NO20021110L - Virvelopplösende system for en sentrifugalkompressor - Google Patents
Virvelopplösende system for en sentrifugalkompressorInfo
- Publication number
- NO20021110L NO20021110L NO20021110A NO20021110A NO20021110L NO 20021110 L NO20021110 L NO 20021110L NO 20021110 A NO20021110 A NO 20021110A NO 20021110 A NO20021110 A NO 20021110A NO 20021110 L NO20021110 L NO 20021110L
- Authority
- NO
- Norway
- Prior art keywords
- swirl
- centrifugal compressor
- dissolving system
- dissolving
- centrifugal
- Prior art date
Links
Classifications
-
- 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
- F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
- F04D29/44—Fluid-guiding means, e.g. diffusers
-
- 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
- F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
- F04D29/44—Fluid-guiding means, e.g. diffusers
- F04D29/441—Fluid-guiding means, e.g. diffusers especially adapted for elastic fluid pumps
- F04D29/444—Bladed diffusers
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/390,876 US6279322B1 (en) | 1999-09-07 | 1999-09-07 | Deswirler system for centrifugal compressor |
PCT/US2000/021941 WO2001018404A1 (en) | 1999-09-07 | 2000-08-10 | Deswirler system for centrifugal compressor |
Publications (2)
Publication Number | Publication Date |
---|---|
NO20021110D0 NO20021110D0 (no) | 2002-03-06 |
NO20021110L true NO20021110L (no) | 2002-05-06 |
Family
ID=23544313
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
NO20021110A NO20021110L (no) | 1999-09-07 | 2002-03-06 | Virvelopplösende system for en sentrifugalkompressor |
Country Status (14)
Country | Link |
---|---|
US (1) | US6279322B1 (xx) |
EP (1) | EP1214522B1 (xx) |
JP (1) | JP4679017B2 (xx) |
KR (1) | KR100767886B1 (xx) |
CN (1) | CN1214191C (xx) |
AU (1) | AU759980B2 (xx) |
CA (1) | CA2384017C (xx) |
DE (1) | DE60016937T2 (xx) |
HK (1) | HK1051715A1 (xx) |
IL (1) | IL148394A0 (xx) |
MX (1) | MXPA02002479A (xx) |
NO (1) | NO20021110L (xx) |
TR (1) | TR200200584T2 (xx) |
WO (1) | WO2001018404A1 (xx) |
Families Citing this family (54)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7025566B2 (en) * | 2003-11-04 | 2006-04-11 | Pratt & Whitney Canada Corp. | Hybrid vane island diffuser |
US7506511B2 (en) * | 2003-12-23 | 2009-03-24 | Honeywell International Inc. | Reduced exhaust emissions gas turbine engine combustor |
US7442006B2 (en) * | 2005-08-15 | 2008-10-28 | Honeywell International Inc. | Integral diffuser and deswirler with continuous flow path deflected at assembly |
US7500364B2 (en) | 2005-11-22 | 2009-03-10 | Honeywell International Inc. | System for coupling flow from a centrifugal compressor to an axial combustor for gas turbines |
US7870739B2 (en) * | 2006-02-02 | 2011-01-18 | Siemens Energy, Inc. | Gas turbine engine curved diffuser with partial impingement cooling apparatus for transitions |
US20070183890A1 (en) * | 2006-02-09 | 2007-08-09 | Honeywell International, Inc. | Leaned deswirl vanes behind a centrifugal compressor in a gas turbine engine |
US7600370B2 (en) | 2006-05-25 | 2009-10-13 | Siemens Energy, Inc. | Fluid flow distributor apparatus for gas turbine engine mid-frame section |
US7717672B2 (en) * | 2006-08-29 | 2010-05-18 | Honeywell International Inc. | Radial vaned diffusion system with integral service routings |
