JPS61182500A - Centrifugal multiblade blower - Google Patents

Centrifugal multiblade blower

Info

Publication number
JPS61182500A
JPS61182500A JP2382385A JP2382385A JPS61182500A JP S61182500 A JPS61182500 A JP S61182500A JP 2382385 A JP2382385 A JP 2382385A JP 2382385 A JP2382385 A JP 2382385A JP S61182500 A JPS61182500 A JP S61182500A
Authority
JP
Japan
Prior art keywords
sound
blower
casing
opening
air
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.)
Pending
Application number
JP2382385A
Other languages
Japanese (ja)
Inventor
Yasuhiko Ebata
江端 泰彦
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 Holdings Corp
Original Assignee
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 Matsushita Electric Industrial Co Ltd filed Critical Matsushita Electric Industrial Co Ltd
Priority to JP2382385A priority Critical patent/JPS61182500A/en
Publication of JPS61182500A publication Critical patent/JPS61182500A/en
Pending legal-status Critical Current

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Abstract

PURPOSE:To reduce the absolute value of a noise with an nz-sound being as the center, by connecting a cavity part of predetermined volume, provided in a nose part of a casing, with an opening part of small size, provided in an external surface of the nose part brought into contact with a flow of air, through a pipe line having an opening section area. CONSTITUTION:A nose part 14 generates a turbulence being hit by air immediately after coming out from a multiblade impeller 11, and a blower, providing an opening part 15 of sectional area S in the depth directional center of an external surface of the nose part 14 opposed to the multiblade impeller 11 while a cavity part 16 of volume V in a position L from the opening part 15, connects the opening part 15 with the cavity part 16 through a pipe line 17 of sectional area S. In this way, the blower, reducing a sound level of frequency with an nz-sound being as the center while also a reverberating sound due to a space surrounded by the impeller 11 and a casing 13, enables also the absolute value of a noise to be reduced. Further the blower, in which a substantially limited position and shape of the multiblade impeller 11, air guider 12 and the casing 13 can be more freely designed because the nz-sound is decreased than usual, can obtain large contribution to the improvement of performance of efficiency or the like of the blower.

Description

【発明の詳細な説明】 産業上の利用分野 本発明は、空気調和機の送風機などとして広く用いられ
ている遠心多翼型送風装置に関するものである。
DETAILED DESCRIPTION OF THE INVENTION Field of the Invention The present invention relates to a centrifugal multi-blade blower that is widely used as a blower for air conditioners.

従来の技術 近年、多汎羽根車を用いた送風装置は空気調和機用送風
装置として広く用いられているが、高効率化が進むにつ
れて、騒音の周波数が回転数nとブレード枚数2の積n
−zとして表わされ、一般にnz音と呼ばれている特異
者か高く発生する条件での送風装態設計が要求され、例
えば実開昭59−41696号公報で知られるように送
風装置効率を低下させずにnz音を押える試みがいろい
ろとなされている。又特願昭58−125049号のよ
うに羽根車のブレード間のピッチ角を周期性を持たずに
乱数的に配列した多翼羽根車などが作られている。
BACKGROUND OF THE INVENTION In recent years, blowers using multi-purpose impellers have been widely used as blowers for air conditioners, but as efficiency increases, the frequency of noise increases by the product n of the number of rotations n and the number of blades 2.
-z, which is generally called nz sound, is required to design a blower system under conditions where a high level of noise occurs. Various attempts have been made to suppress the nz sound without reducing it. Furthermore, as disclosed in Japanese Patent Application No. 125049/1982, a multi-blade impeller is manufactured in which the pitch angle between the blades of the impeller is arranged randomly without periodicity.

以下図面を参照しながら、上述した従来の多翼羽根車を
用いた遠心多翼型送風装置の一例について説明する。
An example of a centrifugal multi-blade blower using the above-mentioned conventional multi-blade impeller will be described below with reference to the drawings.

