JP3071287B2 - Blower impeller - Google Patents

Blower impeller

Info

Publication number
JP3071287B2
JP3071287B2 JP4008804A JP880492A JP3071287B2 JP 3071287 B2 JP3071287 B2 JP 3071287B2 JP 4008804 A JP4008804 A JP 4008804A JP 880492 A JP880492 A JP 880492A JP 3071287 B2 JP3071287 B2 JP 3071287B2
Authority
JP
Japan
Prior art keywords
blade
impeller
pressure
hollow layer
surface side
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
JP4008804A
Other languages
Japanese (ja)
Other versions
JPH05196243A (en
Inventor
浩一 酒井
潔 佐野
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Panasonic Corp
Panasonic Holdings Corp
Original Assignee
Panasonic Corp
Matsushita Electric Industrial Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Panasonic Corp, Matsushita Electric Industrial Co Ltd filed Critical Panasonic Corp
Priority to JP4008804A priority Critical patent/JP3071287B2/en
Publication of JPH05196243A publication Critical patent/JPH05196243A/en
Application granted granted Critical
Publication of JP3071287B2 publication Critical patent/JP3071287B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/70Wind energy
    • Y02E10/72Wind turbines with rotation axis in wind direction

Landscapes

  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Air-Conditioning Room Units, And Self-Contained Units In General (AREA)

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【産業上の利用分野】本発明は複数枚の翼により構成さ
れている送風機の騒音低減を可能にする送風機羽根車の
翼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 a blade of a blower impeller which can reduce noise of a blower composed of a plurality of blades.

【0002】[0002]

【従来の技術】図6(a) は、送風機羽根車の斜視図、図
6(b) は、前記羽根車の翼断面図である。送風機羽根車
aは、円錐台状のハブ部bの外周部に4枚の翼cが取り
付けられ、従来、この種の翼cは図6(b) に示すごとく
中実な金属または樹脂を用いて、所定の設計寸法、形状
に成形し、送風機としての性能を得ていた。c′は翼c
の翼負圧面側、c″は翼圧力面側を示し、dは翼cの翼
前縁部、eは翼後縁部である。
2. Description of the Related Art FIG. 6A is a perspective view of a blower impeller, and FIG. 6B is a sectional view of the impeller blade. The blower impeller a has four blades c attached to the outer periphery of a truncated conical hub portion b. Conventionally, this type of blade c uses a solid metal or resin as shown in FIG. 6 (b). Thus, it was formed into a predetermined design size and shape to obtain the performance as a blower. c 'is the wing c
, C ″ indicates the blade pressure surface side, d indicates the blade leading edge of blade c, and e indicates the blade trailing edge.

【0003】[0003]

【発明が解決しようとする課題】しかしながら、上記の
如き構造においては図7に示すごとく羽根車aの翼cの
回転にともない、空気が翼前縁部dから翼後縁部eへ流
れさる際に、翼cの翼圧力面側c″に層流から乱流に流
れが移行する時に乱流移行点f以降で発生する圧力変動
や翼後縁部eからの後流渦gの放出にともなう翼cの揚
力変動、および前記後流渦gの放出により発生する圧力
波が翼上流側の境界層変動開始点hに伝播して翼負圧面
側c′の境界層変動開始点h以降で翼面境界層の変動i
を発生させることにより生ずる圧力脈動が高レベルであ
るために、羽根車翼面上からは広帯域のスペクトラムを
持つ乱流騒音が発生していた。
However, in the above-mentioned structure, as shown in FIG. 7, when air flows from the leading edge d to the trailing edge e of the blade a with the rotation of the blade c of the impeller a. In addition, pressure fluctuations occurring after the turbulent flow transition point f when the flow transitions from laminar flow to turbulent flow on the blade pressure surface side c ″ of the blade c, and the discharge of the wake vortex g from the blade trailing edge e. The pressure wave generated by the fluctuation of the lift of the blade c and the discharge of the wake vortex g propagates to the boundary layer fluctuation start point h on the upstream side of the blade, and the blade moves after the boundary layer fluctuation start point h on the blade suction side c ′. Variation of surface boundary layer i
Because of the high level of pressure pulsation caused by the generation of turbulence, turbulent noise having a broadband spectrum has been generated on the impeller blade surface.

【0004】本発明は、従来例で発生していた羽根車翼
面上の各種圧力変動および圧力波の発生を抑制し、送風
機の性能を低下させることなく、前記羽根車翼面上から
発生する前記乱流騒音を低減する送風機羽根車を提供す
るものである。
The present invention suppresses the occurrence of various pressure fluctuations and pressure waves on the impeller blade surface, which occur in the conventional example, and generates the pressure waves from the impeller blade surface without deteriorating the performance of the blower. An object of the present invention is to provide a fan impeller for reducing the turbulent noise.

