JPS58183899A - Diffuser with blade - Google Patents

Diffuser with blade

Info

Publication number
JPS58183899A
JPS58183899A JP6531282A JP6531282A JPS58183899A JP S58183899 A JPS58183899 A JP S58183899A JP 6531282 A JP6531282 A JP 6531282A JP 6531282 A JP6531282 A JP 6531282A JP S58183899 A JPS58183899 A JP S58183899A
Authority
JP
Japan
Prior art keywords
diffuser
scroll
outlet
flow
vaned
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
JP6531282A
Other languages
Japanese (ja)
Inventor
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 JP6531282A priority Critical patent/JPS58183899A/en
Publication of JPS58183899A publication Critical patent/JPS58183899A/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/40Casings; Connections of working fluid
    • F04D29/42Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/44Fluid-guiding means, e.g. diffusers
    • F04D29/441Fluid-guiding means, e.g. diffusers especially adapted for elastic fluid pumps
    • F04D29/444Bladed diffusers

Abstract

PURPOSE:To decrease the sectional area of a scroll to reduce the manufacturing cost of a casing by a method wherein the width of an outlet for the diffuser with blades is made larger than the same of an inlet therefor and the circumferential speed element of outlet flow is increased under keeping the reduction ratio of an absolute speed in the same value as before. CONSTITUTION:The diffuser 8, equipped with the blades, is constituted so that the width of the outlet thereof is larger than the same of the inlet thereof. According to this constitution, the angle of the outlet flow of the diffuser 8 is smaller than the angle of the flow in the conventional diffuser, therefore, the component of the circumferential speed at the outlet of the diffuser becomes larger than the same of the conventional diffuser. In case such flow is entered into the scroll 9a, an average speed in the scroll 9a may be made higher because the circumferential speed is high. Accordingly, the sectional area of the scroll 9a may be decreased and, as a result, the scroll 9a may be miniaturized to reduce the manufacturing cost of the scroll casing 9.

Description

【発明の詳細な説明】 本発明は、遠心形あるいは斜流形の流体機械の羽根付デ
ィフューザに関するもので、特に遠心または斜流圧縮機
に適用して好適なものである。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a vaned diffuser for a centrifugal or mixed flow type fluid machine, and is particularly suitable for application to a centrifugal or mixed flow compressor.

第1図は、従来の遠心圧縮機の縦断面図であり、図にお
いて、1は羽根車、2は回転軸、3は前記羽根車1を回
転軸2に固定するためのナツトである。羽根車の半径方
向外方には、一対の互いに平行なディフューザ板4およ
び5のみにより形成される流路すなわち羽根なしディフ
ューザs6と、ディフューザ板4.5および羽根7によ
り形成される羽根付ディフューザ部8とが設けられてお
り、さらにその外方にはスクロールケー7ング9が設け
られている。10は羽根車1の吸込口に流体を導くため
の吸込管である。
FIG. 1 is a longitudinal sectional view of a conventional centrifugal compressor. In the figure, 1 is an impeller, 2 is a rotating shaft, and 3 is a nut for fixing the impeller 1 to the rotating shaft 2. On the radially outward side of the impeller, there is a flow path formed only by a pair of mutually parallel diffuser plates 4 and 5, that is, a bladeless diffuser s6, and a bladed diffuser section formed by the diffuser plate 4.5 and the blades 7. 8 is provided, and a scroll case 7 9 is further provided on the outside thereof. 10 is a suction pipe for guiding fluid to the suction port of the impeller 1.

流体は吸込管10を通り吸込口から羽根車1に吸込まれ
る。流体は羽根車1で昇圧された後、ディフューザ部6
,8に入シ、このディフューザ部6.8内で流れは減速
されたのちスクロールケージング9によシ形成されたス
クロール9aに入る。
Fluid passes through the suction pipe 10 and is sucked into the impeller 1 from the suction port. After the fluid is pressurized by the impeller 1, it passes through the diffuser section 6.
, 8, the flow is decelerated in the diffuser section 6.8 and then enters the scroll 9a formed by the scroll casing 9.

