JPH09126190A - Centrifugal type blower - Google Patents

Centrifugal type blower

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Publication number
JPH09126190A
JPH09126190A JP28213395A JP28213395A JPH09126190A JP H09126190 A JPH09126190 A JP H09126190A JP 28213395 A JP28213395 A JP 28213395A JP 28213395 A JP28213395 A JP 28213395A JP H09126190 A JPH09126190 A JP H09126190A
Authority
JP
Japan
Prior art keywords
ribs
length
centrifugal blower
blade
rib
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.)
Withdrawn
Application number
JP28213395A
Other languages
Japanese (ja)
Inventor
Michihiro Kurokawa
通広 黒河
Kenji Nasako
賢二 名迫
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.)
Sanyo Electric Co Ltd
Original Assignee
Sanyo Electric 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 Sanyo Electric Co Ltd filed Critical Sanyo Electric Co Ltd
Priority to JP28213395A priority Critical patent/JPH09126190A/en
Publication of JPH09126190A publication Critical patent/JPH09126190A/en
Withdrawn legal-status Critical Current

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Abstract

PROBLEM TO BE SOLVED: To reduce noise in frequencies of a wide band by providing a plurality of ribs for each of a plurality of vanes over its pressure surface subjected to positive pressure in a place close to its end part in the outer side in the radial direction wherein the ribs are arranged in parallel at prescribed intervals while each one is prescribed in thickness, length and height, and is lengthwise directed in the flow direction. SOLUTION: A plurality of ribs 7 are provided at prescribed intervals in parallel with the length L direction of each vane 4 at its rear peripheral part for a plurality of the vanes 4 provided for an impeller. Each rib 7 may be provided only for the positive pressure side, or in order to effectively suppress noise, each rib may be provided for both the positive and negative pressure sides of each vane 4. Since vortexes as noise sources in a wide range are mainly developed within the velocity boundary layer of each vane 4, the height of each rib it to be basically determined based on the velocity boundary layer, and it is normally equal to or more than 2mm but less than 3mm. In addition, the spanwisw length of each rib 7, that is, each interval between the adjacent ribs 7 in the width H direction of each vane 4 is to be equal to or more than 10mm but less than 20mm, and its length is nearly equal to an interval between the ribs.

Description

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

【0001】[0001]

【発明の属する技術分野】本発明は、空調設備などに用
いられる遠心式送風機に関し、特に、翼形状の改善によ
り広帯域周波数騒音の低減を図った遠心式送風機に関す
るものである。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a centrifugal blower used for air conditioning equipment and the like, and more particularly to a centrifugal blower designed to reduce broadband frequency noise by improving its blade shape.

【0002】[0002]

【従来の技術】空調設備機器の熱交換器などに用いられ
る従来の遠心式送風機は、図5(a)(b)に示すよう
な羽根車1を有している。この羽根車1は、中央にボス
2aを設けた円形の主プレート2と、この主プレート2
の上方に対向して設けられた、空気取入れ開口3aを有
する副プレート3と、主プレート2の外周近傍において
主プレート2に直角に立上がるように、主プレート2と
副プレート3との間において放射状に配されたブレード
状の複数の翼4とを備えている。図5(a)において羽
根車1が矢印A方向に回転することにより、矢印B方向
の空気流が発生する。
2. Description of the Related Art A conventional centrifugal blower used for a heat exchanger of an air conditioning equipment has an impeller 1 as shown in FIGS. This impeller 1 includes a circular main plate 2 having a boss 2a in the center and a main plate 2
Between the main plate 2 and the sub-plate 3 so as to stand upright at a right angle to the main plate 2 in the vicinity of the outer periphery of the main plate 2 and the sub-plate 3 provided to face above the main plate 2 and facing each other. And a plurality of blade-shaped blades 4 arranged radially. As the impeller 1 rotates in the direction of arrow A in FIG. 5A, an air flow in the direction of arrow B is generated.

【0003】羽根車1は、図6(a)に示すように、空
気吸込み口を構成するベルマウス5aを有する渦巻き状
のケース4内に収容され、一端がボス2aに固定された
駆動軸(図示せず)によって羽根車1が回転駆動される
ことにより、フィルタ6を通って矢印C方向から流入し
た空気は羽根車1内を矢印D方向に流れ、さらにケース
5内において円周方向に流れて矢印C方向に吹き出され
る。
As shown in FIG. 6 (a), the impeller 1 is housed in a spiral case 4 having a bell mouth 5a which constitutes an air suction port, and one end of which is fixed to a boss 2a. When the impeller 1 is rotationally driven by (not shown), the air flowing in from the direction of the arrow C through the filter 6 flows through the impeller 1 in the direction of the arrow D and further flows in the case 5 in the circumferential direction. Is blown out in the direction of arrow C.