第6図、第7図、第8図は従来の遠心多翼型送風装置の
構成、ブレード間のピンチ角を周期性を持たずに乱数的
に配列した多翼羽根車の断面、および、騒音の周波数特
性を示すものである。
Figures 6, 7, and 8 show the configuration of a conventional centrifugal multi-blade blower, the cross-section of a multi-blade impeller in which the pinch angle between the blades is randomly arranged without any periodicity, and the noise level. This shows the frequency characteristics of

第6図において、1は多翼羽根車である。2はエアーガ
イダで、多翼羽根車1へ流入する空気の導入路を形成す
る。3はケーシングで、多翼羽根車1から流出した空気
を整流するとともに、多翼羽根車1の送風性能を向上さ
せる。4はノーズ部て、ケーシング3の端部で、多翼羽
根車1と最も接近した部分である。
In FIG. 6, 1 is a multi-blade impeller. Reference numeral 2 denotes an air guider, which forms an introduction path for air flowing into the multi-blade impeller 1. 3 is a casing that rectifies the air flowing out from the multi-blade impeller 1 and improves the blowing performance of the multi-blade impeller 1. Reference numeral 4 denotes a nose portion, which is the end of the casing 3 and is closest to the multi-blade impeller 1.

第7図において、5はブレードで、多翼羽根車1を構成
しており、これらのブレード5のピッチ角θは一律では
なく乱数的に配設しである。ここで、ピッチとは、ブレ
ード5とブレード5の円周方向の角度である。
In FIG. 7, reference numeral 5 denotes blades constituting the multi-blade impeller 1, and the pitch angle θ of these blades 5 is not uniform but randomly arranged. Here, the pitch is the angle between the blades 5 in the circumferential direction.

以上のように構成された遠心多翼型送風装置について、
以下その動作について説明する。
Regarding the centrifugal multi-blade blower configured as above,
The operation will be explained below.

エアーガイダ2、ケーシング3を備えた多翼羽根車1を
回転させると、回転数nとブレード枚数2の積n・2を
特徴とする特異者(nz音と一般に呼ばれている)が高
く発生するかわりに、第8図の周波数特性因のように、
nz音は複数種の周波数成分に分かれて波高が低くなり
、聴感的なnz音の低減化が図れるものである。
When the multi-blade impeller 1 equipped with the air guider 2 and the casing 3 is rotated, a peculiar sound (generally called nz sound), which is characterized by the product n・2 of the number of rotations n and the number of blades 2, is generated at a high rate. Instead, like the frequency characteristic factor in Figure 8,
The nz sound is divided into a plurality of types of frequency components and the wave height is lowered, so that the perceptible nz sound can be reduced.

発明が解決しようとする問題点 しかしながら上記のような構成では、単一の周波数を持
つnz音を、ブレードのピンチ角を乱数的に配設するこ
とにより、複数種の周波数に分散するため、聴感的なn
z音の低減は図れるが、非常に接近した周波数が連続的
に変化するnz音となるため、聴感的には周波数一定の
連続音とはならず、周期的に周波数が変化する連続音と
して聞こえ、大きな音ではないが、異常音として耳につ
く。特に、渦巻状のケーシングにより性能向上をはかる
遠心多翼型送風装置では、多翼羽根車とケーシングで囲
まれた空間により反響し聴感的に非常に悪いものとなる
Problems to be Solved by the Invention However, with the above configuration, the nz sound with a single frequency is dispersed into multiple frequencies by randomly arranging the pinch angle of the blade, which makes it difficult to hear. n
Although it is possible to reduce the z sound, it becomes a nz sound in which frequencies that are very close to each other change continuously, so it does not sound like a continuous sound with a constant frequency, but as a continuous sound with a periodically changing frequency. Although it is not a loud sound, it is noticeable as an abnormal sound. In particular, in a centrifugal multi-blade blower that uses a spiral casing to improve its performance, the space surrounded by the multi-blade impeller and the casing causes reverberations that result in extremely poor acoustics.