ここで、ディフューザ部6.8出入口の流れの様子を第
2図に示す速度三角形で見てみる。図において、Cは絶
対速度を、Cmは絶対速度Cの周方向成分を、またC1
は絶対速度Cの子午面速度成分である。添字の3はベー
ン付ディフューザ部8の入口を、4ydは羽根付ディフ
ューザ部8の出口を表わす。羽根付ディツユ−ザ部8内
では入口から出口に向って面積は増加するので、子午面
速度C,は、C13からCm4va まで減少する。ま
た、□ 羽根付ディフューザ部8の羽根7は一般に出口
角度(局方向からはかった値)は入口角度より太きくな
るよう設計される。従って、羽根付ディフューザ部8の
出口部における流れ角α4v4もその入口部における流
れ角α3より大きくなり、周方向速度成分C,はC@3
からCm4vdに大幅に減少する。
Here, let us look at the state of the flow at the entrance and exit of the diffuser section 6.8 using the velocity triangle shown in FIG. In the figure, C is the absolute velocity, Cm is the circumferential component of the absolute velocity C, and C1
is the meridional velocity component of the absolute velocity C. The subscript 3 represents the inlet of the vaned diffuser section 8, and 4yd represents the outlet of the vaned diffuser section 8. Since the area within the vaned detuser section 8 increases from the inlet to the outlet, the meridional velocity C, decreases from C13 to Cm4va. Further, the blades 7 of the vaned diffuser section 8 are generally designed so that the exit angle (value measured from the direction of the blade) is larger than the entrance angle. Therefore, the flow angle α4v4 at the outlet of the vaned diffuser section 8 is also larger than the flow angle α3 at the inlet thereof, and the circumferential velocity component C, becomes C@3
to Cm4vd.

その結果、絶対速度CはC3からC4v aまで減少す
る。このように、従来の羽根付ディフューザ部8での流
れの減速は周方向速度成分C1の減少によるところが大
きい。
As a result, the absolute speed C decreases from C3 to C4va. As described above, the deceleration of the flow in the conventional vaned diffuser section 8 is largely due to the decrease in the circumferential velocity component C1.

次にスクロール9aの検討禽第1図〜第3図により行な
う。第3図に示すように、スクロール9a内における流
れの平均速度、をC1,とじたとき、この平均速度C,
,が次式の条件を満足するようにスクロール9aの断面
積は決められる。
Next, the examination of the scroll 9a will be carried out with reference to FIGS. 1 to 3. As shown in FIG. 3, when the average velocity of the flow inside the scroll 9a is C1, this average velocity C,
The cross-sectional area of the scroll 9a is determined so that , satisfies the following condition.

この式において、014日は羽根付ディフューザ部8の
出口における流れの周方向速度成分、几は羽根付ディフ
ューザ部8の出口半径、rBスクロール9aの断面中心
部における半径でおる。即ち、(1)式における等式の
左辺と右辺の値の差が大きい8から吐出される流体とが
衝突してスクロール損失が増加するので、これを避ける
ため(1)式の等式が成立するようにスクロール9aの
断面積が決められている。従来、羽根付ディフューザ部
8出日における周方向速度成分Co4vlは第2図に示
すように小さいので、スクロール損失を少なくするため
にはスクロール9aにおける平均速度Ca aも小さく
なるようにしなければならない。そのためにはスクロー
ル9mの断面積を大きくしなけ′ればならなかった。し
たがって、スクロールケーシング9の製作コストが高く
なるという欠点があった。
In this equation, 014 is the circumferential velocity component of the flow at the outlet of the vaned diffuser section 8, and 014 is the exit radius of the vaned diffuser section 8, and the radius at the center of the cross section of the rB scroll 9a. That is, in equation (1), the fluid discharged from 8, which has a large difference between the values on the left and right sides of the equation, collides with each other, increasing the scrolling loss, so to avoid this, equation (1) is established. The cross-sectional area of the scroll 9a is determined so as to. Conventionally, the circumferential velocity component Co4vl at sunrise of the vaned diffuser portion 8 is small as shown in FIG. 2, so in order to reduce scroll loss, the average velocity Ca a of the scroll 9a must also be small. To achieve this, it was necessary to increase the cross-sectional area of the 9 m scroll. Therefore, there was a drawback that the manufacturing cost of the scroll casing 9 was high.

