CN1464179A - Process and apparatus for expanding multi-stage axial flow gas compressor stable operation zone - Google Patents
Process and apparatus for expanding multi-stage axial flow gas compressor stable operation zone Download PDFInfo
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- CN1464179A CN1464179A CN 02123219 CN02123219A CN1464179A CN 1464179 A CN1464179 A CN 1464179A CN 02123219 CN02123219 CN 02123219 CN 02123219 A CN02123219 A CN 02123219A CN 1464179 A CN1464179 A CN 1464179A
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CN 02123219 CN1291161C (en) | 2002-06-13 | 2002-06-13 | Process and apparatus for expanding multi-stage axial flow gas compressor stable operation zone |
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CN 02123219 CN1291161C (en) | 2002-06-13 | 2002-06-13 | Process and apparatus for expanding multi-stage axial flow gas compressor stable operation zone |
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CN1464179A true CN1464179A (en) | 2003-12-31 |
CN1291161C CN1291161C (en) | 2006-12-20 |
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Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN100451900C (en) * | 2004-06-10 | 2009-01-14 | 上海施耐德日盛压缩机有限公司 | Intelligent control method for air compressor |
CN102022351A (en) * | 2010-12-08 | 2011-04-20 | 北京航空航天大学 | Method for widening stable working range of high-load axial flow gas compressor |
CN102536866A (en) * | 2010-12-01 | 2012-07-04 | 通用电气公司 | Surge precursor protection systems and methods |
CN102900564A (en) * | 2011-07-25 | 2013-01-30 | 中国科学院工程热物理研究所 | Blade top air injection stability controller for axial flow compression system |
CN106640722A (en) * | 2017-01-24 | 2017-05-10 | 中国科学院工程热物理研究所 | Gas compressor aerodynamic stability diagnosis and control device and method |
CN108387378A (en) * | 2018-01-22 | 2018-08-10 | 西安航天动力试验技术研究所 | A kind of engine test Propellant Supply low frequency pulsating suppressing method and system |
CN110608187A (en) * | 2019-10-30 | 2019-12-24 | 江西理工大学 | Axial flow compressor stall surge prediction device based on frequency characteristic change |
CN116771709A (en) * | 2023-08-03 | 2023-09-19 | 哈尔滨工程大学 | Dynamic stall test system of five-stage axial flow compressor |
-
2002
- 2002-06-13 CN CN 02123219 patent/CN1291161C/en not_active Expired - Lifetime
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN100451900C (en) * | 2004-06-10 | 2009-01-14 | 上海施耐德日盛压缩机有限公司 | Intelligent control method for air compressor |
CN102536866B (en) * | 2010-12-01 | 2015-11-25 | 通用电气公司 | The method of compressor assembly and supervision compressor assembly |
CN102536866A (en) * | 2010-12-01 | 2012-07-04 | 通用电气公司 | Surge precursor protection systems and methods |
CN102022351B (en) * | 2010-12-08 | 2012-06-27 | 北京航空航天大学 | Method for widening stable working range of high-load axial flow gas compressor |
CN102022351A (en) * | 2010-12-08 | 2011-04-20 | 北京航空航天大学 | Method for widening stable working range of high-load axial flow gas compressor |
CN102900564A (en) * | 2011-07-25 | 2013-01-30 | 中国科学院工程热物理研究所 | Blade top air injection stability controller for axial flow compression system |
CN102900564B (en) * | 2011-07-25 | 2015-01-07 | 中国科学院工程热物理研究所 | Blade top air injection stability controller for axial flow compression system |
CN106640722A (en) * | 2017-01-24 | 2017-05-10 | 中国科学院工程热物理研究所 | Gas compressor aerodynamic stability diagnosis and control device and method |
WO2018137394A1 (en) * | 2017-01-24 | 2018-08-02 | 中国科学院工程热物理研究所 | Apparatus and method for diagnosing and controlling aerodynamic stability of compressor |
CN106640722B (en) * | 2017-01-24 | 2019-03-01 | 中国科学院工程热物理研究所 | A kind of device and method of pneumatic stability of gas compressor diagnosis and control |
US11536285B2 (en) | 2017-01-24 | 2022-12-27 | Institute Of Engineering Thermophysics, Chinese Academy Of Sciences | Apparatus and method for diagnosing and controlling aerodynamic stability of compressor |
CN108387378A (en) * | 2018-01-22 | 2018-08-10 | 西安航天动力试验技术研究所 | A kind of engine test Propellant Supply low frequency pulsating suppressing method and system |
CN110608187A (en) * | 2019-10-30 | 2019-12-24 | 江西理工大学 | Axial flow compressor stall surge prediction device based on frequency characteristic change |
CN116771709A (en) * | 2023-08-03 | 2023-09-19 | 哈尔滨工程大学 | Dynamic stall test system of five-stage axial flow compressor |
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CN1291161C (en) | 2006-12-20 |
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Assignee: Yancon Cathay Coal Chemicals Co., Ltd. Assignor: Institute of Engineering Thermophysics, Chinese Academy of Sciences Contract fulfillment period: 2008.8.15 to 2013.8.14 Contract record no.: 2008370000068 Denomination of invention: Process and apparatus for expanding multi-stage axial flow gas compressor stable operation zone Granted publication date: 20061220 License type: Exclusive license Record date: 20081024 |
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Free format text: EXCLUSIVE LICENSE; TIME LIMIT OF IMPLEMENTING CONTACT: 2008.8.15 TO 2013.8.14; CHANGE OF CONTRACT Name of requester: YANKUANGGUOTAI CHEMICAL CO., LTD. Effective date: 20081024 |
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Effective date of registration: 20201204 Address after: No.56, Huanghai Avenue, Lianyungang Economic and Technological Development Zone, Lianyungang City, Jiangsu Province 222000 Patentee after: JIANGSU CHINESE ACADEMY OF SCIENCES ENERGY POWER RESEARCH CENTER Patentee after: Institute of Engineering Thermophysics, Chinese Academy of Sciences Address before: 100080 No. 12, Zhongguancun Road, Beijing, Haidian District Patentee before: Institute of Engineering Thermophysics, Chinese Academy of Sciences |
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Granted publication date: 20061220 |
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