本発明は上記問題点に鑑み、nz音を低減するとともに
nz音以外の騒音をも同時に低減し、かつ、周波数が変
化する騒音等を新たに作らないことを目的とするもので
ある。
In view of the above-mentioned problems, it is an object of the present invention to reduce the NZ sound and to simultaneously reduce noises other than the NZ sound, and to avoid creating new noise with changing frequencies.

問題点を解決するための手段 上記問題点を解決するために本発明の遠心多翼型送風装
置は、ケーシングのノーズ部内に所定の容積の空洞部を
設けるとともに、空気の流れに接するノーズ部の外表面
に小径の開口部を設け、空洞部と開口部を開口断面積を
有する管路でつなぐという構成を備えたものである。
Means for Solving the Problems In order to solve the above-mentioned problems, the centrifugal multi-blade blower of the present invention has a cavity with a predetermined volume in the nose of the casing, and a cavity in the nose that is in contact with the air flow. It has a configuration in which a small diameter opening is provided on the outer surface, and the cavity and the opening are connected by a conduit having an opening cross-sectional area.

作   用 本発明は上記した構成によって、ノーズ部に設けた空洞
部の音響インピーダンスが最も低くなる周波数をnz音
の周波数に一致させることにより、nz音を中心とする
駐1音を低減させ、nz音は他の雑音と混ざって殆んど
聞こえない状態となる。
Effect of the present invention With the above-described configuration, by matching the frequency at which the acoustic impedance of the cavity provided in the nose portion is the lowest to the frequency of the nz sound, the nz sound is reduced, and the nz sound is reduced. The sound is mixed with other noise and becomes almost inaudible.

実施例 以下本発明の一実施例の遠心多翼型送風装置について、
図面を参照しながら説明する。
Example Below, regarding a centrifugal multi-blade blower according to an example of the present invention,
This will be explained with reference to the drawings.

第1図、第2図は本発明の遠心多翼型送風装置の一実施
例を示すものである。
FIGS. 1 and 2 show an embodiment of a centrifugal multi-blade blower according to the present invention.

第1図、第2図において、11は多翼羽根車である。1
2はエアーガイグであり、13は渦巻形状をした合成樹
脂製のケーシングである。14はノーズ部で、ケーシン
グ13の一部であり、渦巻形状の巻きはじめと巻き終り
が重なる部分である。
In FIGS. 1 and 2, 11 is a multi-blade impeller. 1
2 is an air guide, and 13 is a spiral-shaped synthetic resin casing. Reference numeral 14 denotes a nose portion, which is a part of the casing 13, and is a portion where the beginning and end of the spiral shape overlap.

渦巻形状のケーシング13内を流れる空気が多翼羽根車
11を出たばかりの空気とぶつかり乱れをおこすノーズ
部14の多翼羽根車11と対向する外表面の奥行方向中
央には、断面積Sの開口部15を設け、開口部15から
距離りの位置に体積Vの空洞部16を設けて、開口部1
5と空洞部16とは断面積Sの管路17でつながってい
る。
At the center in the depth direction of the outer surface facing the multi-blade impeller 11 of the nose portion 14, where the air flowing inside the spiral-shaped casing 13 collides with the air that has just exited the multi-blade impeller 11 and causes turbulence, there is a groove with a cross-sectional area S. An opening 15 is provided, a cavity 16 having a volume V is provided at a distance from the opening 15, and the opening 1
5 and the cavity 16 are connected by a conduit 17 having a cross-sectional area S.

上記の構造をもつノーズ部14の音響インピーダンス土
は、空気の密度p、音速Cとすると、と表わされる。た
だし、H=lZT  である。この式をグラフ化すると
第3図のようになる。また、この周波数f。をnz音の
周波数n’zに一致させることにより、nz音を中心と
する騒音を低減させることができる。
The acoustic impedance of the nose portion 14 having the above structure is expressed as follows, where p is the density of air and C is the speed of sound. However, H=lZT. If this equation is graphed, it will look like Figure 3. Moreover, this frequency f. By matching the frequency n'z of the nz sound, noise centered on the nz sound can be reduced.