本発明は上述した事に基づきなされたもので、スクロー
ルケーシングの製作コストを低減できる羽根付ディフュ
ーザを提供することを目的とするものである。
The present invention has been made based on the above-described matters, and an object of the present invention is to provide a vaned diffuser that can reduce the manufacturing cost of a scroll casing.

本発明の!黴は、一対のディフューザ板およびそのディ
フューザ板間に設けられた多数の羽根により構成される
流体機械の羽根付ディフューザにおいて、羽根付ディフ
ューザ部の出口幅がその人口偏よりも大きくなるように
構成した点にある。
The invention! Mold can be detected in a bladed diffuser for a fluid machine, which is composed of a pair of diffuser plates and a large number of blades provided between the diffuser plates, and is configured so that the outlet width of the bladed diffuser part is larger than the population deviation. At the point.

以下、本発明の一実施例を第4図および第5図により説
明する。図において、第1図〜第3図と同一符号を付し
た部分は同一部分である。この実施例は、本発明を遠心
圧縮機に適用した場合を示すものである。すなわち、本
発明の羽根付ディフューザは、半径方向を同いたハブ側
のディフューザ板5と、羽根なしディフューザ部6では
半径方向を向き羽根付ディフューザs8の入口から下流
ではディフューザの流路幅を拡げるような傾斜関金有す
るように形成したシュラウド側のディフューザ板4と、
これらディフューザ板4と5の間に設けられた多数の羽
根7とから構成されている。
An embodiment of the present invention will be described below with reference to FIGS. 4 and 5. In the figures, parts given the same reference numerals as in FIGS. 1 to 3 are the same parts. This example shows the case where the present invention is applied to a centrifugal compressor. That is, in the vaned diffuser of the present invention, the diffuser plate 5 on the hub side, which is radially the same, and the vaneless diffuser section 6 are oriented in the radial direction so as to widen the flow path width of the diffuser downstream from the inlet of the vaned diffuser s8. a diffuser plate 4 on the shroud side formed to have a sloped metal plate;
It is composed of a large number of blades 7 provided between these diffuser plates 4 and 5.

羽根7は、その出口角度がその入口角度とほぼ等しくな
るように構成さnている。羽根はディフューザs8の出
口半径Rは第1図に示す従来のものと同一であり、また
その出口幅は、その出口における流れの絶対速度C4゜
が従来のものにおける出口流れの絶対速度C4v aと
ほぼ等しくなるように選ばれている。
The vane 7 is configured such that its exit angle is approximately equal to its entrance angle. The exit radius R of the vane diffuser s8 is the same as that of the conventional one shown in FIG. are chosen so that they are approximately equal.

本発明による羽根付ディフューザ部8の出入口における
流れの速度三角形を第5図に示す。添字の40が本発明
による羽根付ディフューザ部8出口における流れを表わ
している。この図は、従来の羽根付ディフューザにおけ
る流れの速度三角形も同時に示している。図かられかる
ように、本発−明による羽根付ディフューザ部8の出口
部は従来の羽根付ディフューザ部の出口幅よりも大きく
なっているので、本発明の羽根付ディフューザ部8の出
口における流れの子午面速度Cm4mは、従来のものの
羽根付ディフューザ部における子午面速度C@4v4よ
りも小さくなる。また、本発明の羽根付ディフューザ部
8の出口流れ角α4.は従来の出口流れ角α4ydより
も小さいため、本発明による出口の周方向速度成分C1
4,は従来の羽根付ディ7−1L−ザ部8出口の周方向
速度成分C146よりも大きくなっている。
FIG. 5 shows a flow velocity triangle at the inlet and outlet of the vaned diffuser section 8 according to the present invention. The subscript 40 represents the flow at the outlet of the vaned diffuser section 8 according to the present invention. This figure also shows the velocity triangle of the flow in a conventional vaned diffuser. As can be seen from the figure, the outlet width of the vaned diffuser section 8 according to the present invention is larger than the exit width of the conventional vaned diffuser section, so that the flow at the outlet of the vaned diffuser section 8 according to the present invention is larger than the outlet width of the conventional vaned diffuser section 8. The meridional velocity Cm4m is smaller than the meridional velocity C@4v4 in the conventional bladed diffuser section. Further, the outlet flow angle α4 of the vaned diffuser portion 8 of the present invention. is smaller than the conventional outlet flow angle α4yd, the outlet circumferential velocity component C1 according to the present invention is smaller than the conventional outlet flow angle α4yd.
4 is larger than the circumferential velocity component C146 at the outlet of the conventional bladed dizzer 7-1L-za section 8.

