JP2003343486A - Centrifugal compressor equipped with long-and-short impeller - Google Patents

Centrifugal compressor equipped with long-and-short impeller

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Publication number
JP2003343486A
JP2003343486A JP2002153306A JP2002153306A JP2003343486A JP 2003343486 A JP2003343486 A JP 2003343486A JP 2002153306 A JP2002153306 A JP 2002153306A JP 2002153306 A JP2002153306 A JP 2002153306A JP 2003343486 A JP2003343486 A JP 2003343486A
Authority
JP
Japan
Prior art keywords
long
blade
short
centrifugal compressor
impeller
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
JP2002153306A
Other languages
Japanese (ja)
Inventor
Hideshi Nakao
秀史 中尾
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.)
IHI Corp
Original Assignee
IHI Corp
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 IHI Corp filed Critical IHI Corp
Priority to JP2002153306A priority Critical patent/JP2003343486A/en
Publication of JP2003343486A publication Critical patent/JP2003343486A/en
Pending legal-status Critical Current

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Abstract

<P>PROBLEM TO BE SOLVED: To provide a centrifugal compressor equipped with a long-and-short impeller capable of reducing blade passing frequency noise by long vanes and maintaining high compression performance. <P>SOLUTION: The centrifugal compressor is equipped with a long-and-short impeller 3 which has long vanes 1 having long blade length extending to the delivery side from the suction side, and short vanes 2 having short blade length provided at the center part between long vanes and extending from the center part to the delivery side. A communicating passage 6 (a plow tooth-shaped groove 6A, a circumference groove 6B and clearance 6C) is provided on a shroud 4 surrounding the outer peripheral part of the long vanes 1 or the impeller of the inducer part introducing air along the rotation direction. <P>COPYRIGHT: (C)2004,JPO

Description

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

【0001】[0001]

【発明の属する技術分野】本発明は、長短羽根をもつ羽
根車を備えた遠心圧縮機に関する。
TECHNICAL FIELD The present invention relates to a centrifugal compressor provided with an impeller having long and short blades.

【0002】[0002]

【従来の技術】過給機等に用いられる遠心圧縮機の羽根
車には、図3に示す長短羽根をもつ羽根車(以下、「長
短羽根車」と呼ぶ)が広く用いられている。この長短羽
根車は、羽根車の吸込み側から吐出側まで延びる翼長さ
の長い長羽根1と、長羽根の中間に設けられその中間位
置から吐出側まで延びる翼長さの短い短羽根2とからな
る。羽根車における羽根枚数は一般に多いほど高い圧力
比を得ることができるが、長羽根1のみを増やすと、吸
込み側における羽根間隔が狭くなり、空気の吸込み(飲
み込み)が悪くなる。そのため、長短羽根車は、長羽根
のみの羽根車に比較して、吸込み側における羽根間隔を
広くできるため飲み込みがよく、かつ圧縮に寄与する遠
心部では羽根枚数が多くなることから、高い圧力比を得
ることができる、等の利点を有している。
2. Description of the Related Art As an impeller of a centrifugal compressor used for a supercharger or the like, an impeller having long and short blades shown in FIG. 3 (hereinafter referred to as "long and short impeller") is widely used. This long / short impeller has a long blade 1 having a long blade length extending from the suction side to the discharge side of the impeller, and a short blade 2 having a short blade length provided in the middle of the long blades and extending from the intermediate position to the discharge side. Consists of. Generally, the higher the number of blades in the impeller, the higher the pressure ratio can be obtained. However, if only the long blades 1 are increased, the blade spacing on the suction side becomes narrower, and the air suction (swallow) becomes worse. Therefore, the long and short impellers have a wider blade interval on the suction side than the impellers with only the long blades, and thus swallow well, and the centrifugal part that contributes to compression has a large number of blades, which results in a high pressure ratio. Can be obtained.

【0003】図4はシュラウド部の翼面静圧分布図であ
る。この図に示すように、回転中の長羽根1の翼面に
は、腹側に正圧、背側に負圧が発生し、翼の正負圧面の
圧力差は大きくなる。従って、長羽根1の回転により、
翼と共に正圧と負圧が回転し、この圧力変化により騒音
が発生する。
FIG. 4 is a distribution diagram of static pressure on the blade surface of the shroud portion. As shown in this figure, a positive pressure is generated on the ventral side and a negative pressure is generated on the back side on the blade surface of the rotating long blade 1, and the pressure difference between the positive and negative pressure surfaces of the blade becomes large. Therefore, by the rotation of the long blade 1,
Positive pressure and negative pressure rotate with the blade, and noise is generated due to this pressure change.