【0004】このような従来の遠心式送風機において
は、ベルマウス5aからケース5内に空気が吸込まれた
後、ケース5のコーナ部などにおいて渦流が発生すると
ともに、副プレート3とケース5との間には逆流が発生
し、その結果送風機の効率を低下させかつ騒音を高める
原因になっていた。
In such a conventional centrifugal blower, after air is sucked into the case 5 from the bell mouth 5a, a vortex is generated in a corner portion of the case 5 and the sub plate 3 and the case 5 are separated from each other. In the meantime, a backflow was generated, resulting in a decrease in the efficiency of the blower and an increase in noise.

【0005】このような従来の遠心式送風機の問題点を
解消することを目的とした従来の技術として、たとえば
特開平5−332293号公報には、副プレート3上に
サブブレードを形成することによって渦流および逆流の
発生をなくすことが開示されている。
As a conventional technique aiming at solving the above-mentioned problems of the conventional centrifugal blower, for example, in Japanese Patent Laid-Open No. 5-332293, a sub blade is formed on the sub plate 3. It is disclosed to eliminate the generation of swirl and backflow.

【0006】また特開平5−126093号公報には、
遠心式送風機の羽根車の回転時に風があたる翼の表面
に、翼の幅方向に延びる凸部を立体的に設けることによ
り、翼の外縁の表面および裏面のそれぞれに沿って放出
される空気の合流を防ぐことにより騒音を抑制する技術
が開示され、特開平5−126351号公報には、遠心
式送風機から吐出される空気を熱交換器に導くようにし
た熱交換ユニットにおいて、熱交換器の直線形状部の吸
込み側には遠心式送風機側へ延びる制御板を取付けるこ
とにより、熱交換器の吸込み側の渦流の発生を抑えて騒
音の発生を防止する技術が開示されている。
Further, Japanese Patent Laid-Open No. 5-126093 discloses that
By providing three-dimensionally convex portions extending in the width direction of the blade on the surface of the blade on which the wind blows when the impeller of the centrifugal blower rotates, the air discharged along the front and back surfaces of the outer edge of the blade A technique for suppressing noise by preventing merging is disclosed, and Japanese Patent Application Laid-Open No. 5-126351 discloses a heat exchange unit in which air discharged from a centrifugal blower is introduced to a heat exchanger. A technique is disclosed in which a control plate extending toward the centrifugal blower side is attached to the suction side of the linear portion to suppress the generation of vortex flow on the suction side of the heat exchanger to prevent the generation of noise.

【0007】その他にも、ベルマウスなどの形状の改良
のよって低騒音化を図る技術も、種々提案されている。
In addition, various techniques for reducing noise by improving the shape of a bell mouth have been proposed.

【0008】[0008]

【発明が解決しようとする課題】以上述べたように、空
調設備機器に用いられる遠心式送風機の低騒音化が進め
られているが、特にパッケージエアコンの室内機などに
用いられる室内側送風用のターボファンについては、広
帯域周波数騒音が依然問題となっており、さらに低騒音
化を図ることが課題となっている。
As described above, the noise reduction of the centrifugal blower used for the air conditioning equipment is being promoted, but especially for the indoor blower used for the indoor unit of the packaged air conditioner or the like. Broadband frequency noise remains a problem for turbofans, and further noise reduction is an issue.

【0009】上記従来の問題点に鑑み本発明は、広帯域
周波数騒音の低減を図ることによって遠心式送風機の低
騒音化をさらに向上させることを目的とする。
In view of the above conventional problems, it is an object of the present invention to further improve the noise reduction of a centrifugal blower by reducing wide band frequency noise.