FR2920033B1 (fr) * | 2007-08-13 | 2014-08-22 | Snecma | Turbomachine avec diffuseur |
FR2920032B1 (fr) * | 2007-08-13 | 2014-08-22 | Snecma | Diffuseur d'une turbomachine |
FR2922939B1 (fr) * | 2007-10-26 | 2014-04-25 | Snecma | Turbomachine comprenant un diffuseur |
US7856834B2 (en) * | 2008-02-20 | 2010-12-28 | Trane International Inc. | Centrifugal compressor assembly and method |
US9353765B2 (en) | 2008-02-20 | 2016-05-31 | Trane International Inc. | Centrifugal compressor assembly and method |
US8037713B2 (en) | 2008-02-20 | 2011-10-18 | Trane International, Inc. | Centrifugal compressor assembly and method |
US7975506B2 (en) | 2008-02-20 | 2011-07-12 | Trane International, Inc. | Coaxial economizer assembly and method |
FR2927951B1 (fr) * | 2008-02-27 | 2011-08-19 | Snecma | Ensemble diffuseur-redresseur pour une turbomachine |
US8272832B2 (en) | 2008-04-17 | 2012-09-25 | Honeywell International Inc. | Centrifugal compressor with surge control, and associated method |
FR2931515B1 (fr) * | 2008-05-22 | 2014-07-18 | Snecma | Turbomachine avec diffuseur |
US8438854B2 (en) * | 2008-05-23 | 2013-05-14 | Honeywell International Inc. | Pre-diffuser for centrifugal compressor |
US8113002B2 (en) * | 2008-10-17 | 2012-02-14 | General Electric Company | Combustor burner vanelets |
FR2941742B1 (fr) * | 2009-02-05 | 2011-08-19 | Snecma | Ensemble diffuseur-redresseur pour une turbomachine |
FR2955364B1 (fr) * | 2010-01-19 | 2012-11-16 | Snecma | Liaison diffuseur-redresseur pour un compresseur centrifuge |
DE102010023816A1 (de) | 2010-06-15 | 2011-12-15 | Rolls-Royce Deutschland Ltd & Co Kg | Gasturbinenbrennkammeranordnung |
FR2961867B1 (fr) | 2010-06-24 | 2014-06-13 | Snecma | Prelevement d'air a travers le diffuseur d'un compresseur centrifuge d'une turbomachine |
US9347328B2 (en) * | 2010-08-09 | 2016-05-24 | Siemens Energy, Inc. | Compressed air plenum for a gas turbine engine |
DE102011108887A1 (de) * | 2011-07-28 | 2013-01-31 | Rolls-Royce Deutschland Ltd & Co Kg | Gasturbinenzentripetalringbrennkammer sowie Verfahren zur Strömungsführung |
US20140338360A1 (en) * | 2012-09-21 | 2014-11-20 | United Technologies Corporation | Bleed port ribs for turbomachine case |
WO2014137430A1 (en) | 2013-03-08 | 2014-09-12 | Rolls-Royce North American Technologies, Inc. | Gas turbine engine centrifugal compressor with seal between two diffuser parts |
US9726185B2 (en) | 2013-05-14 | 2017-08-08 | Honeywell International Inc. | Centrifugal compressor with casing treatment for surge control |
US9134029B2 (en) | 2013-09-12 | 2015-09-15 | Siemens Energy, Inc. | Radial midframe baffle for can-annular combustor arrangement having tangentially oriented combustor cans |
US9528706B2 (en) | 2013-12-13 | 2016-12-27 | Siemens Energy, Inc. | Swirling midframe flow for gas turbine engine having advanced transitions |
US10557358B2 (en) * | 2015-02-06 | 2020-02-11 | United Technologies Corporation | Gas turbine engine containment structures |
DE102015219556A1 (de) * | 2015-10-08 | 2017-04-13 | Rolls-Royce Deutschland Ltd & Co Kg | Diffusor für Radialverdichter, Radialverdichter und Turbomaschine mit Radialverdichter |
DE102015220333A1 (de) | 2015-10-19 | 2017-04-20 | Rolls-Royce Deutschland Ltd & Co Kg | Vorrichtung zur Einstellung eines Spaltes zwischen dem Gehäuse eines Laufrades und dem Laufrad in einem Radialverdichter und eine Turbomaschine |
