JPS6138198A - Diffuser for centrifugal hydraulic machine - Google Patents

Diffuser for centrifugal hydraulic machine

Info

Publication number
JPS6138198A
JPS6138198A JP15749784A JP15749784A JPS6138198A JP S6138198 A JPS6138198 A JP S6138198A JP 15749784 A JP15749784 A JP 15749784A JP 15749784 A JP15749784 A JP 15749784A JP S6138198 A JPS6138198 A JP S6138198A
Authority
JP
Japan
Prior art keywords
diffuser
flow
impeller
angle
fluid
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.)
Granted
Application number
JP15749784A
Other languages
Japanese (ja)
Other versions
JPH0613878B2 (en
Inventor
Masakazu Hoshino
正和 星野
Yoichi Yoshinaga
吉永 洋一
Hideo Nishida
秀夫 西田
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.)
Hitachi Ltd
Original Assignee
Hitachi 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 Hitachi Ltd filed Critical Hitachi Ltd
Priority to JP59157497A priority Critical patent/JPH0613878B2/en
Publication of JPS6138198A publication Critical patent/JPS6138198A/en
Publication of JPH0613878B2 publication Critical patent/JPH0613878B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

PURPOSE:To recover the pressure sufficiently by controlling the secondary flow in lateral direction of flow path in diffuser then smoothing the flow distorted in lateral direction at the inlet of diffuser and decelerating thereby reducing the pressure loss. CONSTITUTION:Upon supply of flow distorted in lateral direction of the flow path of diffuser 7 from an impeller 4, the fluid at the sideboard 2 side having low flow angle is forcefully increased of the flow angle through a guide vane 12 to increase the speed component in radial direction thus to have sufficient kinetic energy for overcoming the pressure gradient in radial direction of the diffuser 7. Consequently, the fluid at the coreboard 3 side will flow to the sideboard 2 side and decelerated smoothly to the position separated by 1.2-1.3 times of the outerdiameter of the impeller 4 while being smoothed gradually. Since the guidevane 13 will guide such that the flow angle at the sideboard 2 side between said position of the outer diameter of the impeller 4 and the outlet of the diffuser 7 is brought to the design flow angle, the secondary flow from the coreboard 3 side to the sideboard 2 side is suppressed and decelerated smoothly thus to reduce the overall pressure loss.

Description

【発明の詳細な説明】 〔発明の利用分野〕 この発明は、遠心形流体機械のディフューザに係り、特
に大流量の遠心圧縮機に好適なディフューザに関する。
DETAILED DESCRIPTION OF THE INVENTION [Field of Application of the Invention] The present invention relates to a diffuser for a centrifugal fluid machine, and particularly to a diffuser suitable for a large flow rate centrifugal compressor.

〔発明の背景〕[Background of the invention]

