JP3411701B2 - Centrifugal blower - Google Patents

Centrifugal blower

Info

Publication number
JP3411701B2
JP3411701B2 JP02756395A JP2756395A JP3411701B2 JP 3411701 B2 JP3411701 B2 JP 3411701B2 JP 02756395 A JP02756395 A JP 02756395A JP 2756395 A JP2756395 A JP 2756395A JP 3411701 B2 JP3411701 B2 JP 3411701B2
Authority
JP
Japan
Prior art keywords
blade
main plate
centrifugal blower
impeller
side plate
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
Application number
JP02756395A
Other languages
Japanese (ja)
Other versions
JPH08200290A (en
Inventor
弘高 東森
英彦 伊高
栄人 松尾
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.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries 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 Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP02756395A priority Critical patent/JP3411701B2/en
Publication of JPH08200290A publication Critical patent/JPH08200290A/en
Application granted granted Critical
Publication of JP3411701B2 publication Critical patent/JP3411701B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Description

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

【0001】[0001]

【産業上の利用分野】本発明はうず巻状のスクロールケ
ーシング内に羽根車を配設してなる遠心送風機に関す
る。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a centrifugal blower having an impeller arranged in a spiral scroll casing.

【0002】[0002]

【従来の技術】図2及び図3には従来の片吸込型遠心送
風機の1例が示されている。図2において、02は電動モ
ータ等の駆動源により回転駆動される回転軸、01は回転
軸02に固定された羽根車、04はうず巻状のスクロールケ
ーシング、08は気体を羽根車01内に導くフローガイド、
012 はフローガイド08の外面とスクロール舌部010 との
間に形成された環状空間である。
2. Description of the Related Art FIG. 2 and FIG. 3 show an example of a conventional single suction centrifugal fan. In FIG. 2, 02 is a rotary shaft that is driven to rotate by a drive source such as an electric motor, 01 is an impeller fixed to the rotary shaft 02, 04 is a spiral scroll casing, and 08 is gas in the impeller 01. Flow guide,
Reference numeral 012 is an annular space formed between the outer surface of the flow guide 08 and the scroll tongue 010.

【0003】羽根車01は回転軸02に固定された円板状の
主板05と円錐状の側板06との間にその円周方向に沿って
等間隔を隔てて複数枚の翼03を固定してなる。
An impeller 01 has a plurality of blades 03 fixed at equal intervals along a circumferential direction between a disc-shaped main plate 05 fixed to a rotary shaft 02 and a conical side plate 06. It becomes.

【0004】しかして、この遠心送風機の運転時、羽根
車01が回転すると、気体がフローガイド08を経て羽根車
01内に導入され、その翼03により付勢された後スクロー
ルケーシング04内の渦室04a を流過して吐出口011 から
吹き出される。
When the impeller 01 rotates during operation of this centrifugal blower, gas passes through the flow guide 08 and the impeller
After being introduced into 01 and urged by its blades 03, it flows through the vortex chamber 04a in the scroll casing 04 and is blown out from the discharge port 011.

【0005】[0005]

【発明が解決しようとする課題】上記従来の遠心送風機
においては、図3(A) に示されるように、羽根車01の主
板05は回転軸02に直交し、側板06はその外周に向かうに
従って主板05に接近するように角度θ傾斜しているとと
もにフローガイド08の内面08a の曲率rが小さいため、
側板06寄りの流れの損失が主板05寄りのそれよりも大き
くなる。
In the above-mentioned conventional centrifugal blower, as shown in FIG. 3 (A), the main plate 05 of the impeller 01 is orthogonal to the rotary shaft 02, and the side plate 06 is directed toward the outer periphery thereof. Since the angle θ is inclined so as to approach the main plate 05 and the curvature r of the inner surface 08a of the flow guide 08 is small,
The flow loss near the side plate 06 becomes larger than that near the main plate 05.

【0006】従って、羽根車01内を気体が流れる際、B
−B断面、即ち、主板05寄りを流過した気体の圧力がC
−C断面、即ち、側板06寄りを流過した気体のそれより
も高くなる。この結果、主板05側から側板06側に向かう
2次流れBが生じ、この2次流れBは原理的には翼03の
圧力面03b 及び負圧面03a の両面に発生する。
Therefore, when the gas flows in the impeller 01, B
-B cross section, that is, the pressure of the gas flowing near the main plate 05 is C
-C cross section, that is, higher than that of gas flowing near the side plate 06. As a result, a secondary flow B from the main plate 05 side to the side plate 06 side is generated, and this secondary flow B is theoretically generated on both the pressure surface 03b and the suction surface 03a of the blade 03.

