JP3008930B2 - Impeller for blower - Google Patents

Impeller for blower

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Publication number
JP3008930B2
JP3008930B2 JP10175506A JP17550698A JP3008930B2 JP 3008930 B2 JP3008930 B2 JP 3008930B2 JP 10175506 A JP10175506 A JP 10175506A JP 17550698 A JP17550698 A JP 17550698A JP 3008930 B2 JP3008930 B2 JP 3008930B2
Authority
JP
Japan
Prior art keywords
impeller
wing
blade
blower
edge
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
JP10175506A
Other languages
Japanese (ja)
Other versions
JP2000009096A (en
Inventor
誠司 佐藤
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.)
Daikin Industries Ltd
Original Assignee
Daikin 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 Daikin Industries Ltd filed Critical Daikin Industries Ltd
Priority to JP10175506A priority Critical patent/JP3008930B2/en
Publication of JP2000009096A publication Critical patent/JP2000009096A/en
Application granted granted Critical
Publication of JP3008930B2 publication Critical patent/JP3008930B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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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】本願発明は、所謂エアフォイ
ル翼を備えた送風機用羽根車の構造に関するものであ
る。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a structure of an impeller for a blower having a so-called airfoil blade.

【0002】[0002]

【従来の技術】送風機に使用される羽根車の翼には種々
の形態のものが提案されているが、その一つに、翼面で
の気流の剥離を抑制して翼の空力性能を高める等の観点
から、翼の前縁部の翼厚を大きくするとともに該翼厚を
該前縁部から後縁部にかけて連続的に漸減変化させた形
状をもつ所謂「エアフォイル翼」が知られている。
2. Description of the Related Art Various types of blades of an impeller used for a blower have been proposed. One of them is to enhance the aerodynamic performance of the blade by suppressing air flow separation on the blade surface. From the viewpoint of such, a so-called "airfoil blade" having a shape in which the blade thickness of the leading edge of the blade is increased and the blade thickness is continuously gradually reduced from the leading edge to the trailing edge is known. I have.

【0003】[0003]

【発明が解決しようとする課題】ところが、かかるエア
フォイル翼においては、気流入口となる翼の前縁部にお
ける翼厚をかなり大きくしないと、気流の流入角の変化
への対応性が損なわれることで、翼の前縁部の負圧面側
において気流の剥離が生じ易くなり、空力騒音の発生と
か空力性能の低下等の問題が生じることになる。
However, in such an airfoil blade, the responsiveness to a change in the inflow angle of the airflow is impaired unless the blade thickness at the leading edge of the airflow inlet blade is considerably increased. Therefore, separation of the airflow is likely to occur on the negative pressure side of the leading edge of the blade, which causes problems such as generation of aerodynamic noise and deterioration of aerodynamic performance.

【0004】また、かかる問題に対処すべく翼の前縁部
の翼厚を大きくすると、翼厚が大きくなった分だけ翼の
前縁部に流入する気流の抵抗が増加して送風効率が低下
するという新たな問題を生じることになる。
If the thickness of the leading edge of the blade is increased to address such a problem, the resistance of the airflow flowing into the leading edge of the blade is increased by the increase in the thickness of the blade, and the blowing efficiency is reduced. A new problem.

【0005】そこで本願発明は、前縁部の翼厚増大を伴
うことなく、翼の負圧面の前縁部側での気流の剥離の抑
制と後縁部側での翼面境界層の発達の抑制とを共に実現
し、これらの相乗効果により、空力騒音の低下と空力性
能の向上との両立を可能とした送風機用羽根車を提供す
ることを目的とするものである。
Accordingly, the present invention suppresses the separation of airflow on the leading edge side of the suction surface of the blade and the development of the boundary layer on the trailing edge side without increasing the blade thickness of the leading edge. An object of the present invention is to provide an impeller for a blower which realizes both suppression and a synergistic effect thereof, thereby enabling both reduction of aerodynamic noise and improvement of aerodynamic performance.

【0006】[0006]

【課題を解決するための手段】本願発明ではかかる課題
を解決するための具体的手段として次のような構成を採
用している。
Means for Solving the Problems In the present invention, the following configuration is adopted as specific means for solving such problems.

【0007】本願の第1の発明では、翼厚が前縁部2a
から後縁部2bにかけて連続的に漸減変化するとともに
翼内部に空室部23が形成された中空の翼2,2,・・
を備えた送風機用羽根車において、上記翼2の負圧面2
Bにおける前縁部2aの近傍に該負圧面2Bの表面と上
記空室部23とを連通する複数個の小孔4,4,・・を
形成するとともに、上記負圧面2Bにおける後縁部2b
の近傍には該負圧面2Bの表面と上記空室部23とを連
通し且つ周方向に延びる長穴5を形成したことを特徴と
している。
In the first aspect of the present invention, the blade thickness is reduced to the leading edge 2a.
To the trailing edge 2b, and the hollow wings 2, 2,.
In the impeller for a blower provided with the negative pressure surface 2
A plurality of small holes 4, 4,... Communicating the surface of the suction surface 2B and the vacant space portion 23 are formed in the vicinity of the front edge portion 2a in B, and the rear edge portion 2b of the suction surface 2B is formed.
Is characterized in that a long hole 5 extending in the circumferential direction and communicating the surface of the negative pressure surface 2B with the empty space portion 23 is formed in the vicinity of.

