GB2467715A - Fan stall detection system - Google Patents
Fan stall detection system Download PDFInfo
- Publication number
- GB2467715A GB2467715A GB1010130A GB201010130A GB2467715A GB 2467715 A GB2467715 A GB 2467715A GB 1010130 A GB1010130 A GB 1010130A GB 201010130 A GB201010130 A GB 201010130A GB 2467715 A GB2467715 A GB 2467715A
- Authority
- GB
- United Kingdom
- Prior art keywords
- rotor
- detection system
- generating
- signal
- stall detection
- 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.)
- Granted
Links
- 238000001514 detection method Methods 0.000 title 1
- 230000003068 static effect Effects 0.000 abstract 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
- F01D21/003—Arrangements for testing or measuring
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
- F04D27/001—Testing thereof; Determination or simulation of flow characteristics; Stall or surge detection, e.g. condition monitoring
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
- F04D27/02—Surge control
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/52—Casings; Connections of working fluid for axial pumps
-
- F05B2270/1081—
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2270/00—Control
- F05D2270/01—Purpose of the control system
- F05D2270/10—Purpose of the control system to cope with, or avoid, compressor flow instabilities
- F05D2270/101—Compressor surge or stall
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Control Of Positive-Displacement Air Blowers (AREA)
Abstract
A system for detecting onset of a stall in a rotor is disclosed, the system comprising a sensor located on a static component spaced radially outwardly and apart from tips of a row of blades arranged circumferentially on the rotor wherein the sensor is capable of generating an input signal corresponding to a flow parameter at a location near the tip of a blade, a control system capable of generating a rotor speed signal, and a correlation processor capable of receiving the input signal and the rotor speed signal wherein the correlation processor generates a stability correlation signal.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/966,242 US20100284785A1 (en) | 2007-12-28 | 2007-12-28 | Fan Stall Detection System |
PCT/US2008/088134 WO2009086358A1 (en) | 2007-12-28 | 2008-12-23 | Fan stall detection system |
Publications (3)
Publication Number | Publication Date |
---|---|
GB201010130D0 GB201010130D0 (en) | 2010-07-21 |
GB2467715A true GB2467715A (en) | 2010-08-11 |
GB2467715B GB2467715B (en) | 2012-12-05 |
Family
ID=40383778
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1010130.1A Expired - Fee Related GB2467715B (en) | 2007-12-28 | 2008-12-23 | Fan stall detection system |
Country Status (6)
Country | Link |
---|---|
US (1) | US20100284785A1 (en) |
JP (1) | JP2011508155A (en) |
CA (1) | CA2710009A1 (en) |
DE (1) | DE112008003400T8 (en) |
GB (1) | GB2467715B (en) |
WO (1) | WO2009086358A1 (en) |
Families Citing this family (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8013738B2 (en) | 2007-10-04 | 2011-09-06 | Kd Secure, Llc | Hierarchical storage manager (HSM) for intelligent storage of large volumes of data |
WO2009045218A1 (en) | 2007-10-04 | 2009-04-09 | Donovan John J | A video surveillance, storage, and alerting system having network management, hierarchical data storage, video tip processing, and vehicle plate analysis |
US20100047055A1 (en) * | 2007-12-28 | 2010-02-25 | Aspi Rustom Wadia | Plasma Enhanced Rotor |
US20100290906A1 (en) * | 2007-12-28 | 2010-11-18 | Moeckel Curtis W | Plasma sensor stall control system and turbomachinery diagnostics |
US8282337B2 (en) * | 2007-12-28 | 2012-10-09 | General Electric Company | Instability mitigation system using stator plasma actuators |
US20090169356A1 (en) * | 2007-12-28 | 2009-07-02 | Aspi Rustom Wadia | Plasma Enhanced Compression System |
US8317457B2 (en) * | 2007-12-28 | 2012-11-27 | General Electric Company | Method of operating a compressor |
US20100205928A1 (en) * | 2007-12-28 | 2010-08-19 | Moeckel Curtis W | Rotor stall sensor system |
US20090169363A1 (en) * | 2007-12-28 | 2009-07-02 | Aspi Rustom Wadia | Plasma Enhanced Stator |
US8282336B2 (en) * | 2007-12-28 | 2012-10-09 | General Electric Company | Instability mitigation system |