【0007】そして、2次流れBは図3(C) に白抜矢印
で示されるように、主板05側から側板06に向かって流れ
た後、翼03の前縁から負圧面03a へ回り込んで負圧面03
a 上に剥離Dを生じさせて遠心送風機の性能低下を引き
起こす。
Then, the secondary flow B flows from the main plate 05 side to the side plate 06, and then wraps around from the front edge of the blade 03 to the suction surface 03a, as shown by the white arrow in FIG. 3 (C). At negative pressure surface 03
a Peeling D occurs on the top, causing the performance of the centrifugal blower to deteriorate.

【0008】一方、C−C断面はB−B断面に対して角
度θ傾斜しているため、C−C断面の翼03の前縁におけ
る取付角αC(図3(C)参照)はB−B断面のそれα
B(図3(B)参照)よりも小さくなる。従って、気体が主
板05寄り及び側板06寄りに同じ流速で流入しても、C−
C断面の方がB−B断面よりも入射角が大きくなり、流
れの剥離や圧力損失が増大する。
On the other hand, since the CC cross section is inclined by the angle θ with respect to the BB cross section, the mounting angle α C (see FIG. 3C) at the leading edge of the blade 03 of the CC cross section is B. -That of section B α
It is smaller than B (see FIG. 3 (B)). Therefore, even if the gas flows into the main plate 05 side and the side plate 06 side at the same flow velocity, C-
The C-section has a larger incident angle than the BB-section, resulting in increased flow separation and pressure loss.

【0009】[0009]

【課題を解決するための手段】本発明は上記課題を解決
するために発明されたものであって、その要旨とすると
ころは、うず巻状のスクロールケーシング内に回転軸に
固定されてこれと直交する円板状の主板と外周に向かう
に従って上記主板に接近するように傾斜する円錐状の側
板との間にその円周方向に沿って等間隔を隔てて複数枚
の翼を固定してなる羽根車を配設してなる遠心送風機に
おいて、上記翼の前縁から前方に突出する補助翼を設
け、この補助翼の入口角を上記翼の入口角より小さくし
たことを特徴とする遠心送風機にある。
The present invention has been invented in order to solve the above-mentioned problems, and the gist of the present invention is to fix it to a rotary shaft in a spiral scroll casing. A plurality of blades are fixed at equal intervals along the circumferential direction between orthogonal disc-shaped main plates and conical side plates inclined so as to approach the main plate toward the outer periphery. In a centrifugal blower provided with an impeller, an auxiliary blade protruding forward from a front edge of the blade is provided, and an inlet angle of the auxiliary blade is smaller than an inlet angle of the blade. is there.

【0010】他の特徴とするところは、上記補助翼の突
出長さを上記側板から主板に向かうに従って漸減させた
ことにある。
Another feature is that the protruding length of the auxiliary blade is gradually reduced from the side plate toward the main plate.

【0011】[0011]

【作用】本発明においては、気体の翼に対する入射角が
主板寄り及び側板寄りでほぼ同一となるので、流れの剥
離や圧力損失の増加を防止しうる。
In the present invention, the incident angles of the gas with respect to the blade are almost the same on the main plate side and the side plate side, so that flow separation and pressure loss increase can be prevented.

【0012】[0012]

【実施例】図1には本発明の実施例に係る片吸込型遠心
送風機の羽根車が示され、(A)は軸心に沿う断面図、(B)
は(A) のB−B線に沿う断面図、(C) は(A) のC−C
線に沿う断面図である。
FIG. 1 shows an impeller of a single suction centrifugal fan according to an embodiment of the present invention.
Is a sectional view taken along the line BB of (A), and (C) is CC of (A).
It is sectional drawing which follows the line.

【0013】図1において、2は電動モータ等の駆動源
により回転駆動される回転軸、1は羽根車、5は回転軸
2にボス7を介して固定されて回転軸2に直交する円板
状の主板、6は円錐状の側板で、その外周に向かうに従
って主板5に接近するように角度θ傾斜している。
In FIG. 1, reference numeral 2 is a rotary shaft which is rotationally driven by a drive source such as an electric motor, 1 is an impeller, and 5 is a disk which is fixed to the rotary shaft 2 via a boss 7 and is orthogonal to the rotary shaft 2. -Shaped main plate, 6 is a conical side plate, and is inclined by an angle θ so as to approach the main plate 5 toward the outer periphery thereof.

