JPH0618080Y2 - Multi-stage centrifugal compressor - Google Patents

Multi-stage centrifugal compressor

Info

Publication number
JPH0618080Y2
JPH0618080Y2 JP1987148569U JP14856987U JPH0618080Y2 JP H0618080 Y2 JPH0618080 Y2 JP H0618080Y2 JP 1987148569 U JP1987148569 U JP 1987148569U JP 14856987 U JP14856987 U JP 14856987U JP H0618080 Y2 JPH0618080 Y2 JP H0618080Y2
Authority
JP
Japan
Prior art keywords
centrifugal compressor
stage
flow
intermediate discharge
intermediate stage
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 - Lifetime
Application number
JP1987148569U
Other languages
Japanese (ja)
Other versions
JPS6451794U (en
Inventor
一三 片山
信之 野島
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.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries 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 Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP1987148569U priority Critical patent/JPH0618080Y2/en
Publication of JPS6451794U publication Critical patent/JPS6451794U/ja
Application granted granted Critical
Publication of JPH0618080Y2 publication Critical patent/JPH0618080Y2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Landscapes

  • Structures Of Non-Positive Displacement Pumps (AREA)

Description

【考案の詳細な説明】 〔産業上の利用分野〕 本考案は多段遠心圧縮機の改良に関するものである。DETAILED DESCRIPTION OF THE INVENTION [Industrial field of application] The present invention relates to an improvement of a multistage centrifugal compressor.

〔従来の技術〕[Conventional technology]

第2図は従来の多段遠心圧縮機の断面図で,図中1は主
軸,2は中間段インペラ,3は中間段ディフューザ,7
は次段に流れを導くためのリターンベンド,8は次段に
流れを導くためのリターンベーンである。
FIG. 2 is a sectional view of a conventional multistage centrifugal compressor, in which 1 is a main shaft, 2 is an intermediate stage impeller, 3 is an intermediate stage diffuser, and 7
Is a return bend for guiding the flow to the next stage, and 8 is a return vane for guiding the flow to the next stage.

〔考案が解決しようとする問題点〕 本考案は従来の多段遠心圧縮機において,中間段の流量
の一部を外部に取り出して利用し得るようにしたもので
ある。この場合,中間吐出流れの圧損の低減と,中間吐
出を行う中間段の性能が中間吐出によって低下しないこ
とが必要である。
[Problems to be Solved by the Invention] The present invention is a conventional multistage centrifugal compressor in which a part of the flow rate of the intermediate stage is taken out to the outside for use. In this case, it is necessary that the pressure loss of the intermediate discharge flow be reduced and that the performance of the intermediate stage that performs the intermediate discharge is not deteriorated by the intermediate discharge.

中間吐出流れの圧損は,中間段から分流する際の流速が
高い程増大するので,分流点を流速の低いところに選ぶ
必要があり,中間段の性能が中間吐出によって低下しな
いためには,中間吐出流れが円周上から均一に流出する
ことが必要である。
Since the pressure drop of the intermediate discharge flow increases as the flow velocity at the time of branching from the intermediate stage increases, it is necessary to select the diversion point at a place where the flow velocity is low. It is necessary that the discharge flow uniformly flows out from the circumference.

また円周上から均一に流出する流体を効率良く集めて吐
出口に導く必要がある。
Further, it is necessary to efficiently collect the fluid that uniformly flows out from the circumference and guide it to the discharge port.

本考案は上記の条件を満足し得る多段遠心圧縮機を提供
せんとするものである。
The present invention is intended to provide a multi-stage centrifugal compressor that can satisfy the above conditions.

〔問題点を解決するための手段〕 本考案は中間吐出流れの圧損の低減と中間段の性能低下
を最小にするため,中間段の分流点を流速の遅い中間段
ディフューザの出口部分に選び,中間吐出流れが円周上
から均一に流出するための流路として円周スリットを設
けると共に,円周スリットから流出する流れを効率良く
中間吐出ダクトに導くための中間吐出スクロールを設け
て,多段遠心圧縮機を構成したことを特徴とするもので
ある。
[Means for solving the problem] In the present invention, in order to reduce the pressure loss of the intermediate discharge flow and minimize the performance deterioration of the intermediate stage, the branch point of the intermediate stage is selected as the outlet part of the intermediate stage diffuser with a slow flow velocity. A multi-stage centrifuge is equipped with a circumferential slit as a flow path for the intermediate discharge flow to uniformly flow out from the circumference, and an intermediate discharge scroll for efficiently guiding the flow flowing from the circumferential slit to the intermediate discharge duct. It is characterized by constituting a compressor.