第4図には、ノーズ部14に開口部15、空洞部16、
管路17を設けない場合の騒音の周波数特性を示してい
る。このような構造では、nz音対策がなされていない
ため、nz音が高いピークとなっている。
FIG. 4 shows an opening 15 in the nose portion 14, a cavity 16,
It shows the frequency characteristics of noise when the pipe line 17 is not provided. In such a structure, no measures are taken against the nz sound, so the nz sound has a high peak.

これに対して、第5図に示す本実施例における騒音の周
波数特性では、ピークはあるものの他の周波数に比べ高
くないために、聴感的には、前者が笛を吹くような高い
音がするのに対して、後者は他の雑音と混ざって殆んど
聞こえない状態となる。
On the other hand, in the frequency characteristics of the noise in this example shown in FIG. 5, although there is a peak, it is not higher than other frequencies, so the former sounds audibly like a high-pitched whistle. On the other hand, the latter is mixed with other noise and becomes almost inaudible.

また本発明による遠心多翼型送風装置は、rIz音を中
心とした周波数の音のレベルを低減させ、羽根車11と
ケーシング13で囲まれた空間による騒音の反響音をも
低減させるため、騒音の絶対値をも低減することができ
、さらに羽根車11の形状および羽根車11とエアーガ
イダ12、ケーシング13との相対位置は変更しないた
め、従来の遠心多翼型送風装置と比べ、他の周波数の音
の上昇や送風性能の低下は見られない。
In addition, the centrifugal multi-blade blower according to the present invention reduces the level of sound at frequencies centered around the rIz sound, and also reduces the echoes of the noise caused by the space surrounded by the impeller 11 and the casing 13. The absolute value of No increase in sound or decrease in air blowing performance was observed.

従って、従来より遠心多翼型送風装置の重大な欠点とさ
れていた流れが乱れるノーズ部で発生するnz音を大幅
に低減するばかりか、それによる他の騒音の増大や効率
の低下を何らともなわず、騒音全体のレベルを低下する
ことができる。しかも、従来よりnz音を低下するため
に、大幅に制限されていた、多翼羽根車11やエアーガ
イダ12、ケーシング13の位置・形状の設計をより自
由にすることができ、送風機の効率等性能の向上に大い
に寄与するものである。
Therefore, not only can the nz sound generated at the nose section where the flow is disturbed, which has traditionally been considered a major drawback of centrifugal multi-blade blowers, be significantly reduced, but it also eliminates any increase in other noise or decrease in efficiency caused by it. First, the overall noise level can be reduced. Moreover, it is now possible to design the positions and shapes of the multi-blade impeller 11, air guider 12, and casing 13 more freely, which had previously been significantly restricted in order to reduce the nz sound, thereby improving the efficiency and other performance of the blower. This greatly contributes to the improvement of

発明の効果 以上のように本発明は、ケーシングのノーズ部内に所定
の容積の空洞部を設け、また、空気の流れに接するノー
ズ部の外表面に小径の開口部を設け、これらを開口断面
積を有する管路でつないたものであり、この構成により
、遠心多翼型送風装置の重大な欠点とされていたnz音
をはじめとする騒音を低減せしめ、静寂で高効率の送風
を行なうことができる効果を有する。
Effects of the Invention As described above, the present invention provides a cavity with a predetermined volume in the nose portion of the casing, and also provides a small diameter opening on the outer surface of the nose portion that is in contact with the air flow. This configuration reduces noise, including NZ sound, which was considered a serious drawback of centrifugal multi-blade blowers, and enables quiet and highly efficient air blowing. It has the effect of