【0008】本願の第2の発明では、上記第1の発明に
かかる送風機用羽根車において、上記小孔4を、上記負
圧面2Bの表面側から上記空室部23に向かってその孔
径が拡大する形状としたことを特徴としている。
According to a second aspect of the present invention, in the impeller for a blower according to the first aspect, the diameter of the small hole 4 is increased from the surface side of the negative pressure surface 2B toward the cavity 23. It is characterized in that it has a shape that does.

【0009】本願の第3の発明では、上記第1又は第2
の発明にかかる送風機用羽根車において、上記長穴5の
開口面積を、上記複数個の小孔4,4,・・の翼表面側
における開口面積の総和よりも大きくしたことを特徴と
している。
In the third invention of the present application, the first or the second
The blower impeller according to the invention is characterized in that the opening area of the elongated hole 5 is larger than the sum of the opening areas of the plurality of small holes 4, 4,... On the blade surface side.

【0010】本願の第4の発明では、上記第1,第2又
は第3の発明にかかる送風機用羽根車において、上記翼
2を、該翼2の負圧面2B側の面に凹部24を備えた翼
本体21と、上記翼本体21の凹部24を覆蓋する如く
該凹部24に嵌合してこれとの間に上記空室部23を形
成し得る蓋状形態をもつとともに上記翼2の前縁部2a
の近傍に対応する部位に上記複数個の小孔4,4,・・
を、また後縁部2bの近傍に対応する部位に上記長穴5
をそれぞれ設けた蓋体22とを、合体接合して構成した
ことを特徴としている。
According to a fourth aspect of the present invention, in the impeller for a blower according to the first, second or third aspect, the blade 2 is provided with a concave portion 24 on the surface of the blade 2 on the side of the negative pressure surface 2B. The wing body 21 has a lid-like form that fits into the recess 24 so as to cover the recess 24 of the wing body 21 so as to form the empty space 23 therebetween. Edge 2a
Are provided in a portion corresponding to the vicinity of the plurality of small holes 4, 4,.
And a slot 5 corresponding to the vicinity of the trailing edge 2b.
And a lid 22 provided with each of them is united and joined.

【0011】本願の第5の発明では、上記第4の発明に
かかる送風機用羽根車において、上記翼本体21をハブ
3と一体的に形成したことを特徴としている。
A fifth invention of the present application is the blower impeller according to the fourth invention, characterized in that the wing body 21 is formed integrally with the hub 3.

【0012】[0012]

【発明の効果】本願発明ではかかる構成とすることによ
り次のような効果が得られる。
According to the present invention, the following effects can be obtained by adopting such a configuration.

【0013】 本願の第1の発明にかかる送風機用羽
根車によれば、翼内部に空室部23が形成された中空の
翼2,2,・・の負圧面2Bにおける前縁部2aの近傍
に該負圧面2Bの表面と上記空室部23とを連通する複
数個の小孔4,4,・・を形成するとともに、上記負圧
面2Bにおける外周縁部2c寄りの後縁部2bの近傍に
は該負圧面2Bの表面と上記空室部23とを連通し且つ
周方向に延びる長穴5を形成しているので、羽根車が回
転する場合、その回転に伴って生じる翼端渦10(即
ち、上記翼2の外周縁部2cに圧力面2A側から負圧面
2B側に回り込み且つ該負圧面2Bに沿って外周縁部2
c側に流れる渦流。図4を参照)が上記長穴5部分を流
れることで該長穴5部分にエゼクタ作用が働き、上記空
室部23内の空気を上記長穴5を通して上記負圧面2B
の表面側に吸い出す方向の吸引力が生じる。そして、こ
の長穴5部分に生じた吸引作用は、上記空室部23を介
して上記前縁部2a側に設けた上記小孔4,4,・・部
分に伝達され、該前縁部2a部分に流入する空気の一部
は該小孔4,4,・・から上記空室部23内に吸い込ま
れ、さらに上記長穴5を通って後縁部2b側に流出する
ことになる。
According to the impeller for a blower according to the first invention of the present application, the vicinity of the leading edge 2a in the suction surface 2B of the hollow blades 2, 2,... A plurality of small holes 4, 4,... Communicating the surface of the suction surface 2B and the vacant space portion 23 are formed in the suction surface 2B and near the rear edge 2b near the outer peripheral edge 2c in the suction surface 2B. Has a long hole 5 which communicates the surface of the negative pressure surface 2B with the vacant space portion 23 and extends in the circumferential direction. Therefore, when the impeller rotates, the blade tip vortex 10 generated with the rotation is formed. (That is, the blade 2 wraps around the outer peripheral edge 2c from the pressure surface 2A side to the negative pressure surface 2B side and extends along the negative pressure surface 2B.
Eddy current flowing to c side. 4) flows through the elongated hole 5 to act as an ejector on the elongated hole 5 to allow the air in the vacant space 23 to pass through the elongated hole 5 to the suction surface 2B.
A suction force in the direction of suction is generated on the surface side of the surface. The suction action generated in the elongated hole 5 is transmitted to the small holes 4, 4,... Provided on the front edge portion 2a side through the empty space portion 23, and the front edge portion 2a A part of the air flowing into the portion is sucked into the vacant space portion 23 from the small holes 4, 4,... And further flows out to the rear edge portion 2b through the long hole 5.