【0010】[0010]

【課題を解決するための手段】上記目的を達成する本発
明の遠心式送風機は、回転軸を中心とする円周の方向に
沿ってブレード状の翼を略放射状に配列し、回転により
遠心方向に空気流を発生させる遠心式送風機であって、
複数の翼の各々が、径方向外側の端部近傍の、正圧を受
ける圧力面上のみまたは該圧力面と該圧力面の裏側の負
圧面との両方の面上に、所定の厚さ、長さおよび高さを
有し、長さ方向が、空気流の方向すなわち翼の長さ方向
を向いて互いに平行に所定間隔をおいて配列された複数
のリブを含むことを特徴とする。
The centrifugal blower of the present invention which achieves the above object has blade-shaped blades arranged substantially radially along the direction of the circumference centered on the rotation axis, and is rotated in the centrifugal direction. A centrifugal blower that generates an air flow in
Each of the plurality of blades has a predetermined thickness near the radially outer end only on the pressure surface that receives positive pressure or on both the pressure surface and the suction surface behind the pressure surface, It is characterized in that it has a length and a height, and the length direction includes a plurality of ribs which are arranged at predetermined intervals in parallel with each other in the direction of the air flow, that is, the length direction of the blade.

【0011】複数の翼は、回転駆動力が伝達されるボス
部を中心とする円形の外周を有する主プレートと、該主
プレートに対向して配され、空気取入れ開口を中央に有
する円形の副プレートと、主プレートと副プレートとの
間の外周近傍において、主プレートに直角に立上がるよ
うに略放射状に配列されて固定されている。
The plurality of blades are provided with a main plate having a circular outer periphery centered on a boss portion to which the rotational driving force is transmitted, and a circular sub-element disposed so as to face the main plate and having an air intake opening in the center. Near the outer periphery of the plate and between the main plate and the sub plate, they are arranged and fixed in a substantially radial pattern so as to stand up at a right angle to the main plate.

【0012】本発明の構造によれば、複数の互いに平行
に配されたリブを有することにより、翼の後縁すなわち
翼の外周端近傍における空気流の乱れが整流化されて、
広帯域周波数騒音となる翼後縁での翼のスパン方向の渦
干渉が低減されるため、広帯域周波数騒音を抑制するこ
とができる。
According to the structure of the present invention, by having the plurality of ribs arranged in parallel to each other, the turbulence of the air flow near the trailing edge of the blade, that is, near the outer peripheral end of the blade is rectified,
Since the eddy interference in the span direction of the blade at the blade trailing edge that causes wideband frequency noise is reduced, the wideband frequency noise can be suppressed.

【0013】複数のリブの各々は、高さが2mm以上3
mm以下、厚みが1mm以上2mm以下を有し、隣り合
うリブ間の間隔が10mm以上20mm以下に設定され
るとともに、複数のリブの各々が、隣り合うリブ間の間
隔と同じ長さまたはそれ以上の長さを有することが好ま
しい。
Each of the plurality of ribs has a height of 2 mm or more and 3
mm or less, the thickness is 1 mm or more and 2 mm or less, the distance between adjacent ribs is set to 10 mm or more and 20 mm or less, and each of the plurality of ribs has the same length or more as the distance between the adjacent ribs. Preferably has a length of.

【0014】リブの高さを2mm以上3mm以下に設定
したのは、広帯域音源となる渦が翼面の速度境界層内で
発生することから、その速度境界層厚さと同じ程度の高
さを有することが適正であるとの理由によるものであ
る。また隣り合うリブ間の間隔を10mm以上20mm
以下としたのは、次の理由による。すなわち、一般に渦
相関のスパン方向の等価相関長は、平板の場合、板厚の
5〜10倍であり、本発明が適用される遠心式送風機に
おいては翼の厚みの最大値が略10mmであり、渦を放
射する翼後縁部の厚みが2mm程度であることから、1
0〜20mm程度の間隔が最適であるとの考察に基づく
ものである。
The height of the rib is set to 2 mm or more and 3 mm or less because the vortex which is a broadband sound source is generated in the velocity boundary layer of the blade surface, and the height is about the same as the velocity boundary layer thickness. This is because it is appropriate. The distance between adjacent ribs is 10 mm or more and 20 mm.
The reason is as follows. That is, generally, the equivalent correlation length in the span direction of the vortex correlation is 5 to 10 times the plate thickness in the case of a flat plate, and the maximum value of the blade thickness is approximately 10 mm in the centrifugal blower to which the present invention is applied. Since the thickness of the trailing edge of the blade that radiates the vortex is about 2 mm, 1
This is based on the consideration that an interval of about 0 to 20 mm is optimal.