【0004】図5は長短羽根車を備えた遠心圧縮機にお
ける騒音周波数と音圧レベルの関係図である。この図に
示すように、長短羽根車を備えた遠心圧縮機では、長羽
根枚数×回転数の周波数と全羽根枚数×回転数の2箇所
に音圧レベルのピークが観測される。この周波数を、翼
通過周波数(BPF:Blade PassingFr
equency)と呼ぶ。またこの周波数における騒音
をBPF音と略称する。
FIG. 5 is a diagram showing the relationship between noise frequency and sound pressure level in a centrifugal compressor equipped with a long and short impeller. As shown in this figure, in the centrifugal compressor equipped with the long and short impellers, peaks of the sound pressure level are observed at two locations, that is, the number of long blades × the frequency of rotation and the number of all blades × the number of rotations. This frequency is taken as the blade passing frequency (BPF: Blade Passing Fr).
This is called "equency". Further, noise at this frequency is abbreviated as BPF sound.

【0005】[0005]

【発明が解決しようとする課題】上述したように長短羽
根車を備えた遠心圧縮機は、高性能である反面、騒音が
大きい問題点があった。またこの騒音のうち、特に長羽
根のBPF音が大きく、長羽根の正負圧面の圧力差が騒
音の主要因であった。従って、インデューサ部の圧力差
を小さくすることで長羽根のBPF音を低減することが
できるが、従来の設計では、該当部分の圧力差のみを低
減することは困難であり、流体性能への影響も大きくな
ってしまう問題点があった。
As described above, the centrifugal compressor equipped with the long and short impellers has high performance, but has a problem of large noise. Among these noises, the BPF noise of the long blades was particularly large, and the pressure difference between the positive and negative pressure surfaces of the long blades was the main cause of the noise. Therefore, it is possible to reduce the BPF sound of the long blades by reducing the pressure difference in the inducer portion, but it is difficult to reduce only the pressure difference in the relevant portion with the conventional design, and it is difficult to reduce the fluid performance. There was a problem that the impact would be large.

【0006】本発明はかかる問題点を解決するために創
案されたものである。すなわち、本発明の目的は、長羽
根によるBPF音(翼通過周波数音)を低減することが
でき、かつ高い圧縮性能を維持できる長短羽根車を備え
た遠心圧縮機を提供することにある。
The present invention was devised to solve such problems. That is, an object of the present invention is to provide a centrifugal compressor equipped with a long / short impeller that can reduce BPF noise (blade passing frequency sound) due to long blades and can maintain high compression performance.

【0007】[0007]

【課題を解決するための手段】本発明によれば、吸込み
側から吐出側まで延びる翼長さの長い長羽根(1)と、
長羽根の中間に設けられその中間位置から吐出側まで延
びる翼長さの短い短羽根(2)とを有する長短羽根車
(3)を備えた遠心圧縮機において、空気を導入するイ
ンデューサ部の長羽根(1)の外周部又は羽根車を囲む
シュラウド(4)に回転方向に沿って連通路(6)を設
けたことを特徴とする長短羽根車を備えた遠心圧縮機が
提供される。
According to the present invention, a long blade (1) having a long blade length extending from the suction side to the discharge side,
In a centrifugal compressor provided with a long and short impeller (3) having a short blade (2) having a short blade length that is provided in the middle of the long blade and extends from the intermediate position to the discharge side, in an inducer section for introducing air. A centrifugal compressor provided with a long and short impeller, characterized in that a shroud (4) surrounding the outer periphery of the long blade (1) or an impeller is provided with a communication passage (6) along the rotational direction.

【0008】上記本発明の構成によれば、空気を導入す
るインデューサ部の長羽根(1)の外周部又は羽根車を
囲むシュラウド(4)に回転方向に沿って連通路(6)
が設けられているので、この連通路(6)を介して長羽
根(1)の外周部の正圧側と負圧側を連通し、その圧力
差を低減し、インデューサ部の圧力差を小さくすること
で長羽根のBPF音を低減することができる。また、こ
の連通路(6)をインデューサ部のみに設けているの
で、圧縮に寄与する遠心部への影響は少なく、高い圧縮
性能を維持することができる。
According to the above-mentioned structure of the present invention, the communication passage (6) is provided along the rotation direction in the shroud (4) surrounding the outer peripheral portion of the long blade (1) of the inducer section for introducing air or the impeller.
Is provided, the positive pressure side and the negative pressure side of the outer peripheral portion of the long blade (1) are communicated with each other through the communication passage (6) to reduce the pressure difference and reduce the pressure difference in the inducer section. This can reduce the BPF sound of the long blades. Moreover, since the communication passage (6) is provided only in the inducer section, the centrifugal section that contributes to compression is less affected, and high compression performance can be maintained.