【0005】[0005]

【課題を解決するための手段】上記、従来例で見られた
欠点を解決するために本発明は、送風機羽根車を構成す
る複数枚の翼の内部に中空層を設け、翼の全面、また
は、少なくとも翼圧力面側または翼負圧面側の一部に、
中空層と外部が連通する多数の小孔または連続気孔を持
つポーラスな圧力変動緩衝部材を使用している。
SUMMARY OF THE INVENTION In order to solve the above-mentioned drawbacks in the conventional example, the present invention provides a blower impeller having a hollow layer inside a plurality of blades, , At least a part of the blade pressure surface side or the blade suction surface side,
A porous pressure fluctuation cushioning member having a number of small holes or continuous pores in which the hollow layer communicates with the outside is used.

【0006】また、本発明は、翼の少なくとも前縁部側
または後縁部側の一部に、中空層と外部が連通する多数
の小孔または連続気孔を持つポーラスな圧力変動緩衝部
材を使用している。
Further, the present invention uses a porous pressure fluctuation cushioning member having a large number of small holes or continuous pores in which the hollow layer communicates with the outside at least at a part of the leading edge side or the trailing edge side of the blade. doing.

【0007】また、本発明は、送風機羽根車を構成する
複数枚の翼の内部に中空層を設け、翼の後縁部側に中空
層と外部が連通する短管を設け静圧のみをうける共鳴型
消音器を備えている。
Further, according to the present invention, a hollow layer is provided inside a plurality of blades constituting a fan impeller, and a short pipe communicating between the hollow layer and the outside is provided on the trailing edge side of the blade to receive only static pressure. It has a resonance type silencer.

【0008】また、本発明は、送風機羽根車を構成する
複数枚の翼の内部に中空層を設け、翼の全面、または、
少なくとも翼圧力面側または翼負圧面側の一部に、中空
層と外部が連通し、静圧のみをうけるように流体の流れ
方向に傾斜させた短管を設けた共鳴型消音器を備えてい
る。
Further, according to the present invention, a hollow layer is provided inside a plurality of blades constituting a fan impeller, and the entire surface of the blades or
At least a part of the blade pressure surface side or the blade suction surface side is provided with a resonance type silencer provided with a short pipe in which the hollow layer communicates with the outside and is inclined in the fluid flow direction so as to receive only static pressure. I have.

【0009】[0009]

【作用】上記構成により、本発明の送風機羽根車は、羽
根車の翼の内部に中空層を設け、翼の前面、または、少
なくとも圧力面側または負圧面側の一部に、中空層と外
部が連通する小孔または連続気孔を持つポーラスな圧力
変動緩和部材を用いているために、空気が羽根車の翼前
縁部から、翼後縁部へ流れさる際に、翼圧力面側または
翼負圧面側において発生する騒音をポーラスな圧力変動
緩和部材が吸音し、さらに翼内部の中空層が共鳴型消音
器の構造をとることにより消音を図る。
According to the above construction, the blower impeller of the present invention is provided with a hollow layer inside the blade of the impeller, and the hollow layer is provided on the front surface of the blade or at least a part on the pressure side or the suction side. When the air flows from the leading edge of the impeller to the trailing edge of the impeller, the air pressure is reduced to the side of the impeller or the impeller. The noise generated on the negative pressure side is absorbed by the porous pressure fluctuation reducing member, and the hollow layer inside the blade has a resonance type silencer structure to reduce noise.

【0010】また、圧力面側と負圧面側の両面にポーラ
スな圧力変動緩和部材を用いると、翼面上における翼圧
力面と翼負圧面間での空気の流入、流出があるため、片
方の翼面上の圧力変動が高くなった場合は、圧力が高い
翼面上から圧力が低い翼面上へ空気が流れ、結果的には
抑制されて翼面上から発生する騒音は低減する。さら
に、翼圧力面側から翼負圧面側に空気が一部流出するた
めに、翼負圧面からの流れのはくりを抑制し、はくりに
ともなう圧力波の発生を軽減する作用がある。また、羽
根車の翼の内部に中空層を設け、翼の少なくとも前縁部
側または後縁部側の一部に、中空層と外部が連通する小
孔または連続気孔を持つポーラスな圧力変動緩和部材を
使用しているために、空気が羽根車の翼前縁部から翼後
縁部へ流れさる際に、翼前縁部での空気の衝突により発
生する騒音、および翼後縁部での後流により発生する騒
音を吸音し、さらに翼内部の中空層が共鳴型消音器の構
造をとることにより消音を図る。
When porous pressure fluctuation reducing members are used on both the pressure surface side and the suction surface side, air flows in and out between the blade pressure surface and the blade suction surface on the blade surface. When the pressure fluctuation on the wing surface becomes high, air flows from the wing surface with high pressure to the wing surface with low pressure, and as a result, the air is suppressed and the noise generated from on the wing surface is reduced. Further, since a part of the air flows out from the blade pressure surface side to the blade suction surface side, there is an effect that the flow of the flow from the blade suction surface is suppressed and the generation of the pressure wave accompanying the peeling is reduced. In addition, a hollow layer is provided inside the blade of the impeller, and at least a part of the leading edge side or the trailing edge side of the blade has pores or continuous pores communicating with the hollow layer and the outside, which alleviates porous pressure fluctuation. Due to the use of the components, the noise generated by the collision of air at the leading edge of the blade when air flows from the leading edge to the trailing edge of the impeller, The noise generated by the wake is absorbed, and the hollow layer inside the wing has a resonance-type silencer structure to reduce noise.

