JPS6137840Y2 - - Google Patents

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Publication number
JPS6137840Y2
JPS6137840Y2 JP1980050317U JP5031780U JPS6137840Y2 JP S6137840 Y2 JPS6137840 Y2 JP S6137840Y2 JP 1980050317 U JP1980050317 U JP 1980050317U JP 5031780 U JP5031780 U JP 5031780U JP S6137840 Y2 JPS6137840 Y2 JP S6137840Y2
Authority
JP
Japan
Prior art keywords
pulsation
air
impeller
centrifugal blower
damping member
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
Application number
JP1980050317U
Other languages
Japanese (ja)
Other versions
JPS56150899U (en
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 filed Critical
Priority to JP1980050317U priority Critical patent/JPS6137840Y2/ja
Publication of JPS56150899U publication Critical patent/JPS56150899U/ja
Application granted granted Critical
Publication of JPS6137840Y2 publication Critical patent/JPS6137840Y2/ja
Expired legal-status Critical Current

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Description

【考案の詳細な説明】 本考案は遠心ブロワに関し、とりわけ、騒音の
原因となる吸込気体の脈動を減衰するようにした
遠心ブロワに関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a centrifugal blower, and more particularly to a centrifugal blower that damps the pulsation of suction gas that causes noise.

一般に、自動車の空気調和装置等には遠心ブロ
ワを備えており、この遠心ブロワで送風するよう
にしてある。ところで、この遠心ブロワ1は第1
図及び第2図に示すように、ケーシング2内に嵌
装した翼車3を有し、この翼車3を前記ケーシン
グ2に固定したモータ4のシヤフト4aに装着し
て回転するようにしてある。前記翼車3はその周
縁部に多数の翼3aを配設する一方、該翼車3の
一端中央部には前記翼3aの内端近傍まで開口し
た空気吸入口3bを形成してあると共に、前記翼
3aの他端は該翼車3内に突出する円錐台形状の
デイスク3cで密閉し、このデイスク3cの中央
を前記モータ4のシヤフト4aに固定するように
してある。また、前述した翼車3,ケーシング2
間の間隙Sは空気流出方向に徐々に大きくなつ
て、流出空気を集めてブロワ出口1a方向に導く
ようにしてある。
Generally, an air conditioner for an automobile is equipped with a centrifugal blower, and the centrifugal blower is used to blow air. By the way, this centrifugal blower 1 is
As shown in the figures and FIG. 2, a casing 2 has a blade wheel 3 fitted therein, and the blade wheel 3 is mounted on a shaft 4a of a motor 4 fixed to the casing 2 so as to rotate. . The blade wheel 3 has a large number of blades 3a arranged around its periphery, and an air intake port 3b that opens near the inner end of the blade 3a is formed at the center of one end of the blade wheel 3. The other end of the blade 3a is hermetically sealed with a truncated conical disk 3c protruding into the impeller 3, and the center of the disk 3c is fixed to the shaft 4a of the motor 4. In addition, the aforementioned impeller 3 and casing 2
The gap S between them gradually becomes larger in the air outflow direction, and is designed to collect the outflowing air and guide it toward the blower outlet 1a.

しかしながら、かかる従来の遠心ブロワ1にあ
つては、遠心ブロワ1の翼車3とケーシング2と
の間の間隙S内の圧力は、翼車3で吐出された空
気がブロワ出口1aに近づくに従つて、徐々に昇
圧され出口1aでは40〜50mm(水柱)に達するた
め、出口側では吹き返しが生ずる。この吹き返し
は一定状態ではなく変動をくり返すので、この変
動によりブロワ内の気流に渦流を生じ不安定な脈
動が発生する。そして、この脈動によりブロワに
脈動音を生じ、騒音の原因になつてしまうという
問題があつた。
However, in such a conventional centrifugal blower 1, the pressure within the gap S between the impeller 3 and the casing 2 of the centrifugal blower 1 increases as the air discharged from the impeller 3 approaches the blower outlet 1a. Then, the pressure gradually increases and reaches 40 to 50 mm (water column) at the outlet 1a, so that blowback occurs on the outlet side. Since this blowback is not constant but repeatedly fluctuates, this fluctuation causes a vortex in the airflow inside the blower, causing unstable pulsation. This pulsation causes a pulsating sound in the blower, causing a problem.