【0014】この結果、上記翼2の負圧面2Bの前縁部
2a側においては、ここに流入する空気流に対して上記
小孔4,4,・・部分において上記空室部23内への吸
引作用が働くことで、該前縁部2aの表面における空気
流の剥離が可及的に抑制されることになる。また一方、
負圧面2Bの外周縁部2c寄りの後縁部2b側において
は、上記空室部23側から上記長穴5を通って負圧面2
Bの表面側に流出する空気流によって該後縁部2b部分
の表面での空気流に乱れが生じ、該表面での翼面境界層
の発達が可及的に抑制されることになる。これら両者の
相乗効果により、空力騒音が低く且つ空力性能に優れた
送風機用羽根車を提供することが可能となるものであ
る。
As a result, on the side of the leading edge 2a of the suction surface 2B of the blade 2, the small holes 4, 4,... With the suction effect, the separation of the airflow on the surface of the front edge 2a is suppressed as much as possible. Meanwhile,
On the rear edge 2b side of the negative pressure surface 2B near the outer peripheral edge 2c, the negative pressure surface 2 passes through the slot 5 from the vacant space 23 side.
The airflow flowing to the surface side of B causes turbulence in the airflow on the surface of the trailing edge portion 2b, and the development of the wing surface boundary layer on the surface is suppressed as much as possible. The synergistic effect of these two makes it possible to provide an impeller for a blower that has low aerodynamic noise and excellent aerodynamic performance.

【0015】 本願の第2の発明にかかる送風機用羽
根車によれば、上記第1の発明にかかる送風機用羽根車
において、上記小孔4を、上記負圧面2Bの表面側から
上記空室部23に向かってその孔径が拡大する形状とし
ているので、該小孔4部分に対して空室部23側からの
吸込力が効果的に作用し、空気流は上記小孔4を通して
滑らかに吸い込まれ、上記負圧面2Bの前縁部2a部分
における気流の剥離抑制効果がさらに高められるととも
に、例えば上記小孔4を同径の直孔とする場合に比し
て、該小孔4の上記負圧面2Bの表面での開口面積が小
さいことから、該小孔4の形成が空力騒音に与える影響
が可及的に軽減され、これらにより上記に記載の効果
がより一層高められるものである。
According to the impeller for a blower according to the second invention of the present application, in the impeller for the blower according to the first invention, the small hole 4 is formed by the vacant portion from the surface side of the negative pressure surface 2B. Since the hole diameter is increased toward 23, the suction force from the vacant space 23 side effectively acts on the small hole 4 portion, and the air flow is smoothly sucked through the small hole 4. The effect of suppressing the separation of the airflow at the front edge portion 2a of the suction surface 2B is further enhanced, and the suction surface of the small holes 4 is smaller than when, for example, the small holes 4 are straight holes having the same diameter. Since the opening area on the surface of 2B is small, the influence of the formation of the small holes 4 on the aerodynamic noise is reduced as much as possible, whereby the effects described above are further enhanced.

【0016】 本願の第3の発明にかかる送風機用羽
根車によれば、上記長穴5の開口面積を、上記複数個の
小孔4,4,・・の翼表面側における開口面積の総和よ
りも大きくしているので、上記小孔4,4,・・から上
記空室部23内に吸い込まれ上記長穴5から流出する空
気流のスムーズな流れが実現され、上記に記載の効果
がさらに高められることになる。
According to the impeller for a blower according to the third invention of the present application, the opening area of the long hole 5 is determined by the sum of the opening areas of the plurality of small holes 4 on the blade surface side. , A smooth flow of the air flow sucked into the vacant space portion 23 from the small holes 4, 4,... And flowing out from the long hole 5 is realized, and the effect described above is further enhanced. Will be enhanced.

【0017】 本願の第4の発明にかかる送風機用羽
根車によれば、上記翼2を、該翼2の負圧面2B側の面
に凹部24を備えた翼本体21と、上記翼本体21の凹
部24を覆蓋する如く該凹部24に嵌合してこれとの間
に上記空室部23を形成し得る蓋状形態をもつとともに
上記翼2の前縁部2aの近傍に対応する部位に上記複数
個の小孔4,4,・・を、また後縁部2bの近傍に対応
する部位に上記長穴5をそれぞれ設けた蓋体22とを、
合体接合して構成している。
According to the impeller for a blower according to the fourth invention of the present application, the wing 2 is provided with a wing body 21 having a concave portion 24 on a surface of the wing 2 on the side of the negative pressure surface 2B, It has a lid-like form that fits into the concave portion 24 so as to cover the concave portion 24 and can form the vacant space 23 therebetween, and has A plurality of small holes 4, 4,... And a lid 22 provided with the long hole 5 at a position corresponding to the vicinity of the rear edge 2b.
It is configured by uniting and joining.