【0011】また、羽根車の翼の内部に中空層を設け、
翼後縁部側に中空層と外部が連通する短管を設け静圧の
みをうけるようにした共鳴型消音器の構造をとることに
より、翼後縁部での後流により発生する騒音の消音を図
る。
In addition, a hollow layer is provided inside the blade of the impeller,
Suppressing the noise generated by the wake at the trailing edge of the wing by using a resonance type silencer that has a short pipe on the trailing edge side of the wing and that communicates the outside with the hollow layer to receive only static pressure Plan.

【0012】また、羽根車の翼の内部に中空層を設け、
翼の全面、または、少なくとも圧力面側または負圧面側
の一部に、中空層と外部が連通し、静圧のみうけるよう
に流体の流れ方向に傾斜させた短管を設けた共鳴型消音
器の構造をとることにより、空気が羽根車の翼前縁部か
ら、翼後縁部へ流れさる際に、翼の圧力面側または負圧
面側において発生する騒音の消音を図ることができる。
Further, a hollow layer is provided inside the blade of the impeller,
A resonance type silencer in which the hollow layer and the outside communicate with the entire surface of the wing, or at least a part of the pressure side or the suction side, and a short pipe inclined in the fluid flow direction so as to receive only static pressure is provided. With this structure, when air flows from the leading edge of the impeller to the trailing edge of the blade, noise generated on the pressure side or the negative pressure side of the blade can be suppressed.

【0013】[0013]

【実施例】本発明の第1の実施例を図1、図2を用いて
説明する。図1(a) は送風機羽根車の斜視図、図1(b)
は前記羽根車の翼断面図、図2は羽根車の使用状態図で
ある。これらの図において、1は、送風機羽根車であっ
て、この送風機羽根車1は、羽根車ボス部2によって電
動機3に対し回転自在に取り付けられ、エアガイダ4の
開口部に対し所定の位置にくるように設置され、電動機
3は電動機支持台5に取り付け固定されている。電動機
3が駆動して所定の回転方向に前記羽根車1が回転する
と空気は図2のAから吸込まれBの方向に吹出されて送
風機として機能する。
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS A first embodiment of the present invention will be described with reference to FIGS. Fig. 1 (a) is a perspective view of a fan impeller, and Fig. 1 (b).
FIG. 2 is a sectional view of the blade of the impeller, and FIG. 2 is a diagram showing a use state of the impeller. In these figures, reference numeral 1 denotes a blower impeller. The blower impeller 1 is rotatably attached to the electric motor 3 by an impeller boss portion 2 and comes to a predetermined position with respect to the opening of the air guider 4. The motor 3 is mounted on the motor support 5 and fixed. When the electric motor 3 is driven to rotate the impeller 1 in a predetermined rotation direction, air is sucked in from A in FIG. 2 and blown out in the direction of B to function as a blower.

【0014】図1(a) (b) に示す如く、送風機羽根車1
は、円錐台状のハブ部6の外周部に翼7が取り付けられ
ている。翼7の内部には断面が流線形状の中空層8が形
成されており、この翼7の翼圧力面側7aと翼負圧面側
7bの主要部は、ポーラスな部材、例えば多数の小孔、
または連続気孔状態の多孔質な金属または樹脂を用いた
圧力変動緩衝部材9で形成されている。なお、圧力変動
緩衝部材9は、翼7の内部の中空層8が翼圧力面側7a
または翼負圧面側7bと連通するように取り付ける。
As shown in FIGS. 1A and 1B, a blower impeller 1
The wing 7 is attached to the outer peripheral portion of the hub 6 having a truncated cone shape. A hollow layer 8 having a streamlined cross section is formed inside the blade 7, and a main part of the blade pressure surface side 7a and the blade suction surface side 7b of the blade 7 is made of a porous member, for example, a number of small holes. ,
Alternatively, the pressure change buffer member 9 is made of a porous metal or resin in a continuous pore state. In addition, the pressure fluctuation buffering member 9 is such that the hollow layer 8 inside the blade 7 is
Alternatively, it is attached so as to communicate with the blade suction side 7b.