本考案はかかる従来の問題点に鑑みて、翼車の
空気吸入口3b内方に吸込気体の脈動を減衰する
脈動減衰部材を配設し、ブロワの脈動音を減少さ
せるようにしたものである。
In view of these conventional problems, the present invention is designed to reduce the pulsation noise of the blower by disposing a pulsation damping member for damping the pulsation of the intake gas inside the air intake port 3b of the impeller. .

以下、本考案の実施例を図と共に従来の構成と
同一部分に同一符号を付して詳述する。
Hereinafter, embodiments of the present invention will be described in detail with reference to the drawings, in which the same parts as those in the conventional structure are denoted by the same reference numerals.

第3図において、3はケーシング2内に配設さ
れた翼車で、この翼車3は従来と同様に周縁部に
翼3aを配設すると共に、一端に空気吸入口3b
を形成し、他端をデイスク3cで密閉してある。
ここで、本考案は前記翼3aの内端径より若干小
径の円板形をし、かつ、薄い可撓性部材よりなる
脈動減衰部材10を設け、この脈動減衰部材10
を空気吸入口3b内方に配置すると共に、この脈
動減衰部材10の中心部を、前記デイスク3cを
装着するモータ4のシヤフト4aにスペーサ11
を介して挿通してあり、これら脈動減衰部材1
0,スペーサ11をシヤフト4a端部に螺着した
ナツトNでデイスク3cに固定し、翼車3と一体
的に回転するようにしてある。
In FIG. 3, reference numeral 3 denotes a blade wheel disposed within the casing 2, and this impeller 3 has blades 3a disposed on its peripheral edge as in the conventional case, and has an air intake port 3b at one end.
The other end is sealed with a disk 3c.
Here, the present invention provides a pulsation damping member 10 which has a disc shape with a diameter slightly smaller than the inner end diameter of the blade 3a and is made of a thin flexible member.
is placed inside the air intake port 3b, and the center portion of this pulsation damping member 10 is attached to the shaft 4a of the motor 4 on which the disk 3c is attached with a spacer 11.
These pulsation damping members 1
0. The spacer 11 is fixed to the disk 3c with a nut N screwed onto the end of the shaft 4a, so that it rotates integrally with the impeller 3.

尚、この実施例では前記脈動減衰部材10を僅
かに笠状に形成し、その頂点部を空気吸入口3b
方向に配置してある。
In this embodiment, the pulsation damping member 10 is formed into a slightly shaded shape, and the apex thereof is connected to the air intake port 3b.
It is placed in the direction.

以上の構成により、遠心ブロワ1の作動に伴つ
て、空気吸入口3bから翼車3内に空気が吸入さ
れ、該空気吸入口3b内方には前述したように吸
入空気に渦流を生じ、この渦流空気が脈動減衰部
材10に衝突する。このとき、この衝突空気の速
度は渦流による脈動によつて異なり、空気速度が
大きい部分は脈動減衰部材10が大きく撓み、逆
に空気速度が小さい部分は脈動減衰部材10の撓
みも小さくなる。つまり、脈動減衰部材10は薄
い可撓性材により構成されているので、回転に基
く遠心力による剛性は小さいため、衝突空気の速
度に応じて部分的に撓んで該空気流の脈動エネル
ギを吸収し、該吸入空気の脈動を減衰する。
With the above configuration, as the centrifugal blower 1 operates, air is sucked into the impeller 3 from the air suction port 3b, and a vortex is generated in the intake air inside the air suction port 3b as described above. The swirling air impinges on the pulsation damping member 10 . At this time, the speed of the colliding air varies depending on the pulsation caused by the vortex flow, and the pulsation damping member 10 is deflected largely in areas where the air velocity is high, and conversely, the pulsation damping member 10 is deflected to a small extent in areas where the air velocity is low. In other words, since the pulsation damping member 10 is made of a thin flexible material, its rigidity due to centrifugal force due to rotation is small, so it partially bends depending on the speed of the colliding air and absorbs the pulsation energy of the air flow. and attenuates the pulsation of the intake air.