従来の遠心形座縮機に用いられている羽根なしディフュ
ーザを第3図および第4図を用いて説明する。第3図に
示す様に、羽根1、側板2および心板3から成る遠心形
の羽根車4が、回転軸5に取り付けられた駆動機(図示
せず)により回転させられることにより、流体は吸込管
6を通り羽根車4内を通過する間にエネルギを与えられ
て高速の流れとなりディフューザ7に流れ込む。ディフ
ューザ7は、一対の対向する心板側ディフューザ板8と
側板側ディフューザ板9により構成され、その間に流路
を形成している。ディフューザ7において、羽根車4か
ら流出した流体は、その速度エネルギを圧力エネルギに
変換されながらスクロールケーシング10内に流入する
。そこで、さらに速度エネルギから圧力エネルギへの変
換が行なわれた流体は、スクロールケーシング10によ
り集合した流れとなり吐出口(図示せず)より流出する
。第4@の実験結果に示す様に、大流量形、つまり比速
度の高い遠心羽根車の出口流れの円周方向からとった流
れ角α2および絶対速度の半径方向速度成分C,は、側
板2側から心板3側にかけて大きくひずんだ分布となっ
ている。この傾向はディフューザ出口に向う程(rl−
+r2→r3になる程)増々強くなる。これは、側板2
側の流体は、流れ角α、が設計流れ角度αイに対して相
熱小さく半径方向速度成分CII+が非常に小さくなる
ために、ディフューザの圧力勾配に打つ勝つに足る運動
量がないため、徐々に側板2側の流れが逆流するように
なり、側板2側より各板3側に向う2次流れが起こるか
らである。
A bladeless diffuser used in a conventional centrifugal compactor will be explained with reference to FIGS. 3 and 4. As shown in FIG. 3, a centrifugal impeller 4 consisting of blades 1, side plates 2, and core plate 3 is rotated by a drive machine (not shown) attached to a rotating shaft 5, so that fluid is While passing through the suction pipe 6 and inside the impeller 4, it is given energy and becomes a high-speed flow, flowing into the diffuser 7. The diffuser 7 is composed of a pair of opposing core diffuser plates 8 and side diffuser plates 9, with a flow path formed therebetween. In the diffuser 7, the fluid flowing out from the impeller 4 flows into the scroll casing 10 while its velocity energy is converted into pressure energy. Therefore, the fluid whose velocity energy has been further converted into pressure energy forms a flow that is collected by the scroll casing 10 and flows out from a discharge port (not shown). As shown in the experimental results in No. 4 @, the flow angle α2 taken from the circumferential direction of the exit flow of a centrifugal impeller of a large flow type, that is, a high specific speed, and the radial velocity component C of the absolute velocity are The distribution is greatly distorted from the side to the core plate 3 side. This tendency becomes more pronounced toward the diffuser outlet (rl-
+r2 → r3) becomes stronger and stronger. This is side plate 2
The fluid on the side gradually loses momentum because the flow angle α is smaller than the design flow angle α, and the radial velocity component CII+ becomes very small. This is because the flow on the side plate 2 side becomes reverse flow, and a secondary flow from the side plate 2 side toward each plate 3 side occurs.

以上述べた様に、従来の遠心流体機械ディフューザでは
、羽根車出口直後の流れが、ディフューザの流路幅方向
にひずんだ分布となっているために、ディフューザにお
ける運動エネルギから圧力エネルギへの変換が十分に行
なわれないことと合せて、ばくり(逆流に起因する) 
ICよる圧力損失が増加することにより、流体性能が低
下するという欠点があった。
As mentioned above, in conventional centrifugal fluid mechanical diffusers, the flow immediately after the impeller exit has a distorted distribution in the width direction of the flow path of the diffuser, which makes it difficult to convert kinetic energy into pressure energy in the diffuser. In combination with not being done enough, exposure (due to reflux)
There was a drawback that fluid performance deteriorated due to increased pressure loss due to the IC.

この欠点を解決する方法として、本出願人番こよ板2側
に取り付けられた高さが低い案内羽根11の効果により
羽根車出口直後のディプユーザ流路幅方向にひずんだ流
れは一様化されるが、第6図(a)の実験結果に示す様
に羽根車外径の1.2から1.3倍を超えてからは各板
3側の減速が大きくなりすぎて、−担はぼ一様化した流
れが、羽根車出口とは逆の傾向のひずみを持つようにな
ってしまうという欠点がある。第6図(b)は、羽根車
出口直後の流れが順調に減速した場合の半径方向速度C
l1lの変化を示したものである。
As a method to solve this drawback, the distorted flow in the width direction of the dip user flow path immediately after the impeller exit is made uniform by the effect of the low-height guide vanes 11 attached to the side of the guard plate 2. However, as shown in the experimental results in Fig. 6(a), after the impeller's outer diameter exceeds 1.2 to 1.3 times, the deceleration on each plate 3 side becomes too large, and the -resistance becomes too large. The disadvantage is that the distorted flow will have a strain with a tendency opposite to that at the impeller outlet. Figure 6(b) shows the radial velocity C when the flow immediately after the impeller exit smoothly decelerates.
This shows the change in l1l.

〔発明の目的〕[Purpose of the invention]

本発明の目的は、ディフューザ内における流路幅方向の
2次流れを制御することにより、ディフューザ入口部に
おける流路幅方向にひずんだ流れを一様化し、この状態
を保ちながら滑らかに減速することによりディフューザ
内における圧力損失を低減し、ディフューザ出口の速度
をtJsさくして大きな圧力回復を得るようにした高性
能の遠心流体機械用ディフューザを提供するにある。
The purpose of the present invention is to uniformize the distorted flow in the width direction of the flow path at the entrance of the diffuser by controlling the secondary flow in the width direction of the flow path in the diffuser, and to smoothly decelerate the flow while maintaining this state. An object of the present invention is to provide a high-performance diffuser for a centrifugal fluid machine in which the pressure loss within the diffuser is reduced and the velocity at the diffuser outlet is reduced by tJs to obtain a large pressure recovery.