【0015】前記構成により羽根車1が回転すると、空
気は前記羽根車1の翼前縁部7cから翼圧力面側7aと
翼負圧面側7bに沿って流れ、翼後縁部7dから流れさ
り所定の方向へ吹き出される。その際、翼圧力面側7a
または翼負圧面側7bにおいて発生する騒音をポーラス
な圧力変動緩衝部材9が吸音するとともに、翼内部の中
空層8が共鳴型消音器の機能をはたして消音を図る。ま
た、翼圧力面側7aと翼負圧面側7bの両面にポーラス
な部材9を用いると、翼面上における前記翼圧力面側7
aと翼負圧面側7b間での空気の流入、流出があるた
め、片方の翼面上の圧力変動が高くなった場合は、圧力
が高い翼面上から圧力が低い翼面上へ空気が流出し、結
果的には抑制されて翼面上から発生する騒音は低減され
る。さらに、翼圧力面側7aから翼負圧面側7bに空気
が一部流出するために、翼負圧面からの流れのはくりを
抑制する効果もあり、はくりにともなう圧力波の発生を
軽減する作用がある。
When the impeller 1 rotates with the above configuration, air flows from the leading edge 7c of the impeller 1 along the blade pressure surface side 7a and the blade suction surface 7b, and flows from the blade trailing edge 7d. It is blown out in a predetermined direction. At this time, the blade pressure surface side 7a
Alternatively, the noise generated on the blade negative pressure surface side 7b is absorbed by the porous pressure fluctuation buffer member 9, and the hollow layer 8 inside the blade acts as a resonance type silencer to muffle the noise. Further, if porous members 9 are used on both surfaces of the blade pressure surface side 7a and the blade suction surface side 7b, the blade pressure surface side 7
a and the outflow and inflow of air between the blade suction side 7b, when the pressure fluctuation on one of the blade surfaces becomes high, the air flows from the high pressure blade surface to the low pressure blade surface. The noise that flows out and is consequently suppressed is reduced. Further, since a part of the air flows out from the blade pressure surface side 7a to the blade suction surface side 7b, there is also an effect of suppressing the separation of the flow from the blade suction surface, thereby reducing the generation of pressure waves accompanying the separation. There is action.

【0016】なお、上記実施例は、翼7の翼圧力面側7
aと翼負圧面側7bの主要部をポーラスな部材9で製作
しているが、翼圧力面側7a、または翼負圧面側7bの
一部分をポーラスな部材9で製作してもよい。
In the above embodiment, the blade pressure surface side 7 of the blade 7 is used.
Although the main part of the blade a and the blade suction surface side 7b is made of the porous member 9, the blade pressure surface side 7a or a part of the blade suction surface 7b may be made of the porous member 9.

【0017】次に、本発明の第2の実施例を図2、図3
を用いて説明する。なお、第1実施例と同一部材につい
ては同一の番号を付してある。図3(a) は送風機羽根車
の斜視図、図3(b) は前記羽根車の翼断面図である。
Next, a second embodiment of the present invention will be described with reference to FIGS.
This will be described with reference to FIG. The same members as those in the first embodiment are denoted by the same reference numerals. FIG. 3A is a perspective view of a blower impeller, and FIG. 3B is a cross-sectional view of the blade of the impeller.

【0018】図3(a)(b)に示される如く、羽根車1は円
錐台状のハブ部6の外周部に翼7が取り付けられてい
る。この翼7の一部を形成している多数の小孔、または
連続気孔状態の多孔質な金属または樹脂を用いたポーラ
スな圧力変動緩衝部材9は、翼前縁部7cと翼後縁部7
dに取り付けられ、翼前縁部7cまたは翼後縁部7dの
圧力変動緩衝部材9によって翼内部の中空層8と外部が
連通している。
As shown in FIGS. 3 (a) and 3 (b), the impeller 1 has a wing 7 attached to an outer peripheral portion of a hub 6 having a truncated cone shape. The porous pressure fluctuation buffer member 9 using a large number of small holes forming a part of the blade 7 or a porous metal or resin in a continuous pore state has a blade leading edge 7c and a blade trailing edge 7c.
d, and the hollow layer 8 inside the wing communicates with the outside by a pressure fluctuation buffering member 9 at the wing leading edge 7c or the wing trailing edge 7d.

【0019】この第2の実施例も送風機羽根車1が電動
機3に対し回転自在に取り付けられ、かつエアガイダ4
の開口部に対し所定の位置にくるように設置されて、電
動機3は電動機支持台5に取付け固定されている。電動
機3により所定の回転方向に送風機羽根車1が駆動され
ると空気は図2のAから吸込まれBの方向に吹出されて
送風機として作動する。
In this second embodiment, too, the blower impeller 1 is rotatably mounted on the electric motor 3 and the air guider 4
The motor 3 is installed at a predetermined position with respect to the opening, and the motor 3 is attached and fixed to the motor support 5. When the blower impeller 1 is driven by the electric motor 3 in a predetermined rotation direction, air is sucked in from A in FIG. 2 and is blown out in the direction of B to operate as a blower.