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 |
US10087839B2 (en) | 2016-02-24 | 2018-10-02 | Pratt & Whitney Canada Corp. | Air intake for turboprop engine |
US10030581B2 (en) | 2016-02-24 | 2018-07-24 | Pratt & Whitney Canada Corp. | Air intake with scroll portion and strutted portion for gas turbine engine |
US10544693B2 (en) * | 2016-06-15 | 2020-01-28 | Honeywell International Inc. | Service routing configuration for a gas turbine engine diffuser system |
US10898627B2 (en) * | 2017-01-12 | 2021-01-26 | California Cardiac Solutions, Inc. | Ventricular assist device |
US10519868B2 (en) | 2017-02-14 | 2019-12-31 | Honeywell International Inc. | System and method for cleaning cooling passages of a combustion chamber |
US10718222B2 (en) | 2017-03-27 | 2020-07-21 | General Electric Company | Diffuser-deswirler for a gas turbine engine |
US11536456B2 (en) | 2017-10-24 | 2022-12-27 | General Electric Company | Fuel and air injection handling system for a combustor of a rotating detonation engine |
KR102000258B1 (ko) * | 2018-12-20 | 2019-07-15 | 한국건설기술연구원 | 2단 원심형 블로워 |
US10989219B2 (en) | 2019-02-04 | 2021-04-27 | Honeywell International Inc. | Diffuser assemblies for compression systems |
US11098730B2 (en) * | 2019-04-12 | 2021-08-24 | Rolls-Royce Corporation | Deswirler assembly for a centrifugal compressor |
US11970279B2 (en) | 2020-02-21 | 2024-04-30 | General Electric Company | Control system and methods of controlling an engine-mounting link system |
US11939070B2 (en) | 2020-02-21 | 2024-03-26 | General Electric Company | Engine-mounting links that have an adjustable inclination angle |
CN111894760B (zh) * | 2020-07-13 | 2022-11-15 | 潍坊联信增压器股份有限公司 | 一种消除尾部旋转涡流的涡喷发动机 |
US11286952B2 (en) | 2020-07-14 | 2022-03-29 | Rolls-Royce Corporation | Diffusion system configured for use with centrifugal compressor |
US11441516B2 (en) | 2020-07-14 | 2022-09-13 | Rolls-Royce North American Technologies Inc. | Centrifugal compressor assembly for a gas turbine engine with deswirler having sealing features |
US11578654B2 (en) | 2020-07-29 | 2023-02-14 | Rolls-Royce North American Technologies Inc. | Centrifical compressor assembly for a gas turbine engine |
CN114593089A (zh) * | 2022-01-26 | 2022-06-07 | 北京盈天航空动力科技有限公司 | 一种微小型涡喷发动机v型子午流道扩压器 |
CN114635876B (zh) * | 2022-05-23 | 2022-09-20 | 宁波威孚天力增压技术股份有限公司 | 一种带有引气机构的离心式压气机及涡轮增压器 |
Family Cites Families (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2681760A (en) | 1949-02-26 | 1954-06-22 | Curtiss Wright Corp | Centrifugal compressor |
GB884507A (en) | 1960-06-02 | 1961-12-13 | Neu Sa | Improvements in or relating to centrifugal compressors |
US3333762A (en) | 1966-11-16 | 1967-08-01 | United Aircraft Canada | Diffuser for centrifugal compressor |
US3719430A (en) * | 1971-08-24 | 1973-03-06 | Gen Electric | Diffuser |
US3861826A (en) | 1972-08-14 | 1975-01-21 | Caterpillar Tractor Co | Cascade diffuser having thin, straight vanes |
US4027997A (en) * | 1975-12-10 | 1977-06-07 | General Electric Company | Diffuser for a centrifugal compressor |
US4100732A (en) * | 1976-12-02 | 1978-07-18 | General Electric Company | Centrifugal compressor advanced dump diffuser |
