JPS569696A - Cetrifugal compressor - Google Patents

Cetrifugal compressor

Info

Publication number
JPS569696A
JPS569696A JP8494379A JP8494379A JPS569696A JP S569696 A JPS569696 A JP S569696A JP 8494379 A JP8494379 A JP 8494379A JP 8494379 A JP8494379 A JP 8494379A JP S569696 A JPS569696 A JP S569696A
Authority
JP
Japan
Prior art keywords
flow passage
flow
impeller
decelerating
compressor
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
JP8494379A
Other languages
Japanese (ja)
Inventor
Koji Nakagawa
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 JP8494379A priority Critical patent/JPS569696A/en
Publication of JPS569696A publication Critical patent/JPS569696A/en
Pending legal-status Critical Current

Links

Landscapes

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

Abstract

PURPOSE: To facilitate stable drives of a compressor in controls of supplied gas amount by ejecting fluid out of an ejecting port installed on the wall surface of a decelerating flow passage so as to hydrodynamically decrease substantial flow passage sectional area directly after the outlet port of an impeller.
CONSTITUTION: When a return control valve 15 has been opened, part of gas to flow through a discharge flow passage 3 is ejected through an ejecting port 12 to a decelerating flow passage 10 as shown by an arrow 18. As a result, part to stream a flux 17 to flow out of an impeller 9 in the decelerating flow passage 10 decreases, and flow rate of gas to pass through the impeller 9 decreases. And, since gas capacity delivered through a supply flow passage 6 is equal to the flow rate to pass through the impeller 9, supplied gas capacity through the supply flow passage 6 is controllable by the opening degree of the return flow control valve 15. Thus, a control of supplied gas capacity enables the compressor to stably drive enlarging the passing flow rate through the decelerating flow passage 10 without occurrence of surging.
COPYRIGHT: (C)1981,JPO&Japio
JP8494379A 1979-07-06 1979-07-06 Cetrifugal compressor Pending JPS569696A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP8494379A JPS569696A (en) 1979-07-06 1979-07-06 Cetrifugal compressor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP8494379A JPS569696A (en) 1979-07-06 1979-07-06 Cetrifugal compressor

Publications (1)

Publication Number Publication Date
JPS569696A true JPS569696A (en) 1981-01-31

Family

ID=13844726

Family Applications (1)

Application Number Title Priority Date Filing Date
JP8494379A Pending JPS569696A (en) 1979-07-06 1979-07-06 Cetrifugal compressor

Country Status (1)

Country Link
JP (1) JPS569696A (en)

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH1061586A (en) * 1996-06-07 1998-03-03 Carrier Corp Centrifugal compressor and method for controlling centrifugal compressor
US7326027B1 (en) * 2004-05-25 2008-02-05 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Devices and methods of operation thereof for providing stable flow for centrifugal compressors
JP2008045783A (en) * 2006-08-11 2008-02-28 National Institutes Of Natural Sciences Continuous burning furnace and continuous burning method
JP2008045789A (en) * 2006-08-11 2008-02-28 Mino Ceramic Co Ltd Continuous burning apparatus
EP2635772A1 (en) * 2010-11-03 2013-09-11 Danfoss Turbocor Compressors BV. Centrifugal compressor with fluid injector diffuser
JP2014513778A (en) * 2011-05-16 2014-06-05 ターボメカ Gas turbine diffuser blowing method and corresponding diffuser
EP2905477A1 (en) * 2014-02-10 2015-08-12 Pratt & Whitney Canada Corp. Centrifugal compressor diffuser and method for controlling same
KR20160124143A (en) * 2014-02-20 2016-10-26 댄포스 아/에스 Control system and method for centrifugal compressor
US9926942B2 (en) 2015-10-27 2018-03-27 Pratt & Whitney Canada Corp. Diffuser pipe with vortex generators
CN108431522A (en) * 2016-01-12 2018-08-21 大金应用美国股份有限公司 The centrifugal compressor of carrying liqs injection
US10570925B2 (en) 2015-10-27 2020-02-25 Pratt & Whitney Canada Corp. Diffuser pipe with splitter vane
US11378005B1 (en) 2020-12-17 2022-07-05 Pratt & Whitney Canada Corp. Compressor diffuser and diffuser pipes therefor
WO2024037886A1 (en) * 2022-08-17 2024-02-22 Rolls-Royce Solutions GmbH Compressor housing, radial compressor with a compressor housing of this type, radial compressor arrangement, exhaust gas turbocharger and internal combustion engine