【0020】前記のように羽根車1が回転すると空気は
羽根車1の翼前縁部7cから、翼圧力面側7a、翼負圧
面側7bに沿って流れ、翼後縁部7dから流れさり所定
の方向へ吹き出される。その際、翼前縁部7cまたは後
縁部7dにポーラスな圧力変動緩衝部材9を用いている
ために、空気が羽根車1の翼前縁部7cから翼後縁部7
dへ流れさる際に、翼前縁部7cでの衝突により発生す
る騒音、および翼後縁部7dでの後流により発生する騒
音を吸音し、さらに翼内部の中空層8が共鳴型消音器の
構造をとり消音を図る。
When the impeller 1 rotates as described above, air flows from the blade leading edge 7c of the impeller 1 along the blade pressure side 7a and the blade suction side 7b, and flows from the blade trailing edge 7d. It is blown out in a predetermined direction. At this time, since the porous pressure fluctuation buffering member 9 is used for the wing leading edge 7c or the trailing edge 7d, air flows from the wing leading edge 7c of the impeller 1 to the wing trailing edge 7c.
d, the noise generated by the collision at the wing leading edge 7c and the noise generated by the wake at the wing trailing edge 7d are absorbed, and the hollow layer 8 inside the wing is a resonance type silencer. The structure is designed to muffle sound.

【0021】なお、上記実施例では、ポーラスな圧力変
動緩衝部材9は、翼前縁部7cと翼後縁部7dに取り付
けられているが、ポーラスな圧力変動緩衝部材9は、翼
前縁部7cまたは翼後縁部7dの一部分に取り付けても
よい。
In the above embodiment, the porous pressure fluctuation buffering member 9 is attached to the wing leading edge 7c and the wing trailing edge 7d. 7c or a part of the wing trailing edge 7d.

【0022】本発明の第3の実施例を図2、図4を用い
て説明する。なお、第1実施例と同一部材については同
一の番号を付してある。図4(a) は送風機羽根車の斜視
図、図4(b) は前記羽根車の翼断面図である。図4(a)
(b)に示される如く、送風機羽根車1は円錐台状のハブ
部6の外周部に翼7を取り付け、この翼後縁部7dに翼
内部の中空層8と連通する短管10を形成して翼後縁部
7dに開口部11を設けることによって、共鳴型消音器
の構造としている。
A third embodiment of the present invention will be described with reference to FIGS. The same members as those in the first embodiment are denoted by the same reference numerals. FIG. 4A is a perspective view of a blower impeller, and FIG. 4B is a cross-sectional view of the blade of the impeller. Fig. 4 (a)
As shown in (b), the impeller 1 of the blower has a wing 7 attached to an outer peripheral portion of a hub 6 having a truncated cone shape, and a short pipe 10 communicating with a hollow layer 8 inside the wing is formed at a trailing edge 7d of the wing. The opening 11 is provided in the wing trailing edge 7d to form a resonance type silencer.

【0023】この第3の実施例も羽根車1が羽根車ボス
部2によって電動機3に対し回転自在に取り付けられエ
アガイダ4の開口部に対し所定の位置にくるように設置
され、電動機3は電動機支持台5に取り付け固定されて
いる。前記電動機3により所定の回転方向に前記羽根車
1が駆動されると空気は図2のAから吸込まれBの方向
に放出されて送風機として作動する。
In the third embodiment, too, the impeller 1 is rotatably mounted on the electric motor 3 by the impeller boss 2 and is installed at a predetermined position with respect to the opening of the air guider 4. It is attached and fixed to the support base 5. When the impeller 1 is driven in a predetermined rotation direction by the electric motor 3, air is sucked from A in FIG. 2 and discharged in the direction of B to operate as a blower.

【0024】前記のように羽根車1が回転すると空気は
前記羽根車1の翼前縁部7cから、翼圧力面側7a、翼
負圧面側7bに沿って流れ、翼後縁部7dから流れさり
所定の方向へ吹出される。その際、翼後縁部7dに貫通
する多数の短管10を設け静圧のみをうけるようにした
共鳴型消音器の構造をとることにより、翼後縁部7dで
の後流により発生する騒音の消音を図る。
When the impeller 1 rotates as described above, air flows from the blade leading edge 7c of the impeller 1 along the blade pressure side 7a and the blade suction side 7b, and from the blade trailing edge 7d. It is blown out in a predetermined direction. At this time, the noise generated by the wake at the wing trailing edge 7d is provided by providing a structure of a resonance type silencer in which a large number of short tubes 10 penetrating the wing trailing edge 7d are provided so as to receive only static pressure. To mute the sound.

【0025】本発明の第4の実施例を図2、図5を用い
て説明する。なお、第1実施例と同一部材については同
一の番号を付してある。図5(a) は送風機羽根車の斜視
図、図5(b) 前記羽根車の翼断面図である。
A fourth embodiment of the present invention will be described with reference to FIGS. The same members as those in the first embodiment are denoted by the same reference numerals. FIG. 5A is a perspective view of a blower impeller, and FIG. 5B is a cross-sectional view of the blade of the impeller.

【0026】図5(a)(b)に示される如く、送風機羽根車
1は円錐台状のハブ部6の外周部に翼7を取り付け、こ
の翼7は翼圧力面側7aおよび翼負圧面側7bに静圧の
みうけるように複数の短管10を流れ方向に傾斜させて
形成し、翼内部の中空層8と連通させて開口部11を設
け共鳴型消音器の構造をとる。
As shown in FIGS. 5 (a) and 5 (b), the blower impeller 1 has blades 7 mounted on the outer peripheral portion of a truncated conical hub portion 6, and the blades 7 have a blade pressure surface side 7a and a blade suction surface. A plurality of short pipes 10 are formed to be inclined in the flow direction so that only the static pressure is applied to the side 7b, and an opening 11 is provided in communication with the hollow layer 8 inside the blade to form a resonance type silencer.