SE8601577L (sv) | 1985-04-29 | 1986-10-30 | Teledyne Ind | Diffusorsystem foe en centrifugalkompressor och forfarande for tillverkning av densamma |
US5011371A (en) | 1987-04-29 | 1991-04-30 | General Motors Corporation | Centrifugal compressor/pump with fluid dynamically variable geometry diffuser |
US5101620A (en) * | 1988-12-28 | 1992-04-07 | Sundstrand Corporation | Annular combustor for a turbine engine without film cooling |
US5062262A (en) * | 1988-12-28 | 1991-11-05 | Sundstrand Corporation | Cooling of turbine nozzles |
US4981018A (en) * | 1989-05-18 | 1991-01-01 | Sundstrand Corporation | Compressor shroud air bleed passages |
US4979361A (en) | 1989-07-13 | 1990-12-25 | United Technologies Corporation | Stepped diffuser |
US5129224A (en) * | 1989-12-08 | 1992-07-14 | Sundstrand Corporation | Cooling of turbine nozzle containment ring |
US5303543A (en) * | 1990-02-08 | 1994-04-19 | Sundstrand Corporation | Annular combustor for a turbine engine with tangential passages sized to provide only combustion air |
JP3010806B2 (ja) * | 1991-07-02 | 2000-02-21 | ソニー株式会社 | 液晶プロジェクタ装置 |
US5335501A (en) | 1992-11-16 | 1994-08-09 | General Electric Company | Flow spreading diffuser |
JP3110205B2 (ja) | 1993-04-28 | 2000-11-20 | 株式会社日立製作所 | 遠心圧縮機及び羽根付ディフューザ |
US5680767A (en) | 1995-09-11 | 1997-10-28 | General Electric Company | Regenerative combustor cooling in a gas turbine engine |
-
1999
- 1999-09-07 US US09/390,876 patent/US6279322B1/en not_active Expired - Lifetime
-
2000
- 2000-08-10 KR KR1020027002962A patent/KR100767886B1/ko not_active IP Right Cessation
- 2000-08-10 EP EP00955443A patent/EP1214522B1/en not_active Expired - Lifetime
- 2000-08-10 TR TR2002/00584T patent/TR200200584T2/xx unknown
- 2000-08-10 IL IL14839400A patent/IL148394A0/xx not_active IP Right Cessation
- 2000-08-10 CN CNB008149496A patent/CN1214191C/zh not_active Expired - Fee Related
- 2000-08-10 AU AU67651/00A patent/AU759980B2/en not_active Ceased
- 2000-08-10 CA CA002384017A patent/CA2384017C/en not_active Expired - Fee Related
- 2000-08-10 WO PCT/US2000/021941 patent/WO2001018404A1/en active IP Right Grant
- 2000-08-10 MX MXPA02002479A patent/MXPA02002479A/es active IP Right Grant
- 2000-08-10 DE DE60016937T patent/DE60016937T2/de not_active Expired - Lifetime
- 2000-08-10 JP JP2001521908A patent/JP4679017B2/ja not_active Expired - Fee Related
-
2002
- 2002-03-06 NO NO20021110A patent/NO20021110L/no not_active Application Discontinuation
-
2003
- 2003-06-03 HK HK03103937A patent/HK1051715A1/xx not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
HK1051715A1 (en) | 2003-08-15 |
KR20020039343A (ko) | 2002-05-25 |
AU759980B2 (en) | 2003-05-01 |
JP4679017B2 (ja) | 2011-04-27 |
TR200200584T2 (tr) | 2002-07-22 |
CA2384017C (en) | 2008-11-18 |
DE60016937D1 (de) | 2005-01-27 |
IL148394A0 (en) | 2002-09-12 |
WO2001018404A1 (en) | 2001-03-15 |
EP1214522A1 (en) | 2002-06-19 |
CN1384902A (zh) | 2002-12-11 |
EP1214522B1 (en) | 2004-12-22 |
MXPA02002479A (es) | 2002-08-28 |
JP2003508690A (ja) | 2003-03-04 |
AU6765100A (en) | 2001-04-10 |
CA2384017A1 (en) | 2001-03-15 |
US6279322B1 (en) | 2001-08-28 |
DE60016937T2 (de) | 2005-12-15 |
CN1214191C (zh) | 2005-08-10 |
NO20021110D0 (no) | 2002-03-06 |
KR100767886B1 (ko) | 2007-10-17 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FC2A | Withdrawal, rejection or dismissal of laid open patent application |