JPS5535173A - Method of and apparatus for enlarging surge margin in centrifugal compressor and axial flow conpressor - Google Patents

Method of and apparatus for enlarging surge margin in centrifugal compressor and axial flow conpressor

Info

Publication number
JPS5535173A
JPS5535173A JP10877378A JP10877378A JPS5535173A JP S5535173 A JPS5535173 A JP S5535173A JP 10877378 A JP10877378 A JP 10877378A JP 10877378 A JP10877378 A JP 10877378A JP S5535173 A JPS5535173 A JP S5535173A
Authority
JP
Japan
Prior art keywords
point
surge
high pressure
enlarging
surge margin
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
JP10877378A
Other languages
Japanese (ja)
Inventor
Sadao Sato
Shigeto Hosomi
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.)
Kobe Steel Ltd
Original Assignee
Kobe Steel 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 Kobe Steel Ltd filed Critical Kobe Steel Ltd
Priority to JP10877378A priority Critical patent/JPS5535173A/en
Publication of JPS5535173A publication Critical patent/JPS5535173A/en
Pending legal-status Critical Current

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  • Control Of Positive-Displacement Air Blowers (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

PURPOSE: To permit enlargement of the surge margin without reducing the maximum stage efficiency by arranging such that part of fluid on the high pressure side is introduced to an inducer tip portion of a vane wheel at an instant when the working point of the compressor reaches a point right before the surge point or in the neighborhood of a stall point.
CONSTITUTION: When the working point of the compressor reaches a point right before the surge point or the neighborhood of a stall point, this is detected, and at the same time part of the high pressure fluid extracted from a high pressure section of the compressor is led through a duct 14 and an on-off valve 13 to a header section 13, and is injected as a high speed jet from jet ports 12a of an injection ring 12 into an inducer tip section 9c. In consequence, instable low speed fluid over a vane surface 8 is given energy to increase the insensity of turbulence, whereby the boundary layer is prevente from being peeled-off or re-attached. In this way, an effect of enlarging the surge margin is reliably obtained to permit stable operation.
COPYRIGHT: (C)1980,JPO&Japio
JP10877378A 1978-09-02 1978-09-02 Method of and apparatus for enlarging surge margin in centrifugal compressor and axial flow conpressor Pending JPS5535173A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP10877378A JPS5535173A (en) 1978-09-02 1978-09-02 Method of and apparatus for enlarging surge margin in centrifugal compressor and axial flow conpressor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP10877378A JPS5535173A (en) 1978-09-02 1978-09-02 Method of and apparatus for enlarging surge margin in centrifugal compressor and axial flow conpressor

Publications (1)

Publication Number Publication Date
JPS5535173A true JPS5535173A (en) 1980-03-12

Family

ID=14493111

Family Applications (1)

Application Number Title Priority Date Filing Date
JP10877378A Pending JPS5535173A (en) 1978-09-02 1978-09-02 Method of and apparatus for enlarging surge margin in centrifugal compressor and axial flow conpressor

Country Status (1)

Country Link
JP (1) JPS5535173A (en)

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS613999U (en) * 1984-06-12 1986-01-11 三菱重工業株式会社 Casing treatment device for fluid machinery
US4930978A (en) * 1988-07-01 1990-06-05 Household Manufacturing, Inc. Compressor stage with multiple vented inducer shroud
JPH0610885A (en) * 1992-04-10 1994-01-21 Ingersoll Rand Co Surge control and recovery of centrifugal compressor
EP0606475A4 (en) * 1991-10-04 1994-01-26 Ebara Corp Turbo-machine.
US5466118A (en) * 1993-03-04 1995-11-14 Abb Management Ltd. Centrifugal compressor with a flow-stabilizing casing
EP0754864A1 (en) * 1995-07-18 1997-01-22 Ebara Corporation Turbomachine
US6244817B1 (en) * 1996-12-05 2001-06-12 Mcdonnell Douglas Corporation Method and apparatus for a fan noise controller
JP2009228625A (en) * 2008-03-25 2009-10-08 Mitsubishi Heavy Ind Ltd Casing for axial flow type compressor
JP2013072418A (en) * 2011-09-29 2013-04-22 Mitsubishi Heavy Ind Ltd Compressor
JP2013194687A (en) * 2012-03-22 2013-09-30 Mitsubishi Heavy Ind Ltd Multistage centrifugal compressor
WO2022202412A1 (en) * 2021-03-25 2022-09-29 三菱重工マリンマシナリ株式会社 Compressor casing, supercharger, and method for operating supercharger
DE112012002692B4 (en) 2011-06-29 2022-11-24 OPRA Technologies, B.V. Apparatus and method for reducing air mass flow for low emission combustion over an extended range in single spool gas turbines

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS613999U (en) * 1984-06-12 1986-01-11 三菱重工業株式会社 Casing treatment device for fluid machinery
US4930978A (en) * 1988-07-01 1990-06-05 Household Manufacturing, Inc. Compressor stage with multiple vented inducer shroud
EP0606475A4 (en) * 1991-10-04 1994-01-26 Ebara Corp Turbo-machine.
EP0606475A1 (en) * 1991-10-04 1994-07-20 Ebara Corporation Turbo-machine
US5458457A (en) * 1991-10-04 1995-10-17 Ebara Corporation Turbomachine
JPH0610885A (en) * 1992-04-10 1994-01-21 Ingersoll Rand Co Surge control and recovery of centrifugal compressor
US5466118A (en) * 1993-03-04 1995-11-14 Abb Management Ltd. Centrifugal compressor with a flow-stabilizing casing
EP0754864A1 (en) * 1995-07-18 1997-01-22 Ebara Corporation Turbomachine
US5707206A (en) * 1995-07-18 1998-01-13 Ebara Corporation Turbomachine
US6244817B1 (en) * 1996-12-05 2001-06-12 Mcdonnell Douglas Corporation Method and apparatus for a fan noise controller
JP2009228625A (en) * 2008-03-25 2009-10-08 Mitsubishi Heavy Ind Ltd Casing for axial flow type compressor
DE112012002692B4 (en) 2011-06-29 2022-11-24 OPRA Technologies, B.V. Apparatus and method for reducing air mass flow for low emission combustion over an extended range in single spool gas turbines
JP2013072418A (en) * 2011-09-29 2013-04-22 Mitsubishi Heavy Ind Ltd Compressor
JP2013194687A (en) * 2012-03-22 2013-09-30 Mitsubishi Heavy Ind Ltd Multistage centrifugal compressor
WO2022202412A1 (en) * 2021-03-25 2022-09-29 三菱重工マリンマシナリ株式会社 Compressor casing, supercharger, and method for operating supercharger

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