【0018】従って、例えば翼2をブロア成形等によっ
て一体的に形成する場合には、上記小孔4を、上記負圧
面2Bの表面側から上記空室部23に向かってその孔径
が拡大する形状にはできないが、上記翼2を上記のよう
に翼本体21と蓋体22の別体構造とすることで上記小
孔4の上記の如き形状の設定が可能となり、結果的に上
記に記載の効果がより確実に実現されることになる。
Therefore, for example, when the blade 2 is integrally formed by blow molding or the like, the small hole 4 is formed in a shape in which the hole diameter increases from the surface side of the negative pressure surface 2B toward the empty space portion 23. However, by forming the wing 2 as a separate structure of the wing body 21 and the lid 22 as described above, it becomes possible to set the shape of the small hole 4 as described above. The effect will be more reliably realized.

【0019】また、上記翼2をブロア成形等によって一
体的に形成する場合には、該翼2の内部に設けられる上
記空室部23の形状、延いては該空室部23に対応する
部分の肉厚を設計通りとすることは難しいが、上記翼2
を上記のように翼本体21と蓋体22の別体構造としこ
れらをそれぞれ型成形とすることで、上記空室部23の
形状、及び該空室部23に対応する部分の肉厚を設計通
りとすることが容易であり、それだけ製品としての翼2
の信頼性が向上するものである。
When the wings 2 are integrally formed by blow molding or the like, the shape of the vacant space 23 provided inside the wing 2 and, consequently, a portion corresponding to the vacant space 23 It is difficult to keep the thickness of the wings as designed,
Is formed as a separate structure of the wing main body 21 and the lid 22 as described above, and these are formed by molding, respectively, thereby designing the shape of the above-mentioned empty space portion 23 and the thickness of the portion corresponding to the empty space portion 23. It is easy to do as it is, and that is the wing 2 as a product
Reliability is improved.

【0020】 本願の第5の発明にかかる送風機用羽
根車によれば、上記翼本体21をハブ3と一体的に形成
しているので、例えば翼2とハブ3とを別体構造とし、
事後的にこれを組み付けて羽根車を得る場合に比して、
該羽根車の製造が容易であり、それだけコストダウンが
期待できるものである。
According to the impeller for a blower according to the fifth invention of the present application, since the wing body 21 is formed integrally with the hub 3, for example, the wing 2 and the hub 3 have a separate structure,
Compared to the case of assembling this after the fact and obtaining an impeller,
The manufacture of the impeller is easy, and cost reduction can be expected accordingly.

【0021】[0021]

【発明の実施の形態】以下、本願発明にかかる送風機用
羽根車を好適な実施形態に基づいて具体的に説明する。
BEST MODE FOR CARRYING OUT THE INVENTION Hereinafter, an impeller for a blower according to the present invention will be specifically described based on a preferred embodiment.

【0022】図1には送風機に使用される樹脂製の羽根
車1の外観形態を、また図2には該羽根車1に備えられ
る翼2の平面形態を、それぞれ示しており、上記羽根車
1は、上記翼2を、ハブ3の外周面にその周方向に所定
間隔で複数枚(この実施形態ては3枚)配置して構成さ
れる。そして、特にこの実施形態のものにおいては、上
記翼2を次述する翼本体21と蓋体22とからなる接合
合体構造とするとともに、該翼本体21を上記ハブ3と
一体的に形成することで、上記羽根車1を一体構造品と
している。
FIG. 1 shows an external appearance of a resin impeller 1 used for a blower, and FIG. 2 shows a plan view of a blade 2 provided on the impeller 1, respectively. Reference numeral 1 denotes a configuration in which a plurality of blades 2 (three in this embodiment) are arranged on an outer peripheral surface of a hub 3 at predetermined intervals in a circumferential direction thereof. In particular, in this embodiment, the wing 2 has a combined structure of a wing body 21 and a lid 22 described below, and the wing body 21 is formed integrally with the hub 3. Thus, the impeller 1 is formed as an integral structure.

【0023】即ち、上記翼2は、図2及び図3に示すよ
うに、前縁部2aの翼厚を比較的厚くするとともに該前
縁部2aから後縁部2bにかけてその翼厚が次第に漸減
する断面形状をもつとともに、前縁部2aが回転方向の
前方側に跳ね出した前進翼形態をもつ中空のエアフォイ
ル翼であって、上記ハブ3の外周面に所要の翼角をもっ
て取り付けられことで、その両側面のうち、回転方向前
方に指向する側面は圧力面2A、背向する側面は負圧面
2Bとされる。そして、この翼2は、次述の翼本体21
と蓋体22とで構成される。
That is, as shown in FIGS. 2 and 3, the wing 2 has a relatively large thickness at the leading edge 2a and a gradually decreasing thickness from the leading edge 2a to the trailing edge 2b. A hollow airfoil wing having a cross-sectional shape and a forward wing shape in which a leading edge portion 2a protrudes forward in the rotational direction, and is attached to the outer peripheral surface of the hub 3 with a required wing angle. Of the two side surfaces, the side surface facing forward in the rotation direction is the pressure surface 2A, and the opposite side surface is the negative pressure surface 2B. The wing 2 is connected to a wing body 21 described below.
And a lid 22.

