flow coefficient, Ψ is the pressure coefficient, Q is the fan flow rate, Δp is the fan pressure increase, D is the fan diameter, and u
is the fan circumferential speed and ρ is the airflow density, Φ=Q/(π/4)・D 2・u Ψ=Δp/(ρ/2)・u 2 However, when expressed using this coefficient, the fan The influence of the rotational speed does not appear, and data obtained by changing the rotational speed can be conveniently illustrated as a single curve. According to the same figure, it is known that the performance curve 11 of the conventional fan without a stall prevention mechanism has the disadvantage that the pressure suddenly decreases at the stall point.
Other curve groups 12, 13, and 14 are performance curves related to the equipped fan, and when the fan rotation speed is increased sequentially from low speed, medium speed, and high speed, the characteristics of the stall improvement portion change to the curves 12, 13, and 14. It changes in the order of 14, and the stall prevention amount decreases as the speed increases.
In other words, there is a phenomenon where the stall speeds up, and the reason for this is not clear, but at low speeds the flow flows gently into the separator of the prevention mechanism installed and the desired purpose is achieved, but at high speeds the flow is turbulent. It is thought that the effect will be diminished as the
The issue that needs to be clarified is how much stall margin should be considered when planning the fan.

考案の解決しようとする問題点 この考案は、失速点で圧力が急激に低下する欠
点を除くとともに、失速マージンの程度を推定で
きるようにすることにある。
Problems to be Solved by the Invention This invention aims to eliminate the drawback of a sudden drop in pressure at the stall point, and also to make it possible to estimate the extent of the stall margin.

問題点を解決するための手段 この考案は、軸流フアンの動翼の外周に覆設し
たケーシングにおいて、該動翼の先端に対向する
前記ケーシングの部分に動翼の前縁先端付近から
上流側に向けて凹所を成形させて循環流路を構成
させ、該循環流路内に旋回除去ベーンを、その一
端が下流側ケーシング内で終端しかつ周方向に並
列させてなるものである。
Means for Solving the Problem This invention is based on a casing covered around the outer periphery of a rotor blade of an axial flow fan, in which a portion of the casing opposite to the tip of the rotor blade is placed on the upstream side from near the leading edge tip of the rotor blade. A recess is formed to form a circulation flow path, and swirl removal vanes are arranged in the circulation flow path, one end of which terminates within the downstream casing, and are arranged in parallel in the circumferential direction.

作 用 したがつて、この考案の構成によれば、循環流
路内においてその旋回除去ベーンが循環気流の旋
回を除去するとともに、ついで軸方向に該気流を
転向させて導くことになる。
Therefore, according to the configuration of this invention, the swirl removal vane eliminates the swirl of the circulating airflow in the circulation flow path, and then turns and guides the airflow in the axial direction.

実施例 つぎに、この考案の実施例を図面について説明
すれば、第1a,1bおよび1c図において、軸
流フアンの動翼1の外周に覆設したケーシング3
の該動翼の先端に対向する部分に前記動翼の前縁
先端付近から上流に向けて凹所を成形させて循環
流路8を構成させ、該循環流路の内部の後流側の
最初の動翼1の先端部分に最も近い個所に多数の
旋回除去ベーン22を並列させるとともに、前記
除去ベーンの内周側の動翼1の先端に接触しない
部位に円環7を固設させて該除去ベーン夫々を連
結させ、さらに前記除去ベーンの上流側には前方
キヤビテイ6を形成させてなるものである。
Embodiment Next, an embodiment of this invention will be described with reference to the drawings. In FIGS. 1a, 1b and 1c, a casing 3 covered around the outer periphery of a rotor blade 1 of an axial flow fan is shown.
A recess is formed in the portion facing the tip of the rotor blade from near the leading edge tip of the rotor blade toward upstream to form a circulation flow path 8, A large number of swirl removal vanes 22 are arranged in parallel at a location closest to the tip of the rotor blade 1, and an annular ring 7 is fixed to a portion of the removal vane that does not contact the tip of the rotor blade 1 on the inner peripheral side. The removal vanes are connected to each other, and a front cavity 6 is formed upstream of the removal vanes.

したがつて、前述実施例によると、旋回除去ベ
ーン22の列は動翼1と同方向に回転する流れを
半径方向にすくい取つてその旋回流を除去させ、
このすくい取られて旋回流が除去された流れは、
第1a図に点線図示の矢印Cの方向の上流側に転
向させられ、ついで前方キヤビテイ6内を経て再
び主流(矢印A)に合流する。換言すれば、従来
機構の旋回防止ベーン5(第3aおよび3b図)
が軸方向流れにさせて旋回除去を行なつていた
が、この考案に係る旋回除去ベーン22は半径方
向流れの段階で旋回除去を行なうもので、すなわ
ち、従来機構の防止ベーン5の後流側の後方キヤ
ビテイ4に流れが流入する前に整流するようにし
たものである。
Therefore, according to the embodiment described above, the row of swirl removal vanes 22 radially scoops the flow rotating in the same direction as the rotor blade 1 to remove the swirl flow,
The flow from which this swirling flow has been removed is
It is turned upstream in the direction of arrow C shown in dotted lines in FIG. 1a, and then passes through the front cavity 6 and joins the main stream (arrow A) again. In other words, the rotation prevention vane 5 of the conventional mechanism (Figures 3a and 3b)
However, the swirl removal vane 22 according to this invention performs swirl removal at the stage of radial flow, that is, the swirl removal vane 22 of this invention performs swirl removal at the stage of radial flow. The flow is rectified before it flows into the rear cavity 4.