【0015】リブの厚さについては、遠心式送風機の性
能上はより薄い方が望ましいが、強度や製造上の容易さ
を考慮して、1mm以上2mm以下に設定した。またリ
ブの長さについても、長すぎると空気抵抗が増加すると
いう問題が生じるため、より短い方が望ましいが、広帯
域騒音を低減するという目的を達成するためには、その
長さが少なくともスパン方向の間隔に等しい程度以上で
あることが望ましい。
The thickness of the rib is preferably thinner in view of the performance of the centrifugal blower, but is set to 1 mm or more and 2 mm or less in consideration of strength and ease of manufacturing. As for the rib length, too long length causes a problem that air resistance increases, so shorter length is desirable, but in order to achieve the purpose of reducing broadband noise, the rib length must be at least the span direction. It is desirable that the distance is equal to or larger than the interval.

【0016】なお、広帯域騒音を抑制するという観点か
らは、基本的にはリブを翼の圧力面とその裏側の負圧面
との両側に設けることが望ましいが、翼の構成上片面か
らの音の放射が著しく大きい場合、すなわちたとえば後
縁付近で逆圧力勾配などによる剥離が発生する場合にお
いては、翼の表裏両面に設ける必要はなく、翼の圧力面
側のみに設置することによって十分広帯域騒音が抑制さ
れる。
From the viewpoint of suppressing broadband noise, it is basically desirable to provide ribs on both sides of the pressure surface of the blade and the suction surface on the back side thereof. If the radiation is extremely large, that is, if separation occurs due to an inverse pressure gradient near the trailing edge, it is not necessary to provide it on both the front and back sides of the blade, and installing it only on the pressure side of the blade will result in sufficient broadband noise. Suppressed.

【0017】[0017]

【発明の実施の形態】以下、本発明の一実施の形態につ
いて、図1ないし図4に基づいて説明する。本発明が適
用される遠心式送風機の羽根車1およびケース5の構造
などについては、図5および図6を用いて説明した従来
のものと特に変わるところはないので、その詳細な説明
を省略する。本発明の一実施の形態においては、羽根車
1に複数個設けられる翼4の各々が、図1(a)(b)
に示すように、その後縁部において、翼4の長さLの方
向に平行に、複数個のリブ7を所定間隔をおいて平行に
設けている。図1においてはリブ7の数を4個とした
が、リブ7の数は必要に応じ適宜増減される。
DESCRIPTION OF THE PREFERRED EMBODIMENTS One embodiment of the present invention will be described below with reference to FIGS. Since the structure of the impeller 1 and the case 5 of the centrifugal blower to which the present invention is applied are not particularly different from the conventional ones described with reference to FIGS. 5 and 6, detailed description thereof will be omitted. . In one embodiment of the present invention, each of the blades 4 provided in the impeller 1 has a structure as shown in FIGS.
As shown in FIG. 7, a plurality of ribs 7 are provided in parallel at the trailing edge portion in the direction of the length L of the blade 4 at a predetermined interval. Although the number of ribs 7 is four in FIG. 1, the number of ribs 7 may be increased or decreased as necessary.

【0018】リブ7は、図2(a)において矢印Fで示
す正圧側のみに設けてもよく、また図2(b)に示すよ
うに翼7の正圧側および矢印Eで示す負圧側の両面に設
けてもよい。広帯域周波数騒音をより効果的に低減させ
るためには、図2(b)に示すように翼7の正圧側およ
び負圧側の両面に設けることが好ましいが、翼7の構成
上、後縁付近で逆圧力勾配などによる剥離が発生するよ
うな場合には、翼7の正圧側からの音の放射が著しく大
きい場合があり、そのような場合には図2(a)に示す
ように翼7の正圧面側のみに設けることによっても、十
分本発明の目的を達成することができる。
The rib 7 may be provided only on the positive pressure side indicated by the arrow F in FIG. 2A, or on both the positive pressure side of the blade 7 and the negative pressure side indicated by the arrow E as shown in FIG. 2B. May be provided. In order to reduce the broadband frequency noise more effectively, it is preferable to provide it on both the positive pressure side and the negative pressure side of the blade 7 as shown in FIG. 2 (b), but due to the configuration of the blade 7, near the trailing edge. When separation occurs due to a reverse pressure gradient or the like, the sound radiation from the positive pressure side of the blade 7 may be extremely large. In such a case, as shown in FIG. The object of the present invention can be sufficiently achieved by providing only on the positive pressure surface side.