〔発明の概要〕[Summary of the invention]

本発明の遠心流体機械のディフューザは、ディフューザ
流路幅の1/3から115の高さを有し流路内の流九方
向に沿う複数枚の案内羽根を側板側ディフューザ板には
羽根車出口直後から羽根車゛外径の162〜1.3倍の
後位置まで、各板側ディフューザ板には羽根車外径の1
.2〜1.3倍の後位置からディフューザ出口径位置ま
で設けるものである。
The diffuser of the centrifugal fluid machine of the present invention has a plurality of guide vanes having a height of 1/3 to 115 times the width of the diffuser flow path and extending in the flow direction in the flow path, and the diffuser plate on the side plate side has a plurality of guide vanes arranged at the impeller outlet. From immediately afterward to the rear position of 162 to 1.3 times the outer diameter of the impeller, each diffuser plate has a diameter of 162 to 1.3 times the outer diameter of the impeller.
.. It is provided from the rear position of 2 to 1.3 times to the diffuser exit diameter position.

上述の構成によると、側板側の流体の流れ角度および半
径方向速度成分が強制的に大きくされることはもちろん
各板側の流体の流れ角度も強制的に任意の角度に保持さ
れることになるため、側板側流体がディフューザの圧力
勾配に打つ勝って流れることができ、且つ各板側流体も
羽根車外径の1.2〜1.3倍の後位置からはディフュ
ーザの圧力勾配に打ち勝って各板側から側板側に向う2
次流れを防止することができる。従って、流れの流路幅
方向の一様性を保ちながら減速できる。
According to the above configuration, not only the fluid flow angle and radial velocity component on the side plate side are forcibly increased, but also the fluid flow angle on each plate side is forcibly held at an arbitrary angle. Therefore, the fluid on the side plate side can overcome the pressure gradient of the diffuser and flow, and the fluid on each plate side can also overcome the pressure gradient of the diffuser and flow from the rear position 1.2 to 1.3 times the outer diameter of the impeller. From the board side to the side board side 2
Next flow can be prevented. Therefore, the flow can be decelerated while maintaining uniformity in the width direction of the flow path.

〔発明の実施例〕[Embodiments of the invention]

以下、本発明の一実施例を図面に基づいて説明する。 Hereinafter, one embodiment of the present invention will be described based on the drawings.

第1図に示すように、羽根1、側板2および心根3から
成る遠心形の羽根車4が、回転軸5に取り付けられた駆
動機(図示せず)により回転させられることにより、流
体が吸込管6を通り羽根車4内を通過する間にエネルギ
を与えられて高速の流れとなってディフューザ7に流れ
込むことは従来のものと同様である。
As shown in FIG. 1, a centrifugal impeller 4 consisting of blades 1, side plates 2, and core 3 is rotated by a drive machine (not shown) attached to a rotating shaft 5, so that fluid is sucked in. While passing through the pipe 6 and inside the impeller 4, it is given energy and becomes a high-speed flow that flows into the diffuser 7, as in the conventional case.

ディフューザ7の流路幅すの1/3〜115の高さの複
数枚の案内羽根が側板側ディフューザ板9の流路面上に
は羽根車直後の位置から羽根車外径の1.2〜1.3倍
の位置に、各板側のディフューザ板8の流路面上には羽
根車4外径の1.2〜1.3倍の位置からディフューザ
出口径の位置に取り付けられている。
A plurality of guide vanes with a height of 1/3 to 115 mm of the flow path width of the diffuser 7 are arranged on the flow path surface of the side diffuser plate 9 from a position immediately behind the impeller to a height of 1.2 to 1 mm of the impeller outer diameter. It is attached to the flow path surface of the diffuser plate 8 on each plate side from a position 1.2 to 1.3 times the outer diameter of the impeller 4 to a position corresponding to the diffuser outlet diameter.

第2図に示すように、側板側の案内羽根12の入口角度
β3は、設計流量点流れ角度αイより小さい値とする。
As shown in FIG. 2, the inlet angle β3 of the guide vane 12 on the side plate side is set to a value smaller than the flow angle αi at the design flow rate point.