【0014】3は翼で、円周方向に沿って等間隔を隔て
て複数枚配設され、その両端は主板5の内面5a及び側板
6の内面6aに固定されている。これら翼3の前縁3cには
それぞれ前方に突出する補助翼14が固定されている。
A plurality of blades 3 are arranged at equal intervals along the circumferential direction, and both ends thereof are fixed to the inner surface 5a of the main plate 5 and the inner surface 6a of the side plate 6. Auxiliary wings 14 projecting forward are fixed to the front edges 3c of these wings 3.

【0015】図1(B) に示すように、補助翼14の中心が
羽根車1の回転軸心2aを中心として翼3の前縁3cに接す
る円Rの翼3の前縁3cにおける接線Yとなす角、即ち、
補助翼14の入射角βは翼3の入射角αよりも若干(5〜
15°)小さくなるように設定されている。
As shown in FIG. 1 (B), the tangent line Y at the leading edge 3c of the blade 3 of the circle R, whose center is the auxiliary blade 14 and is in contact with the leading edge 3c of the blade 3 about the rotational axis 2a of the impeller 1. The angle between
The incident angle β of the auxiliary blade 14 is slightly smaller than the incident angle α of the blade 3 (5 to 5
15 °) is set to be small.

【0016】また、補助翼14の翼弦長lは少なくとも翼
3の翼弦長Lの10%以上とし、かつ、補助翼14の設置に
より隣接する翼3との間隔が流量減少の原因となる狭さ
にならないように翼間ピッチP(=Rφ)の40%以下に
設定されている。更に、補助翼14は主板5寄りに設置す
る必要はないので、その翼弦長lは図1(A) 、(C) に示
すように、主板5に近づくに従い小さくなるように構成
されている。
The chord length l of the auxiliary blade 14 is at least 10% or more of the chord length L of the blade 3, and the distance between the adjacent blades 3 due to the installation of the auxiliary blade 14 causes a decrease in the flow rate. The pitch is set to 40% or less of the blade pitch P (= Rφ) so as not to be narrow. Further, since the auxiliary wing 14 does not need to be installed near the main plate 5, the chord length l thereof is configured to become smaller as it approaches the main plate 5, as shown in FIGS. 1 (A) and 1 (C). .

【0017】しかして、気体が主板5寄り及び側板6寄
りに同じ流速で流入した場合、側板6の内面6aが傾斜し
ているため、側板6寄りの方が主板5寄りよりも入射角
が大きくなる。
However, when the gas flows toward the main plate 5 and the side plate 6 at the same flow velocity, since the inner surface 6a of the side plate 6 is inclined, the incident angle on the side plate 6 side is larger than that on the main plate 5 side. Become.

【0018】しかるに、側板6寄りに翼3の入射角αよ
りも入射角βの小さい補助翼14が設けられているので、
主板5寄りと側板6寄りの入射角がほぼ同一となり、従
来のもののような入射角の不同に基づく流れの剥離や圧
力損失の増加を阻止しうる。
However, since the auxiliary blade 14 having an incident angle β smaller than the incident angle α of the blade 3 is provided near the side plate 6,
The incident angles of the main plate 5 side and the side plate 6 side are substantially the same, and flow separation and increase in pressure loss due to the non-uniform incident angle as in the conventional case can be prevented.

【0019】以上、本発明を片吸込型遠心送風機に適用
した場合について説明したが、本発明を両吸込型送風機
に適用できることは勿論である。
The case where the present invention is applied to the single-suction type centrifugal blower has been described above, but it goes without saying that the present invention can be applied to a double-suction type blower.

【0020】[0020]

【発明の効果】本発明によれば、翼の前縁から前方に突
出する補助翼を設け、この補助翼の入口角を翼の入口角
より小さくしたため、翼に対する入射角が主板寄り及び
側板寄りでほぼ同一となり、従って、流れの剥離や圧力
損失の増加を防止しうる。
According to the present invention, since the auxiliary blade protruding forward from the leading edge of the blade is provided and the entrance angle of this auxiliary blade is smaller than the entrance angle of the blade, the incident angle to the blade is closer to the main plate and the side plate. Therefore, flow separation and increase in pressure loss can be prevented.

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

【図1】本発明の1実施例を示し、(A) は羽根車の軸心
に沿う断面図、(B) は(A) のB−B線に沿う断面図、
(C) は(A) のC−C線に沿う断面図である。
1 shows an embodiment of the present invention, (A) is a sectional view taken along the axis of the impeller, (B) is a sectional view taken along the line BB of (A), FIG.
(C) is a sectional view taken along the line CC of (A).