【0024】上記翼本体21は、その一方の側面21a
を上記圧力面2Aとするとともに、他方の側面21b
(上記負圧面2B側の側面)の翼前縁寄り位置には略扇
形の凹部24を設けて構成されている。そして、この翼
本体21は、その翼基端部2dが上記ハブ3の外周面に
所定の翼角をもって接合された状態で、上記ハブ3と共
に樹脂材による型成形で一体成形される。尚、翼本体2
1は、羽根車1に備えられる翼2,2,・・と同数だけ
設けられることは勿論である。
The wing body 21 has one side surface 21a.
Is the pressure surface 2A and the other side surface 21b
A substantially fan-shaped concave portion 24 is provided at a position near the leading edge of the blade (the side surface on the side of the negative pressure surface 2B). The wing body 21 is integrally formed with the hub 3 by molding with a resin material in a state where the wing base end 2d is joined to the outer peripheral surface of the hub 3 at a predetermined wing angle. The wing body 2
Of course, 1 is provided in the same number as the blades 2, 2,... Provided in the impeller 1.

【0025】上記蓋体22は、上記翼本体21の上記凹
部24の外縁形状に合致する平面形状をもつ所定肉厚の
蓋状体であって、上記翼本体21と同様に樹脂材の型成
形により成形され、その一方の側面22aは上記翼2の
負圧面2Bの一部を構成する。さらに、この蓋体22に
は、その型成形時に、次述する複数の小孔4,4,・・
と単一の長穴5とがそれぞれ形成されている。
The lid body 22 is a lid-like body having a predetermined thickness and a flat shape conforming to the outer edge shape of the recess 24 of the wing body 21, and is formed of a resin material in the same manner as the wing body 21. The one side surface 22a forms a part of the negative pressure surface 2B of the blade 2 described above. In addition, the lid 22 has a plurality of small holes 4, 4,.
And a single elongated hole 5, respectively.

【0026】上記小孔4は、上記蓋体22の一方の側面
22aから他方の側面22bに向けてその孔径が次第に
拡大する形状をもつものであって、上記蓋体22にはか
かる形状をもつ複数個の小孔4,4,・・が上記翼2の
前縁部2aの近傍に対応する部位に、且つその径方向の
略全域に渡って散点配置されている。一方、上記長穴5
は、上記蓋体22の後縁寄りの外周部、即ち、上記翼2
の後縁部2bで且つその外周縁部2c寄り部位に対応す
る位置において、該翼2の周方向に延びるように形成さ
れている。そして、上記各小孔4,4,・・と上記長穴
5との間においては、該各小孔4,4,・・の上記負圧
面2Bの表面における開口面積の総和が、上記長穴5の
上記負圧面2Bの表面における開口面積よりも小さくな
るように設定されている。
The small hole 4 has such a shape that the diameter of the hole gradually increases from one side surface 22a of the lid 22 to the other side surface 22b, and the lid 22 has such a shape. A plurality of small holes 4, 4,... Are scattered at locations corresponding to the vicinity of the leading edge 2a of the wing 2 and over substantially the entire area in the radial direction. On the other hand, the slot 5
The outer periphery of the lid 22 near the rear edge, that is, the wing 2
The wing 2 is formed to extend in the circumferential direction of the blade 2 at a position corresponding to a portion near the outer peripheral edge 2c of the trailing edge 2b. Between the small holes 4, 4,... And the long hole 5, the sum of the opening areas of the small holes 4, 4,. 5 is set to be smaller than the opening area on the surface of the negative pressure surface 2B.

【0027】このように形成された上記翼本体21の上
記凹部24に対して、これをその上方から覆蓋する如く
上記蓋体22を嵌合させて合体しこれら両者を接合する
ことで、図3に示すように、その内部に上記凹部24で
構成される空室部23を備えたエアフォイル翼形状をも
つ翼2が得られるものである。そして、このように上記
翼本体21と蓋体22とを合体させて構成された翼2に
おいては、その負圧面2Bにおける前縁部2aの近傍に
は予め上記蓋体22に設けられた上記小孔4,4,・・
が、また該負圧面2Bにおける後縁部2bの近傍には予
め上記蓋体22に設けられた上記長穴5が、それぞれ配
置されることになる。
By fitting the lid 22 into the recess 24 of the wing body 21 formed as described above so as to cover the recess 24 from above, the two are joined, and these are joined together, as shown in FIG. As shown in FIG. 5, the blade 2 having an airfoil blade shape having a cavity 23 formed therein with the recess 24 is obtained. In the wing 2 configured by combining the wing body 21 and the lid 22 in this way, the small pressure surface previously provided on the lid 22 in the vicinity of the front edge 2a on the suction surface 2B. Hole 4,4, ...
However, the elongated holes 5 previously provided in the lid 22 are arranged in the vicinity of the trailing edge 2b on the negative pressure surface 2B.