【0019】次に、リブ7の好ましい形状および配列に
ついて考察する。リブ7の形状としては、図3(a)に
示すような部分円形のもの、あるいは図3(b)に示す
ような直方体形状のものを用いることができ、その形状
寸法の最適値を考察するための寸法パラメータとして
は、高さh、厚さt、長さcおよび隣接するリブ7,7
間の間隔bが問題となる。これらの寸法パラメータにつ
いては、図3(a)(b)のいずれに示すリブ形状にお
いてもほぼ等価なものとして考えることができる。
Next, the preferable shape and arrangement of the rib 7 will be considered. As the shape of the rib 7, a partial circular shape as shown in FIG. 3A or a rectangular parallelepiped shape as shown in FIG. 3B can be used, and the optimum value of the shape dimension will be considered. The dimension parameters for the height h, the thickness t, the length c, and the adjacent ribs 7, 7 are
The interval b between them becomes a problem. These dimensional parameters can be considered to be substantially equivalent in any of the rib shapes shown in FIGS. 3 (a) and 3 (b).

【0020】まずリブの高さhについては次のように考
察される。広帯域音源となる渦は、翼4の表面の速度境
界層(図4において参照番号8で示す領域)内において
主として発生する。その速度境界層8の厚さ(図4に示
す寸法δ)は、主流の流速U、空気の粘度ν、翼8の前
縁からの距離xによって決定され、δ=f(U,ν,
x)のように表わすことができる。本発明が適用される
遠心式送風機の一般的な諸元から、U=10m/s,x
(=L)=110mm,ν=0.154×10-42
sであるため、速度境界層の厚さδは約2.5mmとな
る。このことから、リブの高さhは2〜3mm程度であ
ることが適正であると考える。
First, the rib height h is considered as follows. The vortex that is a broadband sound source is mainly generated in the velocity boundary layer (the area indicated by reference numeral 8 in FIG. 4) on the surface of the blade 4. The thickness of the velocity boundary layer 8 (dimension δ shown in FIG. 4) is determined by the flow velocity U of the main flow, the viscosity ν of air, and the distance x from the leading edge of the blade 8, and δ = f (U, ν,
It can be represented as x). From the general specifications of the centrifugal blower to which the present invention is applied, U = 10 m / s, x
(= L) = 110 mm, ν = 0.154 × 10 −4 m 2 /
Therefore, the thickness δ of the velocity boundary layer is about 2.5 mm. From this, it is considered appropriate that the height h of the rib is about 2 to 3 mm.

【0021】次にリブのスパン方向間隔b、すなわち翼
4の幅(図1(a)に示す寸法H)方向の隣接リブ間の
間隔bの最適値について考察する。一般に渦相関のスパ
ン方向の等価相関長は、平板の場合、その板厚の5〜1
0倍であり、本発明が適用される遠心式送風機において
は翼4の厚みの最大値が約10mmである。ただし、渦
を放射する翼後縁部の厚みは2mm程度であるため、間
隔bは10〜20mm程度が最適である。
Next, the optimum value of the span distance b between the ribs, that is, the distance b between adjacent ribs in the width direction (dimension H shown in FIG. 1A) of the blade 4 will be considered. Generally, the equivalent correlation length of the eddy correlation in the span direction is 5 to 1 of the plate thickness in the case of a flat plate.
It is 0 times, and the maximum value of the thickness of the blade 4 is about 10 mm in the centrifugal blower to which the present invention is applied. However, since the thickness of the trailing edge of the blade that radiates the vortex is about 2 mm, the interval b is optimally about 10 to 20 mm.

【0022】次にリブ7の厚みtと長さcについて考察
する。まず厚さtについては、遠心式送風機の性能上で
きるだけ薄い方が好ましいが、強度および製造容易性を
考慮すると、厚みtは1〜2mm程度にすることが好ま
しい。またリブ7の長さcについても、長すぎると空気
抵抗が増大するため、空気抵抗低減という観点からは極
力短い方が望ましい。しかしながら広帯域騒音の低減と
いう本発明の目的を達成するためには、その長さcは少
なくともスパン方向の間隔bに等しい程度の長さ以上に
設定することが望ましい。
Next, the thickness t and the length c of the rib 7 will be considered. First, the thickness t is preferably as thin as possible in view of the performance of the centrifugal blower, but considering the strength and the easiness of manufacturing, the thickness t is preferably about 1 to 2 mm. Also, regarding the length c of the rib 7, if the length is too long, the air resistance increases, so it is desirable to be as short as possible from the viewpoint of reducing the air resistance. However, in order to achieve the object of the present invention of reducing broadband noise, it is desirable that the length c be set to be equal to or greater than at least the interval b in the span direction.