US8348592B2 (en) * | 2007-12-28 | 2013-01-08 | General Electric Company | Instability mitigation system using rotor plasma actuators |
US20100172747A1 (en) * | 2009-01-08 | 2010-07-08 | General Electric Company | Plasma enhanced compressor duct |
US20100170224A1 (en) * | 2009-01-08 | 2010-07-08 | General Electric Company | Plasma enhanced booster and method of operation |
US8752394B2 (en) * | 2010-03-15 | 2014-06-17 | Rolls-Royce Corporation | Determining fan parameters through pressure monitoring |
WO2011133293A1 (en) * | 2010-04-23 | 2011-10-27 | General Electric Company | Fan stall detection system |
US9885368B2 (en) | 2012-05-24 | 2018-02-06 | Carrier Corporation | Stall margin enhancement of axial fan with rotating shroud |
US9593670B2 (en) | 2014-04-30 | 2017-03-14 | General Electric Company | System and methods for reducing wind turbine noise |
US9658124B2 (en) | 2014-11-05 | 2017-05-23 | General Electric Company | System and method for wind turbine operation |
DE102016118783A1 (en) | 2016-10-04 | 2018-04-05 | Rolls-Royce Deutschland Ltd & Co Kg | Turbofan engine for a civil supersonic aircraft |
DE102016118779A1 (en) * | 2016-10-04 | 2018-04-05 | Rolls-Royce Deutschland Ltd & Co Kg | Turbofan engine for a civil supersonic aircraft |
US11454131B2 (en) * | 2021-01-05 | 2022-09-27 | General Electric Company | Methods and apparatus for real-time clearance assessment using a pressure measurement |
KR102633244B1 (en) * | 2022-09-15 | 2024-02-05 | 한국생산기술연구원 | Stall recognition device and axial flow blower including same |
CN115306754B (en) * | 2022-10-12 | 2023-02-17 | 中国航发四川燃气涡轮研究院 | Axial flow fan aerodynamic instability identification method based on acoustic array |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2191606A (en) * | 1986-04-28 | 1987-12-16 | Rolls Royce Plc | Active control of unsteady motion phenomena in turbomachinery |
WO1994003862A1 (en) * | 1992-08-10 | 1994-02-17 | Dow Deutschland Inc. | Process and device for monitoring and for controlling of a compressor |
US6438484B1 (en) * | 2001-05-23 | 2002-08-20 | General Electric Company | Method and apparatus for detecting and compensating for compressor surge in a gas turbine using remote monitoring and diagnostics |
EP1908927A1 (en) * | 2006-09-27 | 2008-04-09 | General Electric Company | Method and apparatus for an aerodynamic stability management system |
Family Cites Families (37)
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US2594042A (en) * | 1947-05-21 | 1952-04-22 | United Aircraft Corp | Boundary layer energizing means for annular diffusers |
US3300121A (en) * | 1965-02-24 | 1967-01-24 | Gen Motors Corp | Axial-flow compressor |
GB2245316B (en) * | 1990-06-21 | 1993-12-15 | Rolls Royce Plc | Improvements in shroud assemblies for turbine rotors |
JPH07248273A (en) * | 1994-03-11 | 1995-09-26 | Ishikawajima Harima Heavy Ind Co Ltd | Method and apparatus for detecting surging of axial compressor |
US6793455B2 (en) * | 2001-02-08 | 2004-09-21 | Georgia Tech Research Corporation | Method and apparatus for active control of surge in compressors |
GB2374123B (en) * | 2001-04-05 | 2004-09-08 | Rolls Royce Plc | Gas turbine engine system |
JP2002364582A (en) * | 2001-06-11 | 2002-12-18 | Ishikawajima Harima Heavy Ind Co Ltd | Stall predicting method for axial flow compressor |
FR2835019B1 (en) * | 2002-01-22 | 2004-12-31 | Snecma Moteurs | DIFFUSER FOR A LAND OR AERONAUTICAL GAS TURBINE ENGINE |
US6666017B2 (en) * | 2002-05-24 | 2003-12-23 | General Electric Company | Counterrotatable booster compressor assembly for a gas turbine engine |
US20040011917A1 (en) * | 2002-07-18 | 2004-01-22 | Saeks Richard E. | Shock wave modification via shock induced ion doping |
US6871487B2 (en) * | 2003-02-14 | 2005-03-29 | Kulite Semiconductor Products, Inc. | System for detecting and compensating for aerodynamic instabilities in turbo-jet engines |
US7334394B2 (en) * | 2003-09-02 | 2008-02-26 | The Ohio State University | Localized arc filament plasma actuators for noise mitigation and mixing enhancement |
US7275013B1 (en) * | 2004-09-20 | 2007-09-25 | University Of Notre Dame Duloc | Plasma anemometer and method for using same |
US7159401B1 (en) * | 2004-12-23 | 2007-01-09 | Kulite Semiconductor Products, Inc. | System for detecting and compensating for aerodynamic instabilities in turbo-jet engines |