このような流れがスクロールケーシング9によす形成さ
れたスクロール98に入った場合、周方向速度成分C1
4,が大きいため、スクロール9a内の平均速度C62
も大きくすることができる。したがって、スクロール9
mの断面積を小さくすることができ、その結果、従来よ
りもスクロール9aが小形化され、スクロールケーシン
グ9の製作コストを安価にすることができる。また、羽
根付ディフューザ部8出口流れの子午面速度成分は全て
スクロール内で損失となるが、本発明によるベーン付デ
ィフューザ部8出口流れの子午面速度成分C14,は、
従来の場合の子午面速度成分C,41よりも小さいため
スクロール損失も減少することになシ、遠心形、あるい
は斜流形の流体機械の性能も向上できるという効果があ
る。
When such a flow enters the scroll 98 formed around the scroll casing 9, the circumferential velocity component C1
4, is large, the average speed C62 in the scroll 9a
can also be made larger. Therefore, scroll 9
The cross-sectional area of m can be reduced, and as a result, the scroll 9a can be made smaller than before, and the manufacturing cost of the scroll casing 9 can be reduced. Furthermore, the meridional velocity component of the flow at the outlet of the vaned diffuser section 8 is all lost within the scroll, but the meridional velocity component C14 of the flow at the outlet of the vaned diffuser section 8 according to the present invention is as follows.
Since it is smaller than the meridional velocity component C, 41 in the conventional case, it has the effect of reducing scroll loss and improving the performance of centrifugal or mixed flow type fluid machines.

なお、上述した実施例では、シュラウド側のディフュー
ザ板4にディフューザ部の半径方向中心線に対し傾斜し
た面を有するように構成したが、シュラウド側のディフ
ューザ板4には傾斜面を形成しないでハブ側のディフュ
ーザ板5に傾斜面を形成するようにしてディフューザの
流路幅を拡げること、あるいは両方のディフューザ板4
.5に傾斜面を形成してディフューザ流路幅を拡げるよ
うに構成すること等の応用も可能である。また、しても
効果がある。
In the above-mentioned embodiment, the diffuser plate 4 on the shroud side is configured to have a surface inclined with respect to the radial center line of the diffuser portion, but the diffuser plate 4 on the shroud side is not formed with an inclined surface, By forming an inclined surface on the side diffuser plate 5 to widen the flow path width of the diffuser, or by forming an inclined surface on the side diffuser plate 5, or by forming an inclined surface on the side diffuser plate 5.
.. It is also possible to form an inclined surface on the diffuser 5 to widen the width of the diffuser flow path. It is also effective.

本発明によれば、羽根付ディフューザの絶対速度の減速
比を従来と同じに保ちながら、ディフューザ部出口流れ
の周方向速度成分を従来より大きくできるのでスクロー
ル断面積を小さくでき、し九がってスクロールケーシン
グの製作コストを低減できるという効果がある。
According to the present invention, while keeping the absolute speed reduction ratio of the bladed diffuser the same as before, the circumferential velocity component of the diffuser outlet flow can be made larger than before, so the cross-sectional area of the scroll can be reduced. This has the effect of reducing the manufacturing cost of the scroll casing.