【0023】以上述べた本発明の実施の形態は、あくま
で本発明を実現するための一例にすぎず、特許請求の範
囲に記載された構成に均等の範囲において種々変更した
ものも本発明に包含されることは言うまでもない。
The above-described embodiments of the present invention are merely examples for realizing the present invention, and various modifications within the scope equivalent to the configurations described in the claims are also included in the present invention. It goes without saying that it will be done.

【0024】[0024]

【発明の効果】以上述べたように本発明によれば、所定
の厚さ、長さおよび高さを有するリブを複数個、翼の後
縁近傍表面において、空気流方向を向いて互いに平行に
所定間隔をおいて配列することにより、翼の後縁近傍に
おける空気流の乱れが整流化されて、翼後縁でのスパン
方向の渦干渉が低減される。その結果広帯域周波数騒音
が抑制され、大幅に低騒音化が図られるため、空調設備
機器の室内機用などに適した遠心式送風機を提供するこ
とができる。
As described above, according to the present invention, a plurality of ribs each having a predetermined thickness, length and height are arranged parallel to each other in the air flow direction on the surface near the trailing edge of the blade. By arranging them at a predetermined interval, the turbulence of the air flow near the trailing edge of the blade is rectified, and eddy interference in the span direction at the trailing edge of the blade is reduced. As a result, the broadband frequency noise is suppressed and the noise is significantly reduced, so that it is possible to provide a centrifugal blower suitable for an indoor unit of an air conditioning equipment.

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

【図1】(a)は本発明の一実施の形態における翼4の
構造を示す平面図、(b)は(a)に示した翼の斜視図
である。
1A is a plan view showing a structure of a blade 4 according to an embodiment of the present invention, and FIG. 1B is a perspective view of the blade shown in FIG. 1A.

【図2】(a)は本発明の一実施の形態においてリブ7
を翼4の片面側のみ、すなわち正圧面側のみに設けた形
態を示す図、(b)はリブ7を翼4の正圧面側および負
圧面側の両面に設けた例を示す図である。
FIG. 2 (a) shows a rib 7 according to an embodiment of the present invention.
Is a diagram showing a mode in which the blades are provided only on one surface side of the blade 4, that is, only on the pressure surface side, and (b) is a diagram showing an example in which the ribs 7 are provided on both the pressure surface side and the suction surface side of the blade 4.

【図3】図3は、2通りのリブ7の形状について、その
寸法パラメータの定義を説明するための拡大斜視図であ
る。
FIG. 3 is an enlarged perspective view for explaining the definition of dimensional parameters for two types of ribs 7;

【図4】本発明のリブの高さの最適値を考察する上で
の、速度境界層を説明するための図である。
FIG. 4 is a diagram for explaining a velocity boundary layer in considering an optimum value of the rib height of the present invention.

【図5】(a)は従来の遠心式送風機の羽根車の概略を
示す平面図、(b)は(a)におけるVB−VB線断面
を示す図である。
5A is a plan view showing an outline of an impeller of a conventional centrifugal blower, and FIG. 5B is a view showing a cross section taken along line VB-VB in FIG. 5A.

【図6】(a)は従来の遠心式送風機の部分断面図、
(b)は従来の遠心式送風機の外観を示す斜視図であ
る。
FIG. 6A is a partial cross-sectional view of a conventional centrifugal blower,
(B) is a perspective view showing the appearance of a conventional centrifugal blower.