【0028】以上の如き構成をもつ羽根車1において
は、次のような作用効果が得られる。
In the impeller 1 having the above configuration, the following operation and effect can be obtained.

【0029】即ち、上記羽根車が回転する場合、その回
転に伴って上記翼2の外周縁部2cには、図1,図2及
び図4に示すように、その圧力面2A側から負圧面2B
側に回り込み該負圧面2Bに沿って外周縁部2c側へ流
れる翼端渦10が形成され、しかもこの翼端渦10は、
上記翼2の前縁部2aから後縁部2bにかけて次第に発
達するものである(図1及び図2参照)。従って、上記
長穴5は、上記翼端渦10が最も発達した部位に位置す
ることになり、該長穴5部分には、上記翼端渦10の流
れによるエゼクタ効果が働き、該長穴5を通して上記空
室部23内の空気を負圧面2Bの表面側に吸い出す方向
の吸引作用が生じる。そして、この長穴5部分に生じた
吸引作用は、上記空室部23を介して上記前縁部2a側
に設けた上記小孔4,4,・・部分に伝達され、上記前
縁部2a部分に流入する空気に対してこれを上記各小孔
4,4,・・を通して上記空室部23内に引き込む方向
の吸引作用が働く。この結果、上記前縁部2aに流入し
た空気流の一部は、図3に流線Aで示すように、該小孔
4,4,・・を通って上記空室部23内に吸い込まれ、
さらに該空室部23内を上記長穴5側に向かって流れた
後、該長穴5から再度負圧面2Bにおける後縁部2b側
の表面に流出し、後流となる。
That is, when the impeller rotates, the outer peripheral edge 2c of the blade 2 is rotated from the pressure surface 2A side to the suction surface as shown in FIGS. 1, 2 and 4 with the rotation. 2B
The tip vortex 10 is formed around the suction side 2B and flows toward the outer peripheral edge 2c along the suction surface 2B.
It develops gradually from the leading edge 2a to the trailing edge 2b of the wing 2 (see FIGS. 1 and 2). Therefore, the slot 5 is located at a position where the tip vortex 10 is most developed, and the ejector effect due to the flow of the tip vortex 10 acts on the slot 5, thereby causing the slot 5 to flow. The suction action in the direction of sucking the air in the vacant space portion 23 to the surface side of the negative pressure surface 2B occurs. The suction effect generated in the elongated hole 5 is transmitted to the small holes 4, 4,... Provided on the front edge portion 2a side through the empty space portion 23, and the front edge portion 2a A suction action is performed on the air flowing into the portion through the small holes 4, 4,. As a result, a part of the airflow flowing into the front edge portion 2a is sucked into the empty space portion 23 through the small holes 4, 4,. ,
Further, after flowing toward the long hole 5 side in the vacant space portion 23, it flows out again from the long hole 5 to the surface of the negative pressure surface 2B on the trailing edge portion 2b side, and becomes a downstream flow.

【0030】このように上記空室部23を介して上記負
圧面2Bにおける上記前縁部2a側から後縁部2b側へ
流れる空気流が生じる結果、先ず、上記翼2の負圧面2
Bの前縁部2a側においては、空気流に対して上記小孔
4,4,・・部分で上記空室部23内への吸引作用が働
くことで、該前縁部2aの表面における空気流の剥離が
可及的に抑制される。一方、上記負圧面2Bの後縁部2
b側においては、上記空室部23側から上記長穴5を通
って負圧面2Bの表面側に流出する空気流によって該後
縁部2b部分の表面での空気流に乱れが生じ、該表面で
の翼面境界層の発達が可及的に抑制される。これら両者
の相乗効果により、上記羽根車1は、空力騒音が低く且
つ空力性能に優れた特性を得ることになる。
As described above, as a result of the generation of the airflow flowing from the leading edge 2a to the trailing edge 2b on the suction surface 2B through the vacant space 23, the suction surface 2
On the front edge 2a side of B, the suction action into the vacant space 23 at the small holes 4, 4,... Acts on the air flow, so that the air on the surface of the front edge 2a Flow separation is suppressed as much as possible. On the other hand, the trailing edge 2 of the negative pressure surface 2B
On the b side, the air flow from the vacant space portion 23 side to the surface side of the negative pressure surface 2B through the long hole 5 causes turbulence in the air flow on the surface of the trailing edge portion 2b. The development of the wing surface boundary layer at the site is suppressed as much as possible. Due to the synergistic effect of these two, the impeller 1 has characteristics of low aerodynamic noise and excellent aerodynamic performance.