Cited By (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH1061586A (en) * 1996-06-07 1998-03-03 Carrier Corp Centrifugal compressor and method for controlling centrifugal compressor
US7326027B1 (en) * 2004-05-25 2008-02-05 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Devices and methods of operation thereof for providing stable flow for centrifugal compressors
JP2008045783A (en) * 2006-08-11 2008-02-28 National Institutes Of Natural Sciences Continuous burning furnace and continuous burning method
JP2008045789A (en) * 2006-08-11 2008-02-28 Mino Ceramic Co Ltd Continuous burning apparatus
EP2635772A1 (en) * 2010-11-03 2013-09-11 Danfoss Turbocor Compressors BV. Centrifugal compressor with fluid injector diffuser
US10197064B2 (en) 2010-11-03 2019-02-05 Danfoss A/S Centrifugal compressor with fluid injector diffuser
EP2635772A4 (en) * 2010-11-03 2014-12-03 Danfoss Turbocor Compressors Bv Centrifugal compressor with fluid injector diffuser
US9618008B2 (en) 2011-05-16 2017-04-11 Turbomeca Gas turbine diffuser blowing method and corresponding diffuser
JP2014513778A (en) * 2011-05-16 2014-06-05 ターボメカ Gas turbine diffuser blowing method and corresponding diffuser
US9803652B2 (en) 2014-02-10 2017-10-31 Pratt & Whitney Canada Corp. Centrifugal compressor diffuser and method for controlling same
EP2905477A1 (en) * 2014-02-10 2015-08-12 Pratt & Whitney Canada Corp. Centrifugal compressor diffuser and method for controlling same
KR20160124143A (en) * 2014-02-20 2016-10-26 댄포스 아/에스 Control system and method for centrifugal compressor
JP2017506307A (en) * 2014-02-20 2017-03-02 ダンフォス・エイ／エス Control system and method for a centrifugal compressor
US10557473B2 (en) 2014-02-20 2020-02-11 Danfoss A/S Control system and method for centrifugal compressor
US10570925B2 (en) 2015-10-27 2020-02-25 Pratt & Whitney Canada Corp. Diffuser pipe with splitter vane
US9926942B2 (en) 2015-10-27 2018-03-27 Pratt & Whitney Canada Corp. Diffuser pipe with vortex generators
US10502231B2 (en) 2015-10-27 2019-12-10 Pratt & Whitney Canada Corp. Diffuser pipe with vortex generators
US11215196B2 (en) 2015-10-27 2022-01-04 Pratt & Whitney Canada Corp. Diffuser pipe with splitter vane
CN108431522A (en) * 2016-01-12 2018-08-21 大金应用美国股份有限公司 The centrifugal compressor of carrying liqs injection
CN108431522B (en) * 2016-01-12 2020-11-27 大金应用美国股份有限公司 Centrifugal compressor with liquid injection
US10563673B2 (en) 2016-01-12 2020-02-18 Daikin Applied Americas Inc. Centrifugal compressor with liquid injection
US11378005B1 (en) 2020-12-17 2022-07-05 Pratt & Whitney Canada Corp. Compressor diffuser and diffuser pipes therefor
WO2024037886A1 (en) * 2022-08-17 2024-02-22 Rolls-Royce Solutions GmbH Compressor housing, radial compressor with a compressor housing of this type, radial compressor arrangement, exhaust gas turbocharger and internal combustion engine

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