CN101438432B (en) * | 2006-04-28 | 2011-11-02 | 江森自控帅福得先进能源动力系统有限责任公司 | Battery module assembly |
JP4890095B2 (en) * | 2006-05-19 | 2012-03-07 | 株式会社Ihi | Stall sign detection device and method, and engine control system |
US7819626B2 (en) * | 2006-10-13 | 2010-10-26 | General Electric Company | Plasma blade tip clearance control |
US7766599B2 (en) * | 2006-10-31 | 2010-08-03 | General Electric Company | Plasma lifted boundary layer gas turbine engine vane |
US7870720B2 (en) * | 2006-11-29 | 2011-01-18 | Lockheed Martin Corporation | Inlet electromagnetic flow control |
US7588413B2 (en) * | 2006-11-30 | 2009-09-15 | General Electric Company | Upstream plasma shielded film cooling |
US7695241B2 (en) * | 2006-11-30 | 2010-04-13 | General Electric Company | Downstream plasma shielded film cooling |
US7736123B2 (en) * | 2006-12-15 | 2010-06-15 | General Electric Company | Plasma induced virtual turbine airfoil trailing edge extension |
US7628585B2 (en) * | 2006-12-15 | 2009-12-08 | General Electric Company | Airfoil leading edge end wall vortex reducing plasma |
US20090065064A1 (en) * | 2007-08-02 | 2009-03-12 | The University Of Notre Dame Du Lac | Compressor tip gap flow control using plasma actuators |
US8317457B2 (en) * | 2007-12-28 | 2012-11-27 | General Electric Company | Method of operating a compressor |
US8282336B2 (en) * | 2007-12-28 | 2012-10-09 | General Electric Company | Instability mitigation system |
US20100047060A1 (en) * | 2007-12-28 | 2010-02-25 | Aspi Rustom Wadia | Plasma Enhanced Compressor |
US20100284795A1 (en) * | 2007-12-28 | 2010-11-11 | General Electric Company | Plasma Clearance Controlled Compressor |
US8348592B2 (en) * | 2007-12-28 | 2013-01-08 | General Electric Company | Instability mitigation system using rotor plasma actuators |
US20090169363A1 (en) * | 2007-12-28 | 2009-07-02 | Aspi Rustom Wadia | Plasma Enhanced Stator |
US8282337B2 (en) * | 2007-12-28 | 2012-10-09 | General Electric Company | Instability mitigation system using stator plasma actuators |
US20090169356A1 (en) * | 2007-12-28 | 2009-07-02 | Aspi Rustom Wadia | Plasma Enhanced Compression System |
US20100047055A1 (en) * | 2007-12-28 | 2010-02-25 | Aspi Rustom Wadia | Plasma Enhanced Rotor |
US8006497B2 (en) * | 2008-05-30 | 2011-08-30 | Honeywell International Inc. | Diffusers, diffusion systems, and methods for controlling airflow through diffusion systems |
US7984614B2 (en) * | 2008-11-17 | 2011-07-26 | Honeywell International Inc. | Plasma flow controlled diffuser system |
US20100172747A1 (en) * | 2009-01-08 | 2010-07-08 | General Electric Company | Plasma enhanced compressor duct |
US20100170224A1 (en) * | 2009-01-08 | 2010-07-08 | General Electric Company | Plasma enhanced booster and method of operation |
-
2007
- 2007-12-28 US US11/966,242 patent/US20100284785A1/en not_active Abandoned
-
2008
- 2008-12-23 WO PCT/US2008/088134 patent/WO2009086358A1/en active Application Filing
- 2008-12-23 JP JP2010540859A patent/JP2011508155A/en active Pending
- 2008-12-23 DE DE112008003400T patent/DE112008003400T8/en not_active Expired - Fee Related
- 2008-12-23 CA CA2710009A patent/CA2710009A1/en not_active Abandoned
- 2008-12-23 GB GB1010130.1A patent/GB2467715B/en not_active Expired - Fee Related
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2191606A (en) * | 1986-04-28 | 1987-12-16 | Rolls Royce Plc | Active control of unsteady motion phenomena in turbomachinery |
WO1994003862A1 (en) * | 1992-08-10 | 1994-02-17 | Dow Deutschland Inc. | Process and device for monitoring and for controlling of a compressor |
US6438484B1 (en) * | 2001-05-23 | 2002-08-20 | General Electric Company | Method and apparatus for detecting and compensating for compressor surge in a gas turbine using remote monitoring and diagnostics |
EP1908927A1 (en) * | 2006-09-27 | 2008-04-09 | General Electric Company | Method and apparatus for an aerodynamic stability management system |
Also Published As
Publication number | Publication date |
---|---|
GB201010130D0 (en) | 2010-07-21 |
DE112008003400T5 (en) | 2010-11-11 |
WO2009086358A1 (en) | 2009-07-09 |
JP2011508155A (en) | 2011-03-10 |
US20100284785A1 (en) | 2010-11-11 |
CA2710009A1 (en) | 2009-07-09 |
GB2467715B (en) | 2012-12-05 |
DE112008003400T8 (en) | 2011-02-24 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 20131223 |