【0027】この第4の実施例も羽根車1が電動機3に
対し回転自在に取り付けられ、エアガイダ4に対し所定
の位置にくるように設置されて、電動機3は電動機支持
台5に取付け固定されている。前記電動機3により所定
の回転方向に前記羽根車1が駆動されると空気は図2の
Aから吸込まれBの方向に吹出されて送風機として作動
する。そして、羽根車1が回転すると空気は羽根車1の
翼前縁部7cから、前記翼7の翼圧力面側7a、翼負圧
面側7bに沿って流れ、翼後縁部7dから流れさり所定
の方向へ吹き出される。
In the fourth embodiment, too, the impeller 1 is rotatably mounted on the electric motor 3 and is installed so as to be at a predetermined position with respect to the air guider 4, and the electric motor 3 is mounted and fixed on the electric motor support base 5. ing. When the impeller 1 is driven in a predetermined rotation direction by the electric motor 3, air is sucked in from A in FIG. 2 and is blown out in the direction of B to operate as a blower. When the impeller 1 rotates, air flows from the blade leading edge 7c of the impeller 1 along the blade pressure surface side 7a and the blade suction surface 7b of the blade 7, and flows from the blade trailing edge 7d to a predetermined position. It is blown out in the direction of.

【0028】翼7の全面または一部の翼圧力面側7aま
たは翼負圧面側7bに貫通する多数の短管10を設け、
静圧のみうけるように短管10を流れ方向に傾斜させた
共鳴型消音器の構造をとることにより、空気が羽根車1
の翼前縁部7cから、翼後縁部7dへ流れさる際に、翼
7の翼圧力面側7aまたは翼負圧面側7bにおいて発生
する騒音の消音を図ることができる。
A number of short tubes 10 are provided to penetrate the entire surface or a part of the blade pressure surface side 7a or the blade suction surface side 7b of the blade 7,
By taking the structure of a resonance type silencer in which the short pipe 10 is inclined in the flow direction so as to receive only the static pressure, the air is impeller 1
The noise generated on the blade pressure surface side 7a or the blade suction surface side 7b of the blade 7 when flowing from the blade front edge portion 7c to the blade rear edge portion 7d can be reduced.

【0029】なお、上記実施例は、翼圧力面側7aおよ
び翼負圧面側7bに複数の短管10を流れ方向に傾斜さ
せて形成しされているが、短管10は、翼圧力面側7a
または翼負圧面側7bのいずれか一部に形成してもよ
い。
In the above embodiment, a plurality of short tubes 10 are formed on the blade pressure surface side 7a and the blade suction surface side 7b so as to be inclined in the flow direction. 7a
Alternatively, it may be formed on any part of the blade suction side 7b.

【0030】[0030]

【発明の効果】送風機羽根車の翼の内部に中空層を設
け、翼の前面、または少なくとも圧力面側または翼負圧
面側の一部に中空層と外部が連通する多数の小孔、また
は連続気孔と持つポーラスな圧力変動緩衝部材を用いて
いるために、空気が羽根車の翼前縁部から、翼後縁部か
ら流れさる際に、翼圧力面側または翼負圧面側において
発生する騒音をポーラスな部材が吸音し、さらに翼内部
の中空層が共鳴型消音器の構造をとり消音することがで
きる。
According to the present invention, a hollow layer is provided inside a blade of a blower impeller, and a large number of small holes or continuous holes communicating the hollow layer with the outside at the front surface of the blade or at least a part of the pressure surface side or the blade suction surface side. Noise generated on the blade pressure surface side or blade suction surface side when air flows from the blade leading edge and the blade trailing edge of the impeller due to the use of the pores and the porous pressure fluctuation buffer member The porous member absorbs sound, and the hollow layer inside the wing has a resonance type silencer structure to muffle the sound.

【0031】また、翼圧力面側と翼負圧面側の両面にポ
ーラスな圧力変動緩衝部材を用いると、翼面上における
前記翼圧力面と翼負圧面間で空気の流入、流出があるた
め、片方の翼面上の圧力変動が高くなった場合は、他方
の圧力が低い翼面上へ空気が流出し、結果的には抑制さ
れて翼面上から発生する騒音は低減される。さらに、翼
の圧力面から翼負圧面側に空気が一部流出するために、
翼負圧面からの流れのはくりを抑制する効果もあり、は
くりにともなう圧力波の発生を軽減することができる。
When porous pressure fluctuation buffer members are used on both the blade pressure surface side and the blade suction surface side, air flows in and out between the blade pressure surface and the blade suction surface on the blade surface. When the pressure fluctuation on one of the wing surfaces becomes high, air flows out onto the wing surface with the other low pressure, and as a result, the air is suppressed and the noise generated on the wing surface is reduced. Furthermore, because some air flows out from the blade pressure surface to the blade suction surface side,
There is also an effect of suppressing the separation of the flow from the blade negative pressure surface, and the generation of a pressure wave due to the separation can be reduced.