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

第1図は本発明の一実施例を示す遠心多翼型送風装置の
概略を示す斜視図、第2図は本発明の一実施例を示すノ
ーズ部の部分斜視図、第3図は本発明の一実施例を示す
ノーズ部空洞部の音響インピーダンス特性図、第4図は
本発明の一実施例における空洞部を設けない場合の騒音
の周波数特性図、第5図は本発明の一実施例において空
洞部を設けた場合の騒音の周波数特性図、第6図は従来
の遠心多翼型送風装置の棚略を示す斜視図、第7図は従
来の遠心多翼型送風装置の多翼羽根車の断面図、第8図
は従来の遠心多翼型送風装置より発生する騒音の周波数
特性図である。 11・・・・・・多翼羽根車、12・・・・・・エアー
ガイダ、13 ・ ケーシング、14・・・・ノーズ部
、15・・開口部、16 ・・・・空洞部、1了・・・
・管路。 代理人の氏名 弁理士 中 尾 敏 男 ほか1名11
  シシin良車 I2  エアーガイZ″ I5・開口部 l乙  堂 シ目岩毛 I7  脅  踏 第3図 第6図
Fig. 1 is a perspective view schematically showing a centrifugal multi-blade blower according to an embodiment of the present invention, Fig. 2 is a partial perspective view of a nose portion showing an embodiment of the present invention, and Fig. 3 is a perspective view showing an outline of a centrifugal multi-blade blower according to an embodiment of the present invention. FIG. 4 is an acoustic impedance characteristic diagram of a cavity in the nose section showing an embodiment of the present invention, FIG. 4 is a frequency characteristic diagram of noise when no cavity is provided in an embodiment of the present invention, and FIG. 5 is a diagram of an embodiment of the present invention. Figure 6 is a perspective view showing the shelf of a conventional centrifugal multi-blade blower, and Figure 7 is a diagram of the multi-blade blades of a conventional centrifugal multi-blade blower. FIG. 8, a cross-sectional view of the vehicle, is a frequency characteristic diagram of noise generated by a conventional centrifugal multi-blade blower. 11...Multi-blade impeller, 12...Air guider, 13・Casing, 14...Nose part, 15...Opening part, 16...Cavity part, 1.・・・
・Pipeline. Name of agent: Patent attorney Toshio Nakao and 1 other person11
Shishi in Good Car I2 Air Guy Z'' I5・Opening L Otsudo Shime Iwage I7 Throat Figure 3 Figure 6

Claims (1)

【特許請求の範囲】[Claims]  多翼羽根車の前後にエアーガイダとケーシングを配設
し、さらに前記ケーシングのノーズ部における空気の流
れに接する外表面に小径の開口部を設け、さらに開口断
面積を有する管路で前記開口部と連続し、かつ、所定の
容積を有する空洞部を内蔵した遠心多翼型送風装置。
An air guider and a casing are disposed before and after the multi-blade impeller, and a small diameter opening is provided on the outer surface of the casing in contact with the air flow at the nose portion of the casing, and a conduit having an opening cross-sectional area is connected to the opening. A centrifugal multi-blade blower with a built-in cavity that is continuous and has a predetermined volume.
JP2382385A 1985-02-08 1985-02-08 Centrifugal multiblade blower Pending JPS61182500A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2382385A JPS61182500A (en) 1985-02-08 1985-02-08 Centrifugal multiblade blower

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2382385A JPS61182500A (en) 1985-02-08 1985-02-08 Centrifugal multiblade blower

Publications (1)

Publication Number Publication Date
JPS61182500A true JPS61182500A (en) 1986-08-15

Family

ID=12121076

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2382385A Pending JPS61182500A (en) 1985-02-08 1985-02-08 Centrifugal multiblade blower

Country Status (1)

Country Link
JP (1) JPS61182500A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0638728A1 (en) * 1993-08-02 1995-02-15 Foster Wheeler Energy Corporation Rotary throat cutoff device and method for reducing centrifugal fan noise

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS515009B1 (en) * 1970-03-10 1976-02-17

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS515009B1 (en) * 1970-03-10 1976-02-17

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0638728A1 (en) * 1993-08-02 1995-02-15 Foster Wheeler Energy Corporation Rotary throat cutoff device and method for reducing centrifugal fan noise

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