【0009】本発明の好ましい実施形態によれば、前記
連通路(6)は、長羽根(1)の前縁から短羽根(2)
の前縁までの間の長羽根の外周部に設けられ、軸方向に
間隔を隔てた鋤歯状の溝(6A)である。この構成によ
り、長羽根の外周部に設けられた鋤歯状の溝(6A)を
介して長羽根(1)の外周部の正圧側と負圧側を直接連
通するので、長羽根の外周部以外への影響を小さくでき
る。
According to a preferred embodiment of the present invention, the communication passages (6) are formed from the leading edge of the long blade (1) to the short blade (2).
Is a veil-shaped groove (6A) which is provided on the outer peripheral portion of the long blade up to the front edge of and is axially spaced. With this configuration, since the positive pressure side and the negative pressure side of the outer peripheral portion of the long blade (1) are directly communicated with each other via the vase-shaped groove (6A) provided on the outer peripheral portion of the long blade, other than the outer peripheral portion of the long blade. Can be less affected.

【0010】また、別の好ましい実施形態によれば、前
記連通路(6)は、シュラウド(4)の内周面に設けら
れ、軸方向に間隔を隔てた複数の円周溝(6B)であ
る。この構成により、インデューサ部の内周面に設けら
れた複数の円周溝(6B)を介して長羽根(1)の外周
部の正圧側と負圧側を連通するので、長短羽根車の構造
を従来のままにできる。
Further, according to another preferred embodiment, the communication passage (6) is provided on the inner peripheral surface of the shroud (4), and comprises a plurality of circumferential grooves (6B) axially spaced from each other. is there. With this configuration, the positive pressure side and the negative pressure side of the outer peripheral portion of the long blade (1) communicate with each other via the plurality of circumferential grooves (6B) provided on the inner peripheral surface of the inducer portion, so that the structure of the long and short impeller is provided. Can be left as is.

【0011】更に、別の好ましい実施形態によれば、前
記連通路(6)は、長羽根(1)とこれを囲むシュラウ
ドとの隙間(6C)であり、該隙間(6C)は、短羽根
(2)とこれを囲むシュラウドとの隙間(2C)より大
きく設定されている。この構成により、長短羽根車とシ
ュラウドとの隙間(6C、2C)を単に違えるだけで、
長羽根のBPF音を低減することができ、長短羽根車と
シュラウドを容易に製作できる。
Further, according to another preferred embodiment, the communication passage (6) is a gap (6C) between the long blade (1) and the shroud surrounding the long blade (1), and the gap (6C) is the short blade. It is set larger than the gap (2C) between (2) and the shroud surrounding it. With this configuration, simply changing the gap (6C, 2C) between the long and short impellers and the shroud,
The BPF sound of the long blades can be reduced, and the long and short impellers and the shroud can be easily manufactured.

【0012】[0012]

【発明の実施の形態】以下、本発明の好ましい実施形態
を図面を参照して説明する。なお、各図において、共通
する部分には同一の符号を付し、重複した説明を省略す
る。
BEST MODE FOR CARRYING OUT THE INVENTION Preferred embodiments of the present invention will be described below with reference to the drawings. In each drawing, common portions are denoted by the same reference numerals, and redundant description will be omitted.

【0013】図1は、本発明の遠心圧縮機の長短羽根車
を示す側面図である。この図において、(A)は第1実
施形態、(B)は第2実施形態、(C)は第3実施形態
を示している。各図において、本発明の遠心圧縮機は、
吸込み側から吐出側まで延びる翼長さの長い長羽根1
と、長羽根1の中間に設けられその中間位置から吐出側
まで延びる翼長さの短い短羽根2とを有する長短羽根車
3を備えている。この長短羽根車3は軸心Z-Zを中心
に回転し、図に矢印で示すように軸方向に空気を吸込
み、長羽根1と短羽根2とで遠心圧縮し、半径方向に圧
縮空気を吐出する。
FIG. 1 is a side view showing a long and short impeller of a centrifugal compressor according to the present invention. In this figure, (A) shows the first embodiment, (B) shows the second embodiment, and (C) shows the third embodiment. In each figure, the centrifugal compressor of the present invention is
Long blade 1 with a long blade length that extends from the suction side to the discharge side
And a short / short impeller 3 having a short blade 2 provided in the middle of the long blade 1 and extending from the intermediate position to the discharge side. The long / short impeller 3 rotates about the axis Z-Z, sucks air in the axial direction as indicated by an arrow in the figure, centrifugally compresses the long blade 1 and the short blade 2, and compresses compressed air in the radial direction. Discharge.