【符号の説明】[Explanation of symbols]

1 羽根車 2 主プレート 2a ボス 3 副プレート 3a 空気取入れ開口 4 翼 5 ケース 5a ベルマウス 7 リブ 1 Impeller 2 Main plate 2a Boss 3 Sub-plate 3a Air intake opening 4 Wing 5 Case 5a Bell mouth 7 Rib

Claims (3)

【特許請求の範囲】[Claims] 【請求項1】 回転軸を中心とする円周の方向に沿っ
て、ブレード状の翼を略放射状に配列し、回転により遠
心方向に空気流を発生させる遠心式送風機であって、 前記複数の翼の各々は、径方向外側の端部近傍の、正圧
を受ける圧力面上のみまたは該圧力面と該圧力面の裏側
の負圧面との両方の面上に、所定の厚さ、長さおよび高
さを有し、長さ方向が空気流の方向を向いて互いに平行
に所定間隔をおいて配列された複数のリブを設けた、遠
心式送風機。
1. A centrifugal blower in which blade-shaped blades are arranged in a substantially radial pattern along a circumferential direction around a rotation axis, and an air flow is generated in a centrifugal direction by rotation. Each of the blades has a predetermined thickness and length near the radially outer end only on the pressure surface that receives positive pressure or on both the pressure surface and the suction surface on the back side of the pressure surface. And a plurality of ribs having a height and a length direction facing the direction of the air flow and arranged in parallel with each other at a predetermined interval, and a centrifugal blower.
【請求項2】 回転駆動力が伝達されるボス部を中心と
する円形の外周を有する主プレートと、該主プレートに
対向して配され、空気取入れ開口を中央に有する円形の
副プレートと、前記主プレートと前記副プレートとの間
の前記主プレートの外周近傍において、該主プレートに
直角に立上がるとともに、略放射状に配列されたプレー
ト状の複数の翼とを有する羽根車と、 空気吸込み口を形成するベルマウスを有するとともに前
記羽根車を収容する渦巻き状ケースとを備えた遠心式送
風機であって、 前記複数の翼の各々は、径方向外側の端部近傍の、正圧
を受ける圧力面上のみまたは該圧力面と該圧力面の裏側
の負圧面との両方の面上に、所定の厚さ、長さおよび高
さを有し、長さ方向が前記翼の長さ方向を向いて互いに
平行に所定間隔をおいて配列された複数のリブを設け
た、遠心式送風機。
2. A main plate having a circular outer periphery centering on a boss portion to which a rotational driving force is transmitted, and a circular sub-plate arranged so as to face the main plate and having an air intake opening in the center. An impeller having a plurality of plate-shaped blades that stand up at a right angle to the main plate in the vicinity of the outer periphery of the main plate between the main plate and the sub plate and that are substantially radially arranged, A centrifugal blower having a bell mouth that forms a mouth and a spiral case that houses the impeller, wherein each of the plurality of blades receives a positive pressure in the vicinity of the radially outer end portion. It has a predetermined thickness, length and height only on the pressure surface or on both the pressure surface and the suction surface on the back side of the pressure surface, and the length direction is the length direction of the blade. Facing each other and parallel to each other at a specified interval A plurality of ribs arranged Te provided, centrifugal blower.
【請求項3】 前記複数のリブの各々は、高さが2mm
以上3mm以下、厚みが1mm以上2mm以下を有し、
隣り合う前記リブ間の間隔が10mm以上20mm以下
に設定されるとともに、前記複数のリブの各々が、隣り
合うリブ間の前記間隔と同じ長さまたはそれ以上の長さ
を有する、請求項1または2記載の遠心式送風機。
3. The height of each of the plurality of ribs is 2 mm.
Has a thickness of 3 mm or less and a thickness of 1 mm or more and 2 mm or less,
The distance between the adjacent ribs is set to 10 mm or more and 20 mm or less, and each of the plurality of ribs has a length equal to or greater than the distance between the adjacent ribs. The centrifugal blower described in 2.
JP28213395A 1995-10-30 1995-10-30 Centrifugal type blower Withdrawn JPH09126190A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP28213395A JPH09126190A (en) 1995-10-30 1995-10-30 Centrifugal type blower

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP28213395A JPH09126190A (en) 1995-10-30 1995-10-30 Centrifugal type blower

Publications (1)

Publication Number Publication Date
JPH09126190A true JPH09126190A (en) 1997-05-13

Family

ID=17648550

Family Applications (1)

Application Number Title Priority Date Filing Date
JP28213395A Withdrawn JPH09126190A (en) 1995-10-30 1995-10-30 Centrifugal type blower

Country Status (1)

Country Link
JP (1) JPH09126190A (en)