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

第1図は従来の羽根付ディフューザを備えた遠心形流体
機械を示す縦断面図、第2図は従来の羽根付ディフュー
ザにおける出入口の速度三角形を示す図、第3図はディ
フューザ出口とスクロール内渡れの関係を説明する図、
第4図は本発明の羽根付ディフューザの一実施例を備え
だ遠心形流体機械を示す縦断面図、第5図は本発明の羽
根付ディフューザにおける出入口の速度三角形を示す図
である。 4・・・シュラウド側のディフューザ板、5・・・ハブ
側のディフューザ板、7・・・羽根、8・・・羽根付デ
ィフューザ部。 代理人 弁理士 薄田利幸 て1図 v3図 7 ′f3 4  図
Figure 1 is a vertical cross-sectional view showing a centrifugal fluid machine equipped with a conventional vaned diffuser, Figure 2 is a diagram showing the velocity triangle of the entrance and exit in a conventional vaned diffuser, and Figure 3 is a diagram showing the velocity triangle between the diffuser outlet and the scroll. A diagram explaining the relationship between
FIG. 4 is a longitudinal cross-sectional view showing a centrifugal fluid machine equipped with an embodiment of the vaned diffuser of the present invention, and FIG. 5 is a diagram showing velocity triangles at the entrance and exit of the vaned diffuser of the present invention. 4... Diffuser plate on the shroud side, 5... Diffuser plate on the hub side, 7... Vane, 8... Diffuser part with vane. Agent Patent Attorney Toshiyuki Usuda 1 Figure v 3 Figure 7 'f3 4 Figure

Claims (1)

【特許請求の範囲】[Claims] 一対のディフューザ板およびそのティフユーザ板間に設
けられた多数の羽根により構成される流体機械の羽根付
ディフューザにおいて、羽根付ディフューザ部の出口幅
がその入口幅よりも大きくなるように構成したことを特
徴とする羽根付ディフューザ。
In a vaned diffuser for a fluid machine consisting of a pair of diffuser plates and a large number of vanes provided between the tiff user plates, the outlet width of the vaned diffuser section is configured to be larger than the inlet width. Features a diffuser with blades.
JP6531282A 1982-04-21 1982-04-21 Diffuser with blade Pending JPS58183899A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP6531282A JPS58183899A (en) 1982-04-21 1982-04-21 Diffuser with blade

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP6531282A JPS58183899A (en) 1982-04-21 1982-04-21 Diffuser with blade

Publications (1)

Publication Number Publication Date
JPS58183899A true JPS58183899A (en) 1983-10-27

Family

ID=13283257

Family Applications (1)

Application Number Title Priority Date Filing Date
JP6531282A Pending JPS58183899A (en) 1982-04-21 1982-04-21 Diffuser with blade

Country Status (1)

Country Link
JP (1) JPS58183899A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5320489A (en) * 1993-06-01 1994-06-14 Ingersoll-Dresser Pump Company Diffuser for a centrifugal pump
US5529457A (en) * 1994-03-18 1996-06-25 Hitachi, Ltd. Centrifugal compressor
US10066638B2 (en) 2013-08-06 2018-09-04 Ihi Corporation Centrifugal compressor and turbocharger
CN108602170A (en) * 2015-11-20 2018-09-28 Ntt前进技术株式会社 The multistage of end surface of optical fiber connector grinding method and grinding film together
EP3708849A1 (en) * 2019-03-13 2020-09-16 Garrett Transportation I Inc. Turbocharger having adjustable-trim centrifugal compressor including divergent-wall diffuser

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5320489A (en) * 1993-06-01 1994-06-14 Ingersoll-Dresser Pump Company Diffuser for a centrifugal pump
US5529457A (en) * 1994-03-18 1996-06-25 Hitachi, Ltd. Centrifugal compressor
US10066638B2 (en) 2013-08-06 2018-09-04 Ihi Corporation Centrifugal compressor and turbocharger
CN108602170A (en) * 2015-11-20 2018-09-28 Ntt前进技术株式会社 The multistage of end surface of optical fiber connector grinding method and grinding film together
US10981256B2 (en) 2015-11-20 2021-04-20 Ntt Advanced Technology Corporation Multi-stage batch polishing method for end surface of optical fiber connector, and polishing film
EP3708849A1 (en) * 2019-03-13 2020-09-16 Garrett Transportation I Inc. Turbocharger having adjustable-trim centrifugal compressor including divergent-wall diffuser
US11131236B2 (en) 2019-03-13 2021-09-28 Garrett Transportation I Inc. Turbocharger having adjustable-trim centrifugal compressor including divergent-wall diffuser

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