【0014】本発明の遠心圧縮機は、更に、空気を導入
するインデューサ部の長羽根1の外周部又は羽根車を囲
むシュラウド4に設けられた回転方向に沿った連通路6
を備える。
In the centrifugal compressor of the present invention, a communication passage 6 is provided in the shroud 4 surrounding the outer peripheral portion of the long blade 1 of the inducer section for introducing air or the impeller.
Equipped with.

【0015】図1(A)において、第1実施形態の連通
路6は、長羽根1の外周部に設けられた鋤歯状の溝6A
である。この鋤歯状の溝6Aは、この例では3つの切り
欠き部からなり、長羽根1の前縁から短羽根2の前縁ま
での間に軸方向に間隔を隔てて設けられている。
In FIG. 1 (A), the communication passage 6 of the first embodiment is a veneer-shaped groove 6 A provided on the outer peripheral portion of the long blade 1.
Is. The veil-shaped groove 6A is composed of three notches in this example, and is provided between the leading edge of the long blade 1 and the leading edge of the short blade 2 at an axial interval.

【0016】図1(B)において、第2実施形態の連通
路6は、シュラウド4の内周面に設けられた複数(この
例では3本)の円周溝6Bであり、各円周溝6Bは軸方
向に間隔を隔てて設けられている。
In FIG. 1B, the communication passage 6 of the second embodiment is a plurality of (three in this example) circumferential grooves 6B provided on the inner circumferential surface of the shroud 4, and each circumferential groove is formed. 6B are provided at intervals in the axial direction.

【0017】図1(C)において、第3実施形態の連通
路6は、長羽根1とこれを囲むシュラウド4との隙間6
Cである。この隙間6Cは、短羽根2とこれを囲むシュ
ラウド4との隙間2Cより大きく設定されている。
In FIG. 1C, the communication passage 6 of the third embodiment has a gap 6 between the long blade 1 and the shroud 4 surrounding the long blade 1.
It is C. The gap 6C is set larger than the gap 2C between the short blade 2 and the shroud 4 surrounding the short blade 2.

【0018】上述した連通路6、すなわち鋤歯状の溝6
A、円周溝6B、隙間6Cの大きさと個数は、長羽根の
BPF音を低減するように該当部分の圧力差を緩和し、
かつ漏れ損失による流体性能への悪影響を最小に留める
ように、実験等で決定するのがよい。また、図1(A)
(B)(C)の連通路6は、それぞれ単独でも、組合わ
せてもよい。
The above-mentioned communication passage 6, that is, the groove 6 in the shape of a vomer tooth.
The size and number of A, the circumferential groove 6B, and the gap 6C alleviate the pressure difference in the corresponding part so as to reduce the BPF sound of the long blades,
In addition, it is preferable to make an experiment or the like so as to minimize the adverse effect of the leakage loss on the fluid performance. In addition, FIG.
The communication passages 6 of (B) and (C) may be used alone or in combination.

【0019】[0019]

【実施例】図2(A)は、本発明の遠心圧縮機の翼負荷
分布図である。この図において横軸は、図2(B)に示
すシュラウドの子午面長さm2で無次元化したものであ
る。また縦軸は、正圧面側圧力P(P/S)と負圧正圧
面側圧力P(S/S)との圧力差を大気圧P0で割った
ものである。
EXAMPLE FIG. 2 (A) is a blade load distribution diagram of the centrifugal compressor of the present invention. In this figure, the horizontal axis is dimensionless with the meridional length m2 of the shroud shown in FIG. 2 (B). The vertical axis represents the pressure difference between the positive pressure surface side pressure P (P / S) and the negative pressure positive pressure surface side pressure P (S / S) divided by the atmospheric pressure P0.