【0032】また、送風羽根車の翼の内部に中空層を設
け、翼の少なくとも前縁側または後縁側の一部に、中空
層と外部が連通する多数の小孔または連続気孔を持つポ
ーラスな部材を用いているために、空気が羽根車の翼前
縁部から、翼後縁部へ流れさる際に、翼前縁部での衝突
により発生する騒音および翼後流部での後流により発生
する騒音を吸音し、さらに翼内部の中空層が共鳴型消音
器の構造をとり消音することができる。
Further, a hollow layer is provided inside the blade of the blower impeller, and a porous member having a number of small holes or continuous pores at least at a part of a leading edge side or a trailing edge side of the blade which allows the hollow layer to communicate with the outside. As the air flows from the leading edge of the impeller to the trailing edge of the impeller, the noise generated by the collision at the leading edge of the blade and the wake at the trailing edge of the blade And the hollow layer inside the wing can be silenced by the structure of a resonance type silencer.

【0033】また、羽根車の翼の内部に中空層を設け、
翼の後縁部側に中空層と外部が連通する多数の短管を備
え静圧のみをうけるようにした共鳴型消音器の構造をと
ることにより、翼の後縁部での後流により発生する騒音
を消音することができる。
Also, a hollow layer is provided inside the impeller wing,
Generated by the wake at the trailing edge of the wing by using a resonance type silencer structure that has a large number of short tubes on the trailing edge side of the wing and that communicates with the outside, and that receives only static pressure Noise can be reduced.

【0034】また、羽根車の翼の内部に中空層を設け、
翼の全面または少なくとも圧力面側または翼負圧面側の
一部に中空層と外部が連通し、静圧のみうけるように流
体の流れ方向に傾斜させた短管を設けた共鳴型消音器の
構造をとることにより、空気が羽根車の翼前縁部から、
翼後縁部へ流れさる際に翼の圧力面側または翼負圧面側
において発生する騒音を消音することができる。
Also, a hollow layer is provided inside the blade of the impeller,
A structure of a resonance type silencer in which a hollow layer and the outside communicate with the entire surface of the blade or at least a part on the pressure surface side or the blade suction surface side, and a short pipe is provided which is inclined in a fluid flow direction so as to receive only static pressure. By taking the air from the leading edge of the impeller,
Noise generated on the pressure surface side or the suction side of the blade when flowing to the blade trailing edge can be reduced.

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

【図1】(a) は本発明の第1の実施例の送風機羽根車の
斜視図、(b) は前記羽根車の翼断面図である。
FIG. 1A is a perspective view of a blower impeller according to a first embodiment of the present invention, and FIG. 1B is a cross-sectional view of the blade of the impeller.

【図2】羽根車を使用した送風機の断面図である。FIG. 2 is a sectional view of a blower using an impeller.

【図3】(a) は本発明の第2の実施例の送風機羽根車の
斜視図、(b) は前記羽根車の翼断面図である。
FIG. 3 (a) is a perspective view of a blower impeller according to a second embodiment of the present invention, and FIG. 3 (b) is a sectional view of the blade of the impeller.

【図4】(a) は本発明の第3の実施例の送風機羽根車の
斜視図、(b) は前記羽根車の翼断面図である。
FIG. 4A is a perspective view of a blower impeller according to a third embodiment of the present invention, and FIG. 4B is a cross-sectional view of the blade of the impeller.

【図5】(a) は本発明の第4の実施例の送風機羽根車の
斜視図、(b) は前記羽根車の翼断面図である。
FIG. 5A is a perspective view of a blower impeller according to a fourth embodiment of the present invention, and FIG. 5B is a cross-sectional view of the blade of the impeller.

【図6】(a) は従来型送風機羽根車の斜視図、(b) は前
記翼断面図である。
FIG. 6A is a perspective view of a conventional fan impeller, and FIG. 6B is a sectional view of the blade.

【図7】従来型送風機羽根車翼面上における圧力および
騒音発生原理模式図である。
FIG. 7 is a schematic view of the principle of pressure and noise generation on the blade surface of a conventional blower impeller.