本考案に基いて実際に製作した遠心ブロワの資
料を示すと、翼車の直径は140mm〜150mm、脈動減
衰部材は直径80mm、厚さ0.5〜1mm、材質は布入
りの塩化ビニールシートであつて、脈動音の減衰
は1〜1.5dBに達している。
Documents of a centrifugal blower actually manufactured based on the present invention show that the diameter of the impeller is 140 mm to 150 mm, the pulsation damping member is 80 mm in diameter, 0.5 to 1 mm thick, and made of cloth-filled vinyl chloride sheet. , the attenuation of pulsating sound reaches 1 to 1.5 dB.

以上説明したように、本考案の遠心ブロワにあ
つて、翼車の気体吸込口内に、翼車と一体的に回
転するように、円板状の薄い可撓性材よりなり吸
込気体の脈動を減衰する脈動減衰部材を、吸気流
方向に対して略直角に配設し、脈動減衰部材は衝
突気体の速度に応じて部分的に撓んで吸込気体の
脈動エネルギを吸収し、該吸込気体の脈動を減衰
するようにしたので、ブロワ後流の送風吐出側に
生ずる脈動音を著しく減少することができるとい
う実用上優れた効果を奏する。
As explained above, in the centrifugal blower of the present invention, a disk-shaped thin flexible material is installed in the gas suction port of the impeller so that it rotates integrally with the impeller. A pulsation damping member that attenuates is disposed substantially perpendicular to the intake flow direction, and the pulsation damping member partially bends according to the velocity of the colliding gas to absorb the pulsation energy of the intake gas, thereby reducing the pulsation of the intake gas. Since the noise is attenuated, the pulsating noise generated on the air discharge side downstream of the blower can be significantly reduced, which is an excellent practical effect.

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

第1図は従来の遠心ブロワの概略構成図、第2
図は従来の遠心ブロワの断面図、第3図は本考案
の遠心ブロワの断面図である。 1……遠心ブロワ、3……翼車、3b……気体
吸込口、10……脈動減衰部材。
Figure 1 is a schematic configuration diagram of a conventional centrifugal blower, Figure 2
The figure is a sectional view of a conventional centrifugal blower, and FIG. 3 is a sectional view of a centrifugal blower according to the present invention. 1... Centrifugal blower, 3... Impeller, 3b... Gas suction port, 10... Pulsation damping member.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 翼車の気体吸込口内に、前記翼車と一体的に回
転するように、円板状の薄い可撓性材よりなり吸
込気体の脈動を減衰する脈動減衰部材を、吸気流
方向に対して略直角に配設したことを特徴とする
遠心ブロワ。
A pulsation damping member made of a disk-shaped thin flexible material and damping the pulsation of the intake gas is installed in the gas suction port of the impeller so as to rotate integrally with the impeller, approximately in the direction of the intake air flow. A centrifugal blower characterized by being arranged at right angles.
JP1980050317U 1980-04-14 1980-04-14 Expired JPS6137840Y2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1980050317U JPS6137840Y2 (en) 1980-04-14 1980-04-14

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1980050317U JPS6137840Y2 (en) 1980-04-14 1980-04-14

Publications (2)

Publication Number Publication Date
JPS56150899U JPS56150899U (en) 1981-11-12
JPS6137840Y2 true JPS6137840Y2 (en) 1986-11-01

Family

ID=29645261

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1980050317U Expired JPS6137840Y2 (en) 1980-04-14 1980-04-14

Country Status (1)

Country Link
JP (1) JPS6137840Y2 (en)

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS448675Y1 (en) * 1965-10-29 1969-04-08

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS448675Y1 (en) * 1965-10-29 1969-04-08

Also Published As

Publication number Publication date
JPS56150899U (en) 1981-11-12

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