【0020】図中の実線は従来の翼負荷分布図、破線は
本発明の第1実施形態(図1A)による翼負荷分布図で
ある。なお短羽根の前縁より下流側では、従来と本発明
で翼負荷分布図は一致している。
The solid line in the figure is a conventional blade load distribution chart, and the broken line is a blade load distribution chart according to the first embodiment (FIG. 1A) of the present invention. In the downstream side of the leading edge of the short blade, the blade load distribution maps of the conventional and the present invention are the same.

【0021】この図から、長羽根1の前縁(入口)から
短羽根2の前縁までの間において、正圧面側圧力P(P
/S)と負圧正圧面側圧力P(S/S)との圧力差が破
線に示すように低くなっており、その分、図5に示した
長羽根のBPF音(長羽根枚数×回転数の周波数音)を
低減できることがわかる。また、短羽根2の前縁より下
流側では、従来と本発明で翼負荷分布図が一致している
ことから、従来と同等の高い圧縮性能を維持できること
がわかる。
From this figure, from the leading edge (inlet) of the long blade 1 to the leading edge of the short blade 2, the pressure P side pressure P (P
/ S) and the pressure difference between the negative pressure and the positive pressure side P (S / S) are low as shown by the broken line, and the BPF sound of the long blade shown in FIG. It can be seen that the number of frequency sounds) can be reduced. Further, on the downstream side of the front edge of the short blade 2, since the blade load distribution maps of the conventional and the present invention are the same, it can be seen that the same high compression performance as the conventional can be maintained.

【0022】なお、本発明は上述した実施例に限定され
ず、本発明の要旨を逸脱しない限りで自由に変更するこ
とができることは勿論である。
The present invention is not limited to the above-mentioned embodiments, and it goes without saying that the present invention can be freely modified without departing from the gist of the present invention.

【0023】[0023]

【発明の効果】上述した本発明の構成によれば、空気を
導入するインデューサ部の長羽根1の外周部又は羽根車
を囲むシュラウド4に回転方向に沿って連通路6が設け
られているので、この連通路6を介して長羽根1の外周
部の正圧側と負圧側を連通し、その圧力差を低減し、イ
ンデューサ部の圧力差を小さくすることで長羽根のBP
F音を低減することができる。また、この連通路6をイ
ンデューサ部のみに設けているので、圧縮に寄与する遠
心部への影響は少なく、高い圧縮性能を維持することが
できる。
According to the above-described configuration of the present invention, the communication passage 6 is provided along the rotational direction in the shroud 4 surrounding the outer peripheral portion of the long blade 1 of the inducer portion for introducing air or the impeller. Therefore, the positive pressure side and the negative pressure side of the outer peripheral portion of the long blade 1 are communicated with each other through the communication passage 6, the pressure difference between them is reduced, and the pressure difference in the inducer portion is reduced, so that the BP of the long blade
The F sound can be reduced. Further, since the communication passage 6 is provided only in the inducer portion, the centrifugal portion that contributes to compression is less affected, and high compression performance can be maintained.

【0024】従って、インデューサ部の長羽根の正負圧
面の圧力差を緩和し、長羽根によるBPF音を低減で
き、かつ、漏れ損失も抑制でき、高い流体性能を維持す
ることができる。
Therefore, it is possible to reduce the pressure difference between the positive and negative pressure surfaces of the long blades of the inducer portion, reduce the BPF noise due to the long blades, suppress leakage loss, and maintain high fluid performance.

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

【図1】本発明の遠心圧縮機の長短羽根車を示す側面図
である。
FIG. 1 is a side view showing a long and short impeller of a centrifugal compressor according to the present invention.

【図2】本発明の遠心圧縮機の翼負荷分布図である。FIG. 2 is a blade load distribution diagram of the centrifugal compressor of the present invention.

【図3】従来の長短羽根車の模式図である。FIG. 3 is a schematic view of a conventional long / short impeller.

【図4】従来の長短羽根車のシュラウド部の翼面静圧分
布図である。
FIG. 4 is a blade surface static pressure distribution map of a shroud portion of a conventional long / short impeller.

【図5】従来の騒音周波数と音圧レベルの関係図であ
る。
FIG. 5 is a conventional relationship diagram between noise frequency and sound pressure level.