〔作用〕[Action]

本考案の多段遠心圧縮機は上記のように構成されている
ので,主軸及び中間段インペラが回転すると,流体はイ
ンペラから流出して中間段ディフューザを通り,中間段
ディフューザの出口部分で,一部は円周スリット,中間
吐出スクロールを通って中間吐出ダクトに導かれ,一部
はリターンベンドを通って次の段に導かれることにな
る。
Since the multistage centrifugal compressor of the present invention is configured as described above, when the main shaft and the intermediate stage impeller rotate, the fluid flows out of the impeller, passes through the intermediate stage diffuser, and partially exits the intermediate stage diffuser. Is guided to the intermediate discharge duct through the circumferential slit and the intermediate discharge scroll, and part of it is guided to the next stage through the return bend.

〔実施例〕〔Example〕

以下,本考案を図面に示す実施例に基づいて具体的に説
明する。
Hereinafter, the present invention will be described in detail with reference to the embodiments shown in the drawings.

第1図は本考案の1実施例を示す多段遠心圧縮機の断面
図で,図中第2図に示す部材と同一部材には同一符号を
付し,重複した説明は省略する。
FIG. 1 is a cross-sectional view of a multi-stage centrifugal compressor showing an embodiment of the present invention. In the figure, the same members as those shown in FIG.

図中4は中間吐出用の円周スリット,5は中間吐出スク
ロール,6は中間吐出ダクトを示し,この部分が新規に
工夫した点である。
In the figure, 4 is a circumferential slit for intermediate discharge, 5 is an intermediate discharge scroll, and 6 is an intermediate discharge duct. This part is a newly devised point.

上記のように構成された本実施例の多段遠心圧縮機にお
いては,主軸1,中間段インペラ2が回転すると,流体
は中間段インペラ2から流出して中間段ディフューザ3
を通り,中間段ディフューザ3の出口部分で,一部は円
周スリット4,中間吐出スクロール5を通って中間吐出
ダクト6に導かれ,一部はリターンベンド7,リターン
ベーン8を通って次の段に導かれる。
In the multistage centrifugal compressor of the present embodiment configured as described above, when the main shaft 1 and the intermediate stage impeller 2 rotate, the fluid flows out from the intermediate stage impeller 2 and the intermediate stage diffuser 3
At the outlet of the intermediate diffuser 3, a part is guided to the intermediate discharge duct 6 through the circumferential slit 4 and the intermediate discharge scroll 5, and a part is further passed through the return bend 7 and the return vane 8. Guided to the stage.

〔考案の効果〕[Effect of device]

以上具体的に説明したように,本考案の多段遠心圧縮機
においては,中間段の分流点が中間段ディフューザの出
口部分に設けられているため,この点の流速が低いこ
と,及び中間吐出流れが円周スリットにより円周上均一
であり,かつ,中間吐出スクロールにより効率良く中間
吐出ダクトまで導かれることにより,中間吐出流れの圧
損は最低限に押えられる。またこの結果,リターンベン
ドを通る流れも円周上均一となり,中間段の性能低下は
最小となる。
As described in detail above, in the multistage centrifugal compressor of the present invention, since the intermediate stage branch point is provided at the outlet of the intermediate stage diffuser, the flow velocity at this point is low and the intermediate discharge flow is low. Is uniform on the circumference by the circumferential slit, and is efficiently guided to the intermediate discharge duct by the intermediate discharge scroll, so that the pressure loss of the intermediate discharge flow is suppressed to a minimum. As a result, the flow through the return bend is also uniform on the circumference, and the performance degradation of the intermediate stage is minimized.