出口角度β4は、設計流量点流れ角度αイにほぼ等しく
する。流れ角度β3からβ4までの変化は、滑らかにな
るように一円弧や対数螺旋などの曲線で近似して結ぶ。
The outlet angle β4 is made approximately equal to the design flow point flow angle αi. The change from flow angle β3 to β4 is approximated and connected by a curve such as a circular arc or a logarithmic spiral so as to be smooth.

また、心板側の案内羽根13の入口角度β5および出口
角度β6は、設計流量点流れ角度αイつまりβ4とほぼ
等しくする。
Further, the inlet angle β5 and the outlet angle β6 of the guide vane 13 on the core plate side are approximately equal to the design flow point flow angle αi, that is, β4.

このような構造とすることにより、羽根車4からディフ
ューザ流路幅方向にひずんだ流れがディフューザ7内に
流入した場合、流れ角度α2の小さい側板2側の流体は
、案内羽根12により強制的に流れ角度α2が起こされ
ることにより、半径方向速度成分が大きくなってディフ
ューザ7の半径方向の圧力勾配に打ち勝つに足る運動量
を持つようになるために、各板3側の流体が側板2側に
流れ込むようになり、ひずんだ流れが徐々に一様化され
ながら羽根車外径の1.2〜1.3倍の位置まで滑らか
に減速していく。また、案内羽根13は羽根車外径の1
.2〜1.3倍の位置からディフューザ出口までの各板
2側の流体の流れ角度を強制的に設計流れ角度αイにな
るようにガイドするので各板3側から側板2側に向う二
次流れが抑制される。
With this structure, when a distorted flow flows from the impeller 4 in the width direction of the diffuser flow path into the diffuser 7, the fluid on the side plate 2 side where the flow angle α2 is small is forcibly blocked by the guide vanes 12. By creating the flow angle α2, the radial velocity component becomes large and has enough momentum to overcome the radial pressure gradient of the diffuser 7, so the fluid on each plate 3 side flows into the side plate 2 side. The distorted flow gradually becomes uniform and decelerates smoothly to a position of 1.2 to 1.3 times the outer diameter of the impeller. Moreover, the guide vane 13 is 1 of the outer diameter of the impeller.
.. Since the fluid flow angle on each plate 2 side from the 2 to 1.3 times the position to the diffuser outlet is forced to be guided to the designed flow angle α, the secondary flow from each plate 3 side to the side plate 2 side is forced. Flow is restricted.

そのために、羽根外径の1.2〜1.3倍の位置からデ
ィフューザ出口径まで滑らか減速が達成される。
Therefore, smooth deceleration is achieved from a position 1.2 to 1.3 times the blade outer diameter to the diffuser outlet diameter.

〔発明の効果〕〔Effect of the invention〕

上述のとおり、本発明によれば、ディフューザ内におけ
る流体のばくり(逆流)が抑制され、ディフューザ内で
の減速が滑らかに達成されるようになり、全圧力損失が
低減されると共に十分な圧力回復が得られることになり
、ディフューザの性能が大幅に向上する。
As described above, according to the present invention, fluid backflow (backflow) within the diffuser is suppressed, smooth deceleration within the diffuser is achieved, total pressure loss is reduced, and sufficient pressure is maintained. Recovery will be obtained and the performance of the diffuser will be greatly improved.

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

第1図は本発明の実施例の縦断面図、第2図は第1図の
A−A矢視正面図、第3図および第5図は従来の遠心形
流体機械の縦断面図、第4図は第3図に示したディフュ
ーザ向流れの分布図、第6図は第5図に示したディフュ
ーザ向流れの分布図である。
FIG. 1 is a longitudinal sectional view of an embodiment of the present invention, FIG. 2 is a front view taken along the line A-A in FIG. 1, and FIGS. 3 and 5 are longitudinal sectional views of a conventional centrifugal fluid machine. 4 is a distribution diagram of the flow toward the diffuser shown in FIG. 3, and FIG. 6 is a distribution diagram of the flow toward the diffuser shown in FIG. 5.