【符号の説明】 1 長羽根、2 短羽根、3 長短羽根車、4 シュラ
ウド、6 連通路、6A 鋤歯状の溝、6B 円周溝、
6C 隙間、
[Explanation of reference numerals] 1 long blade, 2 short blade, 3 long and short impeller, 4 shroud, 6 communicating passages, 6A vomer-shaped groove, 6B circumferential groove,
6C gap,

Claims (4)

【特許請求の範囲】[Claims] 【請求項1】 吸込み側から吐出側まで延びる翼長さの
長い長羽根(1)と、長羽根の中間に設けられその中間
位置から吐出側まで延びる翼長さの短い短羽根(2)と
を有する長短羽根車(3)を備えた遠心圧縮機におい
て、 空気を導入するインデューサ部の長羽根(1)の外周部
又は羽根車を囲むシュラウド(4)に回転方向に沿って
連通路(6)を設けたことを特徴とする長短羽根車を備
えた遠心圧縮機。
1. A long blade (1) having a long blade length extending from the suction side to the discharge side, and a short blade (2) provided in the middle of the long blade and having a short blade length extending from the intermediate position to the discharge side. In a centrifugal compressor provided with a long and short impeller (3) having an air passage, a communication passage (in a rotational direction) is provided to a shroud (4) surrounding the outer periphery of the long blade (1) of the inducer section for introducing air or the impeller. 6) The centrifugal compressor provided with a long and short impeller characterized by being provided.
【請求項2】 前記連通路(6)は、長羽根(1)の前
縁から短羽根(2)の前縁までの間の長羽根の外周部に
設けられ、軸方向に間隔を隔てた鋤歯状の溝(6A)で
ある、ことを特徴とする請求項1に記載の長短羽根車を
備えた遠心圧縮機。
2. The communication passages (6) are provided on an outer peripheral portion of the long blade between a front edge of the long blade (1) and a front edge of the short blade (2), and are axially spaced from each other. The centrifugal compressor with long and short impellers according to claim 1, wherein the centrifugal compressor is a groove (6A) in the shape of a tooth.
【請求項3】 前記連通路(6)は、シュラウド(4)
の内周面に設けられ、軸方向に間隔を隔てた複数の円周
溝(6B)である、ことを特徴とする請求項1に記載の
長短羽根車を備えた遠心圧縮機。
3. The shroud (4) is provided with the communication passage (6).
The centrifugal compressor with long and short impellers according to claim 1, wherein there are a plurality of circumferential grooves (6B) provided on the inner peripheral surface of the and spaced apart in the axial direction.
【請求項4】 前記連通路(6)は、長羽根(1)とこ
れを囲むシュラウドとの隙間(6C)であり、該隙間
(6C)は、短羽根(2)とこれを囲むシュラウドとの
隙間(2C)より大きく設定されている、ことを特徴と
する請求項1に記載の長短羽根車を備えた遠心圧縮機。
4. The communication passage (6) is a gap (6C) between the long blade (1) and a shroud surrounding the long blade (1), and the gap (6C) is formed between the short blade (2) and the shroud surrounding the short blade (2). The centrifugal compressor provided with the long and short impeller according to claim 1, wherein the centrifugal compressor is set to be larger than the gap (2C).
JP2002153306A 2002-05-28 2002-05-28 Centrifugal compressor equipped with long-and-short impeller Pending JP2003343486A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2002153306A JP2003343486A (en) 2002-05-28 2002-05-28 Centrifugal compressor equipped with long-and-short impeller

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2002153306A JP2003343486A (en) 2002-05-28 2002-05-28 Centrifugal compressor equipped with long-and-short impeller

Publications (1)

Publication Number Publication Date
JP2003343486A true JP2003343486A (en) 2003-12-03

Family

ID=29770367

Family Applications (1)

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

Country Link
JP (1) JP2003343486A (en)

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WO2014004238A1 (en) * 2012-06-25 2014-01-03 Borgwarner Inc. Exhaust-gas turbocharger
US10119411B2 (en) 2012-06-25 2018-11-06 Borgwarner Inc. Exhaust-gas turbocharger
US9982685B2 (en) 2012-07-26 2018-05-29 Borgwarner Inc. Compressor cover with circumferential groove
WO2014018270A1 (en) * 2012-07-26 2014-01-30 Borgwarner Inc. Compressor cover with circumferential groove
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DE102013201771A1 (en) 2013-02-04 2014-08-07 Bosch Mahle Turbo Systems Gmbh & Co. Kg Compressor of exhaust gas turbocharger mounted in internal combustion engine, forms with passage gap having passage gap inlet opening and passage gap outlet opening that are fluid connected with inlet and outlet channels of compressor
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