さらに、この考案に係る失速防止機構を備えた
軸流フアンの実験結果を前述した第4図と同様に
第2図によつて示すと、その性能曲線31は、前
述した性能曲線11に比較して失速防止効果が格
段に向上していることが知られるとともに安定化
しているから、フアンの大形、小形、あるいは回
転速度の高低を問わずに、フアン計画時に安心し
てその効果を考慮に入れることが可能である。
Furthermore, when the experimental results of the axial flow fan equipped with the stall prevention mechanism according to this invention are shown in FIG. 2 in the same manner as in FIG. It is known that the stall prevention effect is significantly improved and stabilized, so you can feel confident taking this effect into consideration when planning the fan, regardless of whether the fan is large or small, or whether the rotation speed is high or low. Is possible.

考案の効果 上述したように、この考案は、失速防止の効果
を格段に向上するとともに、安定した効果を実現
できるので計画が容易確実に行なえるから製品製
作上極めて好都合であるなど、実益の多大な考案
ということができる。
Effects of the invention As mentioned above, this invention greatly improves the effect of preventing stalls, and also provides a stable effect, making planning easier and more reliable, making it extremely convenient for product manufacturing. It can be said that this is a great idea.

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

第1a図は、この考案の実施例を示す要部の縦
断側面図、第1b図は、前図のY−Y切断面図、
第1c図は、同じく失速除去ベーンと動翼との相
関々係を示す要部の斜視図、第2図は、防止機構
のないフアンと従来機構をもつフアンの性能曲線
図、第3a図は、従来失速防止機構を備えた軸流
フアンの要部の縦断側面図、第3b図は、前図の
X−X切断面図、第4図は、失速防止機構を装備
しない軸流フアンおよびこの考案に係る軸流フア
ンの性能曲線図である。 1……動翼、3……ケーシング、4……後方キ
ヤビテイ、5……旋回防止ベーン、6……前方キ
ヤビテイ、7……円環、8……循環流路、11…
…一般フアン性能曲線、12,13,14……従
来機構をもつフアンの性能曲線(低速、中速,高
速)、31……この考案に係るフアンの性能曲線。
Fig. 1a is a vertical sectional side view of the main part showing an embodiment of this invention, Fig. 1b is a YY sectional view of the previous figure,
Figure 1c is a perspective view of the main parts showing the relationship between the stall removal vanes and the rotor blades, Figure 2 is a performance curve diagram of a fan without a prevention mechanism and a fan with a conventional mechanism, and Figure 3a is a diagram of the performance curves of a fan without a prevention mechanism and a fan with a conventional mechanism. , Fig. 3b is a cross-sectional view taken along the line X-X in the previous figure, and Fig. 4 is a longitudinal sectional side view of the main parts of an axial flow fan equipped with a conventional stall prevention mechanism. FIG. 3 is a performance curve diagram of the axial fan according to the invention. DESCRIPTION OF SYMBOLS 1... Moving blade, 3... Casing, 4... Rear cavity, 5... Rotation prevention vane, 6... Front cavity, 7... Annular ring, 8... Circulation channel, 11...
...Performance curve of a general fan, 12, 13, 14... Performance curve of a fan with a conventional mechanism (low speed, medium speed, high speed), 31... Performance curve of a fan according to this invention.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 軸流フアンの動翼の外周に覆設したケーシング
の該動翼の先端に対向する部分に動翼の前縁先端
付近から上流側に向けて凹所を成形させて循環流
路を構成させ、該循環流路内に旋回除去ベーン
を、その一端が下流側ケーシング内で終端し、か
つ周方向に並列させたことを特徴とする軸流フア
ンの失速防止機構。
Forming a recess from near the leading edge tip of the rotor blade toward the upstream side in a portion of the casing covered around the outer periphery of the rotor blade of the rotor blade facing the tip of the rotor blade to form a circulation flow path, A stall prevention mechanism for an axial fan, characterized in that swirl removal vanes are disposed in the circulation flow path, one end of which terminates within the downstream casing, and are arranged in parallel in the circumferential direction.
JP1986068190U 1986-05-08 1986-05-08 Expired JPH045760Y2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1986068190U JPH045760Y2 (en) 1986-05-08 1986-05-08

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1986068190U JPH045760Y2 (en) 1986-05-08 1986-05-08

Publications (2)

Publication Number Publication Date
JPS62180700U JPS62180700U (en) 1987-11-16
JPH045760Y2 true JPH045760Y2 (en) 1992-02-18

Family

ID=30907778

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1986068190U Expired JPH045760Y2 (en) 1986-05-08 1986-05-08

Country Status (1)

Country Link
JP (1) JPH045760Y2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2005264803A (en) * 2004-03-18 2005-09-29 Matsushita Electric Ind Co Ltd Blower, heat exchange unit using the blower, and refrigerator-freezer

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU1252553A1 (en) * 1982-07-29 1986-08-23 Донецкий государственный проектно-конструкторский и экспериментальный институт комплексной механизации шахт "Донгипроуглемаш" Axial-flow fan
JPS643839Y2 (en) * 1984-08-31 1989-02-01

Also Published As

Publication number Publication date
JPS62180700U (en) 1987-11-16

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