Claims (1)

【特許請求の範囲】[Claims] 遠心形流体機械の羽根車の外周に設けられる一対のディ
フューザ板の間に流路を形成したディフューザにおいて
、ディフューザ流路幅の1/3から1/5の高さを有し
流路内の流れ方向に沿う複数枚の案内羽根を側板側ディ
フューザ板には羽根車出口直後から羽根車外径の1.2
〜1.3倍の径位置まで、心板側ディフューザ板には羽
根車外径の1.2〜1.3倍の径位置からディフューザ
出口径位置まで設けたことを特徴とする遠心形流体機械
のディフューザ。
In a diffuser in which a flow path is formed between a pair of diffuser plates provided on the outer periphery of an impeller of a centrifugal fluid machine, the diffuser has a height of 1/3 to 1/5 of the width of the diffuser flow path and extends in the flow direction within the flow path. A plurality of guide vanes are installed along the side diffuser plate from immediately after the impeller exit to 1.2 of the outer diameter of the impeller.
A centrifugal fluid machine characterized in that the core plate side diffuser plate is provided from a diameter position of 1.2 to 1.3 times the impeller outer diameter to a diffuser outlet diameter position. diffuser.
JP59157497A 1984-07-30 1984-07-30 Centrifugal compressor Expired - Fee Related JPH0613878B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP59157497A JPH0613878B2 (en) 1984-07-30 1984-07-30 Centrifugal compressor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP59157497A JPH0613878B2 (en) 1984-07-30 1984-07-30 Centrifugal compressor

Publications (2)

Publication Number Publication Date
JPS6138198A true JPS6138198A (en) 1986-02-24
JPH0613878B2 JPH0613878B2 (en) 1994-02-23

Family

ID=15650973

Family Applications (1)

Application Number Title Priority Date Filing Date
JP59157497A Expired - Fee Related JPH0613878B2 (en) 1984-07-30 1984-07-30 Centrifugal compressor

Country Status (1)

Country Link
JP (1) JPH0613878B2 (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4877370A (en) * 1987-09-01 1989-10-31 Hitachi, Ltd. Diffuser for centrifugal compressor
EP0610051A1 (en) * 1993-02-03 1994-08-10 Dresser-Rand Company Rib diffuser
US5516263A (en) * 1993-04-28 1996-05-14 Hitachi, Ltd. Centrifugal compressor and vaned diffuser
JP2011089460A (en) * 2009-10-22 2011-05-06 Hitachi Plant Technologies Ltd Turbo type fluid machine
CN113217470A (en) * 2020-02-04 2021-08-06 三菱重工业株式会社 Diffuser structure of centrifugal compressor and centrifugal compressor
WO2022093434A1 (en) * 2020-10-30 2022-05-05 Praxair Technology, Inc. Hydrogen centrifugal compressor

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR102260315B1 (en) * 2020-10-12 2021-06-03 유진기공산업 주식회사 Centrifugal compressor

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5629099A (en) * 1979-08-01 1981-03-23 Hitachi Ltd Diffuser for centrifugal fluid machinery

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5629099A (en) * 1979-08-01 1981-03-23 Hitachi Ltd Diffuser for centrifugal fluid machinery

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4877370A (en) * 1987-09-01 1989-10-31 Hitachi, Ltd. Diffuser for centrifugal compressor
EP0610051A1 (en) * 1993-02-03 1994-08-10 Dresser-Rand Company Rib diffuser
US5516263A (en) * 1993-04-28 1996-05-14 Hitachi, Ltd. Centrifugal compressor and vaned diffuser
US5709531A (en) * 1993-04-28 1998-01-20 Hitachi, Ltd. Centrifugal compressor and vaned diffuser
JP2011089460A (en) * 2009-10-22 2011-05-06 Hitachi Plant Technologies Ltd Turbo type fluid machine
CN113217470A (en) * 2020-02-04 2021-08-06 三菱重工业株式会社 Diffuser structure of centrifugal compressor and centrifugal compressor
JP2021124046A (en) * 2020-02-04 2021-08-30 三菱重工業株式会社 Diffuser structure of centrifugal compressor, and centrifugal compressor
WO2022093434A1 (en) * 2020-10-30 2022-05-05 Praxair Technology, Inc. Hydrogen centrifugal compressor
US11401947B2 (en) 2020-10-30 2022-08-02 Praxair Technology, Inc. Hydrogen centrifugal compressor

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Publication number Publication date
JPH0613878B2 (en) 1994-02-23

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