【0031】また、この場合、上記翼2の前縁部2aの
近傍に設けられる上記小孔4は、上記負圧面2Bの表面
側から上記空室部23に向かってその孔径が拡大する形
状とされているので、該小孔4部分に対して空室部23
側からの吸込力が効果的に作用することになる。この結
果、空気流は上記小孔4を通して滑らかに吸い込まれ、
上記負圧面2Bの前縁部2a部分における気流の剥離抑
制効果がさらに高められるとともに、例えば上記小孔4
を同径の直孔とする場合に比して、該小孔4の上記負圧
面2Bの表面での開口面積が小さいことから、該小孔4
の形成が空力騒音に与える影響が可及的に軽減されるこ
とになる。
In this case, the small hole 4 provided in the vicinity of the leading edge 2a of the blade 2 has a shape in which the hole diameter increases from the surface side of the negative pressure surface 2B toward the empty space 23. Therefore, the vacant space portion 23 is
The suction force from the side will work effectively. As a result, the air flow is smoothly sucked through the small holes 4,
The effect of suppressing the separation of the airflow at the front edge portion 2a of the negative pressure surface 2B is further enhanced.
Since the opening area of the small holes 4 on the surface of the negative pressure surface 2B is smaller than when the
The effect on the aerodynamic noise due to the formation of the air-fuel ratio is reduced as much as possible.

【0032】さらに、上記空室部23内に吸入されて上
記小孔4,4,・・側から上記長穴5側に流れる空気流
は翼2の回転に伴う遠心力を受けて外周寄りに次第に偏
向せしめられるが、この場合、上記長穴5が上記負圧面
2Bにおける外周縁部2c寄りの後縁部2bに設けられ
ているため、上記空室部23内における空気流の集合位
置とその出口となる上記長穴5の形成位置とが略合致
し、該長穴5からの空気流の吹出がよりスムーズとな
り、それだけ空力騒音の低減及び空力性能の向上がさら
に促進されるものである。
Further, the air flow sucked into the vacant space portion 23 and flowing from the small holes 4, 4,... To the long hole 5 side receives centrifugal force due to the rotation of the blade 2 and moves toward the outer periphery. In this case, since the elongated hole 5 is provided at the rear edge 2b of the negative pressure surface 2B near the outer peripheral edge 2c, the position of the air flow in the vacant space 23 and its position The formation position of the slot 5 serving as an outlet substantially matches the position of the slot 5, so that the air flow from the slot 5 is blown out more smoothly, which further reduces aerodynamic noise and improves aerodynamic performance.

【0033】また、上記長穴5の開口面積を、上記複数
個の小孔4,4,・・の翼表面側における開口面積の総
和よりも大きくしているので、上記小孔4,4,・・か
ら上記空室部23内に吸い込まれ、さらに上記長穴5か
ら流出する空気流のスムーズな流れが実現され、空力騒
音の低減及び空力性能のさらなる向上が期待できるもの
である。
Since the opening area of the long hole 5 is larger than the sum of the opening areas of the plurality of small holes 4, 4,... On the blade surface side, the small holes 4, 4,. ················ Smooth flow of the air flow sucked into the vacant space portion 23 and flowing out of the long hole 5 is realized, and reduction of aerodynamic noise and further improvement of aerodynamic performance can be expected.

【0034】一方、この実施形態のものにおいては、上
記翼2を、翼本体21と、該翼本体21に合体せしめら
れるとともに上記小孔4,4,・・と長穴5とを予め形
成した上記蓋体22とで構成しているので、上記小孔4
が上記負圧面2Bの表面側から上記空室部23に向かっ
てその孔径が拡大する形状であってもこれを容易に形成
することができるとともに、上記空室部23の形状、及
び該空室部23に対応する部分の肉厚を設計通りに製作
することも容易である。
On the other hand, in this embodiment, the wing 2 is combined with the wing body 21 and the small holes 4, 4,... And the long hole 5 are formed in advance. Since it is composed of the lid 22, the small hole 4
Can easily be formed even when the hole diameter increases from the surface side of the negative pressure surface 2B toward the vacant space 23, and the shape of the vacant space 23 and the vacant space It is also easy to manufacture the thickness corresponding to the portion 23 as designed.

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

【図1】本願発明にかかる送風機用羽根車の全体斜視図
である。
FIG. 1 is an overall perspective view of an impeller for a blower according to the present invention.

【図2】図1に示した羽根車における翼の平面図であ
る。
FIG. 2 is a plan view of a blade in the impeller shown in FIG.

【図3】図2のIII−III拡大断面図である。FIG. 3 is an enlarged sectional view taken along the line III-III of FIG. 2;

【図4】図2のIV−IV拡大断面図である。FIG. 4 is an enlarged sectional view taken along line IV-IV of FIG. 2;

【符号の説明】[Explanation of symbols]

1は羽根車、2は翼、2Aは圧力面、2Bは負圧面、2
aは前縁部、2bは後縁部、2cは外周縁部、3はハ
ブ、4は小孔、5は長穴、10は翼端渦、21は翼本
体、22は蓋体、23は空室部、24は凹部である。
1 is an impeller, 2 is a blade, 2A is a pressure surface, 2B is a suction surface, 2
a is a leading edge, 2b is a trailing edge, 2c is an outer peripheral edge, 3 is a hub, 4 is a small hole, 5 is a long hole, 10 is a wing tip vortex, 21 is a wing body, 22 is a lid, 23 is The vacant space 24 is a concave portion.