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

第1図は本考案の1実施例を示す多段遠心圧縮機の断面
図,第2図は従来の多段遠心圧縮機の断面図である。 1…主軸,2…中間段インペラ,3…中間段ディフュー
ザ,4…中間吐出用の円周スリット,5…中間吐出スク
ロール,6…中間吐出ダクト,7…次段に流れを導くた
めのリターンベンド,8…次段に流れを導くためのリタ
ーンベーン
FIG. 1 is a sectional view of a multistage centrifugal compressor showing one embodiment of the present invention, and FIG. 2 is a sectional view of a conventional multistage centrifugal compressor. DESCRIPTION OF SYMBOLS 1 ... Main shaft, 2 ... Intermediate stage impeller, 3 ... Intermediate stage diffuser, 4 ... Circumferential slit for intermediate discharge, 5 ... Intermediate discharge scroll, 6 ... Intermediate discharge duct, 7 ... Return bend for guiding flow to the next stage , 8 ... Return vanes to guide the flow to the next stage

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 【請求項1】多段遠心圧縮機の中間段ディフューザの出
口部分に,中間段を流れる流量の一部を圧縮機から取り
出すための円周スリットと,円周スリットから流出する
流体を中間吐出ダクトに導くための中間吐出スクロール
を設けたことを特徴とする多段遠心圧縮機。
1. A circumferential slit for taking out a part of the flow rate of the intermediate stage from the compressor at an outlet portion of an intermediate stage diffuser of a multistage centrifugal compressor, and a fluid flowing out from the circumferential slit to an intermediate discharge duct. A multistage centrifugal compressor characterized by being provided with an intermediate discharge scroll for guiding.
JP1987148569U 1987-09-29 1987-09-29 Multi-stage centrifugal compressor Expired - Lifetime JPH0618080Y2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1987148569U JPH0618080Y2 (en) 1987-09-29 1987-09-29 Multi-stage centrifugal compressor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1987148569U JPH0618080Y2 (en) 1987-09-29 1987-09-29 Multi-stage centrifugal compressor

Publications (2)

Publication Number Publication Date
JPS6451794U JPS6451794U (en) 1989-03-30
JPH0618080Y2 true JPH0618080Y2 (en) 1994-05-11

Family

ID=31420006

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1987148569U Expired - Lifetime JPH0618080Y2 (en) 1987-09-29 1987-09-29 Multi-stage centrifugal compressor

Country Status (1)

Country Link
JP (1) JPH0618080Y2 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP5929016B2 (en) * 2011-06-10 2016-06-01 株式会社Ihi Scroll housing and turbocharger
DE102012204403A1 (en) * 2012-03-20 2013-09-26 Man Diesel & Turbo Se Centrifugal compressor unit
JP2023119272A (en) 2022-02-16 2023-08-28 三菱重工コンプレッサ株式会社 centrifugal compressor

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4884903A (en) * 1972-02-15 1973-11-10
JPS57206800A (en) * 1981-06-15 1982-12-18 Hitachi Ltd Single shaft multi-stage centrifugal compressor

Also Published As

Publication number Publication date
JPS6451794U (en) 1989-03-30

Similar Documents

Publication Publication Date Title
US6279322B1 (en) Deswirler system for centrifugal compressor
US2658455A (en) Impeller with center intake
CN101163889B (en) Turbocharger compressor having ported second-stage shroud, and associated method
US3986791A (en) Hydrodynamic multi-stage pump
EP0425651A1 (en) Compressor shroud air bleed passages
DK158213B (en) AXIAL BLADE WITH A STABILIZING DEVICE FOR STABILIZING OPERATION
GB1024584A (en) Improvements in or relating to centrifugal blowers, compressors, pumps or the like
KR100822070B1 (en) Centrifugal type turbo machine
JP2001200797A (en) Multistage centrifugal compressor
JPH0618080Y2 (en) Multi-stage centrifugal compressor
JP7429810B2 (en) Multi-stage centrifugal fluid machine
JPH03264796A (en) Mixed flow compressor
US2311024A (en) Guide apparatus for centrifugal blowers and pumps
GB920188A (en) Improvements in or relating to centrifugal fans and compressors
JPS60132099A (en) Centrifugal compressor
US3278115A (en) Control of inlet flow to centrifugal fluid movers
JPH04143499A (en) Diffuser of centrifugal fluid machine
JPS6138198A (en) Diffuser for centrifugal hydraulic machine
SE509390C2 (en) Steam turbine
JPH0278794A (en) Mixed flow type compressor
JP3036220B2 (en) Centrifugal compressor
WO2024122378A1 (en) Centrifugal fluid machine and single-shaft multi-stage centrifugal compressor
JP2703055B2 (en) Mixed flow compressor
US2995293A (en) Guide means on impellers for centrifugal pumps or blowers
JPH0676697U (en) Centrifugal compressor