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2001234888A (en) * 2000-02-25 2001-08-31 Mitsubishi Heavy Ind Ltd Blower
US6299409B1 (en) 1998-04-10 2001-10-09 Denso Corporation Centrifugal type blower unit
KR100429998B1 (en) * 2001-10-25 2004-05-03 엘지전자 주식회사 Turbo fan
JP2008069709A (en) * 2006-09-14 2008-03-27 Topre Corp Impeller for centrifugal fan
JP2009133271A (en) * 2007-11-30 2009-06-18 Mitsubishi Electric Corp Cross-flow fan and air-conditioner
WO2011121943A1 (en) 2010-03-29 2011-10-06 三菱電機株式会社 Turbofan and indoor air conditioner equipped with same
CN104251231A (en) * 2013-06-28 2014-12-31 苏州宝时得电动工具有限公司 Centrifugal impeller and blowing and inducing device comprising same
CN104251229A (en) * 2013-06-28 2014-12-31 苏州宝时得电动工具有限公司 Centrifugal type impeller and blowing and sucking device comprising centrifugal type impeller
EP2835585A4 (en) * 2012-04-06 2016-02-24 Mitsubishi Electric Corp Indoor unit for air conditioning device
JP2016521821A (en) * 2013-06-13 2016-07-25 ヌオーヴォ ピニォーネ ソチエタ レスポンサビリタ リミタータNuovo Pignone S.R.L. Compressor impeller
CN107050542A (en) * 2017-04-28 2017-08-18 浙江理工大学 Minitype centrifugal blood pump and its circulation blood supply method that a kind of anti-haemocyte is damaged
US9995303B2 (en) 2012-11-22 2018-06-12 Mitsubishi Electric Corporation Air conditioner
JP2020183721A (en) * 2019-05-07 2020-11-12 レノボ・シンガポール・プライベート・リミテッド Centrifugal fan and electronic device
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Cited By (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6299409B1 (en) 1998-04-10 2001-10-09 Denso Corporation Centrifugal type blower unit
JP2001234888A (en) * 2000-02-25 2001-08-31 Mitsubishi Heavy Ind Ltd Blower
KR100429998B1 (en) * 2001-10-25 2004-05-03 엘지전자 주식회사 Turbo fan
JP2008069709A (en) * 2006-09-14 2008-03-27 Topre Corp Impeller for centrifugal fan
JP2009133271A (en) * 2007-11-30 2009-06-18 Mitsubishi Electric Corp Cross-flow fan and air-conditioner
WO2011121943A1 (en) 2010-03-29 2011-10-06 三菱電機株式会社 Turbofan and indoor air conditioner equipped with same
CN102822532A (en) * 2010-03-29 2012-12-12 三菱电机株式会社 Turbofan and indoor air conditioner equipped with same
US9267511B2 (en) 2010-03-29 2016-02-23 Mitsubishi Electric Corporation Turbofan and indoor unit of air-conditioning apparatus including the same
EP2835585A4 (en) * 2012-04-06 2016-02-24 Mitsubishi Electric Corp Indoor unit for air conditioning device
US9995303B2 (en) 2012-11-22 2018-06-12 Mitsubishi Electric Corporation Air conditioner
EP2924296B1 (en) * 2012-11-22 2018-10-03 Mitsubishi Electric Corporation Air conditioner
JP2016521821A (en) * 2013-06-13 2016-07-25 ヌオーヴォ ピニォーネ ソチエタ レスポンサビリタ リミタータNuovo Pignone S.R.L. Compressor impeller
CN104251229A (en) * 2013-06-28 2014-12-31 苏州宝时得电动工具有限公司 Centrifugal type impeller and blowing and sucking device comprising centrifugal type impeller
CN104251231A (en) * 2013-06-28 2014-12-31 苏州宝时得电动工具有限公司 Centrifugal impeller and blowing and inducing device comprising same
CN107050542A (en) * 2017-04-28 2017-08-18 浙江理工大学 Minitype centrifugal blood pump and its circulation blood supply method that a kind of anti-haemocyte is damaged
CN107050542B (en) * 2017-04-28 2023-07-04 浙江理工大学 Miniature centrifugal blood pump capable of preventing blood cells from being damaged and circulating blood supply method thereof
JP2020183721A (en) * 2019-05-07 2020-11-12 レノボ・シンガポール・プライベート・リミテッド Centrifugal fan and electronic device
WO2022014376A1 (en) * 2020-07-14 2022-01-20 株式会社デンソー Turbofan
JP2022017860A (en) * 2020-07-14 2022-01-26 株式会社デンソー Turbo fan

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