フロントページの続き (58)調査した分野(Int.Cl.7,DB名) F04D 29/18 - 29/38 F04D 29/66 Continuation of front page (58) Field surveyed (Int.Cl. 7 , DB name) F04D 29/18-29/38 F04D 29/66

Claims (5)

(57)【特許請求の範囲】(57) [Claims] 【請求項1】 翼厚が前縁部(2a)から後縁部(2
b)にかけて連続的に漸減変化するとともに翼内部に空
室部(23)が形成された中空の翼(2),(2),・
・を備えた送風機用羽根車であって、 上記翼(2)の負圧面(2B)における前縁部(2a)
の近傍に該負圧面(2B)の表面と上記空室部(23)
とを連通する複数個の小孔(4),(4),・・が形成
されるとともに、上記負圧面(2B)における外周縁部
(2c)寄りの後縁部(2b)の近傍には該負圧面(2
B)の表面と上記空室部(23)とを連通し且つ周方向
に延びる長穴(5)が形成されていることを特徴とする
送風機用羽根車。
The wing thickness is increased from the leading edge (2a) to the trailing edge (2).
b) Hollow wings (2), (2),.
The impeller for a blower comprising: a leading edge (2a) on the suction surface (2B) of the blade (2).
Near the surface of the suction surface (2B) and the vacant space (23).
Are formed, and a plurality of small holes (4), (4),... Are formed, and an outer peripheral edge of the negative pressure surface (2B) is formed.
(2c) Near the rear edge (2b) near the suction surface (2c).
An impeller for a blower, characterized in that an elongated hole (5) extending in the circumferential direction is formed so as to communicate the surface of (B) with the empty space (23).
【請求項2】 請求項1において、 上記小孔(4)が、上記負圧面(2B)の表面側から上
記空室部(23)に向かってその孔径が拡大する形状で
あることを特徴とする送風機用羽根車。
2. The small hole (4) according to claim 1, wherein a diameter of the small hole (4) increases from a surface side of the negative pressure surface (2B) toward the empty space portion (23). Impeller for blowers.
【請求項3】 請求項1又は2において、 上記長穴(5)の開口面積を、上記複数個の小孔
(4),(4),・・の翼表面側における開口面積の総
和よりも大きくしたことを特徴とする送風機用羽根車。
3. The method of claim 1 or 2, the opening area of the slot (5), the plurality of small holes (4), (4), than the sum of the opening area of the blade surface side of ... An enlarged impeller for a blower.
【請求項4】 請求項1,2又は3において、 上記翼(2)が、 該翼(2)の負圧面(2B)側の面に凹部(24)を備
えた翼本体(21)と、上記翼本体(21)の上記凹部
(24)を覆蓋する如く該凹部(24)に嵌合してこれ
との間に上記空室部(23)を形成し得る蓋状形態をも
つとともに上記翼(2)の前縁部(2a)の近傍に対応
する部位に上記複数個の小孔(4),(4),・・を、
また後縁部(2b)の近傍に対応する部位に上記長穴
(5)をそれぞれ設けた蓋体(22)とを、合体接合し
て構成されていることを特徴とする送風機用羽根車。
4. A wing body (21) according to claim 1, 2 or 3, wherein said wing (2) is provided with a concave portion (24) on a surface of the wing (2) on the side of the suction surface (2B). The wing has a lid-like form capable of fitting into the concave portion (24) so as to cover the concave portion (24) of the wing body (21) and forming the empty space portion (23) therewith. The above-mentioned plurality of small holes (4), (4),... Are provided in a portion corresponding to the vicinity of the front edge (2a) of (2).
Further, an impeller for a blower, wherein a lid body (22) provided with the elongated hole (5) at a position corresponding to the vicinity of the rear edge part (2b) is united and joined.
【請求項5】 請求項4において、 上記翼本体(21)がハブ(3)と一体的に形成されて
いることを特徴とする送風機用羽根車。
5. An impeller for a blower according to claim 4, wherein said wing body (21) is formed integrally with said hub (3).
JP10175506A 1998-06-23 1998-06-23 Impeller for blower Expired - Fee Related JP3008930B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP10175506A JP3008930B2 (en) 1998-06-23 1998-06-23 Impeller for blower

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP10175506A JP3008930B2 (en) 1998-06-23 1998-06-23 Impeller for blower

Publications (2)

Publication Number Publication Date
JP2000009096A JP2000009096A (en) 2000-01-11
JP3008930B2 true JP3008930B2 (en) 2000-02-14

Family

ID=15997245

Family Applications (1)

Application Number Title Priority Date Filing Date
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Country Status (1)

Country Link
JP (1) JP3008930B2 (en)

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Also Published As

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LAPS Cancellation because of no payment of annual fees