【符号の説明】[Explanation of symbols]

1 送風機羽根車 2 羽根車ボス部 3 電動機 4 エアガイダ 5 電動機支持台 6 ハブ部 7 翼 7a 翼圧力面側 7b 翼負圧面側 7c 翼前縁部 7d 翼後縁部 8 中空層 9 圧力変動緩衝部材 10 短管 11 開口部 REFERENCE SIGNS LIST 1 blower impeller 2 impeller boss 3 motor 4 air guider 5 motor support 6 hub 7 blade 7 a blade pressure surface side 7 b blade suction surface 7 c blade front edge 7 d blade rear edge 8 hollow layer 9 pressure fluctuation buffer member 10 Short pipe 11 Opening

───────────────────────────────────────────────────── フロントページの続き (56)参考文献 特開 平4−12199(JP,A) 特開 昭58−45029(JP,A) 特開 平1−203698(JP,A) 実開 昭50−125109(JP,U) 実開 昭64−53843(JP,U) 実開 平2−34797(JP,U) (58)調査した分野(Int.Cl.7,DB名) F24F 1/00 316 F03D 1/06 F04D 29/38 ──────────────────────────────────────────────────続 き Continuation of the front page (56) References JP-A-4-12199 (JP, A) JP-A-58-45029 (JP, A) JP-A-1-203698 (JP, A) Japanese Utility Model Showa 50- 125109 (JP, U) Japanese Utility Model Showa 64-53843 (JP, U) Japanese Utility Model Utility Model No. 2-34797 (JP, U) (58) Fields investigated (Int. Cl. 7 , DB name) F24F 1/00 316 F03D 1/06 F04D 29/38

Claims (4)

(57)【特許請求の範囲】(57) [Claims] 【請求項1】 送風機羽根車を構成する複数枚の翼の内
部に中空層を設け、翼の全面、または、少なくとも翼圧
力面側または翼負圧面側の一部に、中空層と外部が連通
する多数の小孔または連続気孔を持つポーラスな圧力変
動緩衝部材を使用した送風機羽根車。
1. A hollow layer is provided inside a plurality of blades constituting a fan impeller, and the hollow layer and the outside communicate with the entire surface of the blade or at least a part of the blade pressure surface side or the blade suction surface side. A blower impeller using a porous pressure fluctuation buffer member having a large number of small holes or continuous pores.
【請求項2】 翼の少なくとも前縁部側または後縁部側
の一部に、中空層と外部が連通する多数の小孔または連
続気孔を持つポーラスな圧力変動緩衝部材を使用した請
求項1記載の送風機羽根車。
2. A porous pressure fluctuation cushioning member having a number of small holes or continuous pores communicating between the hollow layer and the outside is used at least on a part of the blade at the leading edge side or the trailing edge side. Blower impeller as described.
【請求項3】 送風機羽根車を構成する複数枚の翼の内
部に中空層を設け、翼の後縁部側に中空層と外部が連通
する短管を設け静圧のみをうける共鳴型消音器を備えた
送風機羽根車。
3. A resonance type silencer which receives only a static pressure by providing a hollow layer inside a plurality of blades constituting a fan impeller, and providing a short pipe communicating between the hollow layer and the outside at a trailing edge side of the blade. Blower impeller equipped with.
【請求項4】 送風機羽根車を構成する複数枚の翼の内
部に中空層を設け、翼の全面、または、少なくとも翼圧
力面側または翼負圧面側の一部に、中空層と外部が連通
し、静圧のみをうけるように流体の流れ方向に傾斜させ
た短管を設けた共鳴型消音器を備えた送風機羽根車。
4. A hollow layer is provided inside a plurality of blades constituting a fan impeller, and the hollow layer and the outside communicate with the entire surface of the blade or at least a part of the blade pressure surface side or the blade suction surface side. A blower impeller provided with a resonance type silencer provided with a short pipe inclined in a fluid flow direction so as to receive only static pressure.
JP4008804A 1992-01-22 1992-01-22 Blower impeller Expired - Fee Related JP3071287B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP4008804A JP3071287B2 (en) 1992-01-22 1992-01-22 Blower impeller

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP4008804A JP3071287B2 (en) 1992-01-22 1992-01-22 Blower impeller

Publications (2)

Publication Number Publication Date
JPH05196243A JPH05196243A (en) 1993-08-06
JP3071287B2 true JP3071287B2 (en) 2000-07-31

Family

ID=11703036

Family Applications (1)

Application Number Title Priority Date Filing Date
JP4008804A Expired - Fee Related JP3071287B2 (en) 1992-01-22 1992-01-22 Blower impeller

Country Status (1)

Country Link
JP (1) JP3071287B2 (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100549891B1 (en) * 1994-02-03 2006-04-06 포베르크 운트 컴파니 인터홀딩 게엠베하 Radial impeller
CA2353904C (en) 1998-12-09 2008-01-08 Aloys Wobben Reduction in the noise produced by a rotor blade of a wind turbine
DK174319B1 (en) * 2000-06-20 2002-12-02 Lm Glasfiber As Wind turbine blade with noise canceling means
JP5107865B2 (en) * 2008-10-24 2012-12-26 三菱重工メカトロシステムズ株式会社 Fluctuating wind generator and wind tunnel device
CN102312798B (en) * 2011-07-22 2014-06-11 上海庆华蜂巢建材有限公司 Full honeycomb board wind power generator wind wheel blade
JP2021134751A (en) * 2020-02-28 2021-09-13 公立大学法人 富山県立大学 Fan unit and blower using the same

Also Published As

Publication number Publication date
JPH05196243A (en) 1993-08-06

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