【図2】従来の片吸込型遠心送風機の1例を示し、(A)
は(B) のA−A線に沿う断面図、(B) は(A) のB−B線
に沿う断面図、(C) は羽根車の外観斜視図である。
FIG. 2 shows an example of a conventional single suction centrifugal fan, (A)
3B is a cross-sectional view taken along the line AA of (B), (B) is a cross-sectional view taken along the line BB of (A), and (C) is an external perspective view of the impeller.

【図3】従来の片吸込型遠心送風機の羽根車を示し、
(A) は軸心に沿う断面図、(B) は(A) のB−B線に沿う
断面図、(C) は(A) のC−C線に沿う断面図である。
FIG. 3 shows an impeller of a conventional single-suction centrifugal fan,
(A) is a sectional view taken along the axial center, (B) is a sectional view taken along line BB of (A), and (C) is a sectional view taken along line CC of (A).

【符号の説明】[Explanation of symbols]

1 羽根車 2 回転軸 3 翼 3a 負圧面 3b 圧力面 5 主板 6 側板 14 補助翼 1 impeller 2 rotation axes 3 wings 3a suction side 3b Pressure side 5 Main plate 6 side plate 14 Aileron

───────────────────────────────────────────────────── フロントページの続き (56)参考文献 実開 昭60−107399(JP,U) 実開 平1−66500(JP,U) (58)調査した分野(Int.Cl.7,DB名) F04D 29/30 F04D 29/28 F04D 29/42 ─────────────────────────────────────────────────── ─── Continuation of the front page (56) Bibliography Sho 60-107399 (JP, U) Rikai Hei 1-66500 (JP, U) (58) Fields investigated (Int.Cl. 7 , DB name) F04D 29/30 F04D 29/28 F04D 29/42

Claims (2)

(57)【特許請求の範囲】(57) [Claims] 【請求項1】 うず巻状のスクロールケーシング内に回
転軸に固定されてこれと直交する円板状の主板と外周に
向かうに従って上記主板に接近するように傾斜する円錐
状の側板との間にその円周方向に沿って等間隔を隔てて
複数枚の翼を固定してなる羽根車を配設してなる遠心送
風機において、 上記翼の前縁から前方に突出する補助翼を設け、この補
助翼の入口角を上記翼の入口角より小さくしたことを特
徴とする遠心送風機。
1. Between a disc-shaped main plate which is fixed to a rotary shaft in a spiral scroll casing and which is orthogonal to the rotary shaft, and a conical side plate which is inclined so as to approach the main plate toward the outer periphery. In a centrifugal blower comprising an impeller having a plurality of blades fixed at equal intervals along the circumferential direction thereof, an auxiliary blade protruding forward from the front edge of the blade is provided. A centrifugal blower, wherein the blade inlet angle is smaller than the blade inlet angle.
【請求項2】 上記補助翼の突出長さを上記側板から主
板に向かうに従って漸減させたことを特徴とする請求項
1記載の遠心送風機。
2. The centrifugal blower according to claim 1, wherein the protruding length of the auxiliary blade is gradually reduced from the side plate toward the main plate.
JP02756395A 1995-01-24 1995-01-24 Centrifugal blower Expired - Fee Related JP3411701B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP02756395A JP3411701B2 (en) 1995-01-24 1995-01-24 Centrifugal blower

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP02756395A JP3411701B2 (en) 1995-01-24 1995-01-24 Centrifugal blower

Publications (2)

Publication Number Publication Date
JPH08200290A JPH08200290A (en) 1996-08-06
JP3411701B2 true JP3411701B2 (en) 2003-06-03

Family

ID=12224507

Family Applications (1)

Application Number Title Priority Date Filing Date
JP02756395A Expired - Fee Related JP3411701B2 (en) 1995-01-24 1995-01-24 Centrifugal blower

Country Status (1)

Country Link
JP (1) JP3411701B2 (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100393834B1 (en) * 2001-01-05 2003-08-06 삼성엔지니어링 주식회사 Air intake appartus for air cleaning room
JP2005127311A (en) * 2003-10-02 2005-05-19 Daikin Ind Ltd Centrifugal blower and air conditioner using it
JP2005133710A (en) * 2003-10-07 2005-05-26 Daikin Ind Ltd Centrifugal blower and air conditioner using it
JP4665472B2 (en) * 2004-09-28 2011-04-06 パナソニック株式会社 Blower
WO2016042698A1 (en) * 2014-09-18 2016-03-24 株式会社デンソー Blower
JP6409666B2 (en) * 2014-09-18 2018-10-24 株式会社デンソー Blower

Also Published As

Publication number Publication date
JPH08200290A (en) 1996-08-06

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