JPH0254400U - - Google Patents

Info

Publication number
JPH0254400U
JPH0254400U JP13375788U JP13375788U JPH0254400U JP H0254400 U JPH0254400 U JP H0254400U JP 13375788 U JP13375788 U JP 13375788U JP 13375788 U JP13375788 U JP 13375788U JP H0254400 U JPH0254400 U JP H0254400U
Authority
JP
Japan
Prior art keywords
holes
hollow chamber
internal passage
annular hollow
outlet side
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
JP13375788U
Other languages
Japanese (ja)
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 JP13375788U priority Critical patent/JPH0254400U/ja
Publication of JPH0254400U publication Critical patent/JPH0254400U/ja
Pending legal-status Critical Current

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Description

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

第1図は本考案の第1実施例に係るターボ圧縮
機の断面図、第2図は第1図の―線部分の断
面図、第3図は本考案の第2実施例に係るターボ
圧縮機の断面図、第4図は従来のターボ圧縮機の
全体構成図である。 3……インペラ、4a,4b,4c……内部通
路、5……静止隔壁、6……環状中空室、7,7
a……凹所、8……第1貫通孔、10……流量調
節リング、11……第2貫通孔。
Fig. 1 is a sectional view of a turbo compressor according to a first embodiment of the present invention, Fig. 2 is a sectional view taken along the line - - in Fig. 1, and Fig. 3 is a turbo compressor according to a second embodiment of the present invention. A sectional view of the machine, FIG. 4 is an overall configuration diagram of a conventional turbo compressor. 3... Impeller, 4a, 4b, 4c... Internal passage, 5... Stationary bulkhead, 6... Annular hollow chamber, 7, 7
a... Recess, 8... First through hole, 10... Flow rate adjustment ring, 11... Second through hole.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] インペラの入側と出側の内部通路を仕切る静止
隔壁の内部に上記出側或いはこれより後段のイン
ペラの出側の内部通路に連通させるように設けた
環状中空室と、この環状中空室の壁部に上記入側
の内部通路に連通するように適宜数形成した第1
貫通孔と、この各第1貫通孔と同じ位置関係で同
数の第2貫通孔を形成するとともに、上記環状中
空室の第1貫通孔側の壁面に対して摺動可能に当
接させて、上記各第2貫通孔の開口面積を同時に
調節可能に設けた流量調節リングとを設けたこと
を特徴とするターボ圧縮機。
An annular hollow chamber is provided inside a stationary partition wall that partitions the internal passage on the inlet side and the outlet side of the impeller so as to communicate with the internal passage on the outlet side or the outlet side of the impeller at a later stage, and a wall of the annular hollow chamber. An appropriate number of first holes are formed in the section so as to communicate with the internal passage on the input side.
The same number of second through holes are formed in the same positional relationship as the through holes and each of the first through holes, and the second through holes are slidably abutted against the wall surface on the first through hole side of the annular hollow chamber, A turbo compressor characterized in that a flow rate adjustment ring is provided in which the opening area of each of the second through holes can be adjusted simultaneously.
JP13375788U 1988-10-12 1988-10-12 Pending JPH0254400U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP13375788U JPH0254400U (en) 1988-10-12 1988-10-12

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP13375788U JPH0254400U (en) 1988-10-12 1988-10-12

Publications (1)

Publication Number Publication Date
JPH0254400U true JPH0254400U (en) 1990-04-19

Family

ID=31391916

Family Applications (1)

Application Number Title Priority Date Filing Date
JP13375788U Pending JPH0254400U (en) 1988-10-12 1988-10-12

Country Status (1)

Country Link
JP (1) JPH0254400U (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2009011241A1 (en) * 2007-07-19 2009-01-22 Ihi Corporation Gas compression device and method of controlling gas compression device
WO2015119140A1 (en) * 2014-02-05 2015-08-13 三菱重工業株式会社 Diaphragm and centrifugal rotating machine
EP3805565A1 (en) * 2019-10-07 2021-04-14 Elliott Company Methods and mechanisms for surge avoidance in multi-stage centrifugal compressors

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2009011241A1 (en) * 2007-07-19 2009-01-22 Ihi Corporation Gas compression device and method of controlling gas compression device
WO2015119140A1 (en) * 2014-02-05 2015-08-13 三菱重工業株式会社 Diaphragm and centrifugal rotating machine
EP3805565A1 (en) * 2019-10-07 2021-04-14 Elliott Company Methods and mechanisms for surge avoidance in multi-stage centrifugal compressors
JP2021060033A (en) * 2019-10-07 2021-04-15 エリオット・カンパニー Methods and mechanisms for surge avoidance in multi-stage centrifugal compressors
CN112696364A (en) * 2019-10-07 2021-04-23 艾略特公司 Method and mechanism for preventing surge of multistage centrifugal compressor
US11255338B2 (en) 2019-10-07 2022-02-22 Elliott Company Methods and mechanisms for surge avoidance in multi-stage centrifugal compressors
CN112696364B (en) * 2019-10-07 2024-02-20 艾略特公司 Method and mechanism for preventing surge of multistage centrifugal compressor

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