TR200200584T2 - Santrifüj kompresörü için anafor önleme sistemi - Google Patents
Santrifüj kompresörü için anafor önleme sistemiInfo
- Publication number
- TR200200584T2 TR200200584T2 TR2002/00584T TR200200584T TR200200584T2 TR 200200584 T2 TR200200584 T2 TR 200200584T2 TR 2002/00584 T TR2002/00584 T TR 2002/00584T TR 200200584 T TR200200584 T TR 200200584T TR 200200584 T2 TR200200584 T2 TR 200200584T2
- Authority
- TR
- Turkey
- Prior art keywords
- vortex
- centrifugal compressor
- vortex system
- curved passage
- outlet
- 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)
Abstract
Bir gaz türbin motorununbir santrifüj kompresörü için olan bir anafor önleme sistemi sürtünme kuvvetlerini önlemli ölçüde azaltarak genel motor performansini arttirir. Anafor öleme sistemi genel olarak bir dagiticindan (116) radyal olarak disari dogru akan gazi almak üzere düzenlenen bir girise, eksenin devami dogrultusunda gaz çikisi için düzenlenen bir çikisa ve bunlarin arasinda kavisli bir geçise (124) sahip ollan bir dairesel sekilli manifold (122) içerir. Anafor önleme sistemi ayrica, direkt olarak kavisli geçisin (124) içinde yer alan ve dagiticiya (116) birlesik olan bir çok anafor önleyici kanat (126,136,142,150)içerir.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/390,876 US6279322B1 (en) | 1999-09-07 | 1999-09-07 | Deswirler system for centrifugal compressor |
Publications (1)
Publication Number | Publication Date |
---|---|
TR200200584T2 true TR200200584T2 (tr) | 2002-07-22 |
Family
ID=23544313
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
TR2002/00584T TR200200584T2 (tr) | 1999-09-07 | 2000-08-10 | Santrifüj kompresörü için anafor önleme sistemi |
Country Status (14)
Country | Link |
---|---|
US (1) | US6279322B1 (tr) |
EP (1) | EP1214522B1 (tr) |
JP (1) | JP4679017B2 (tr) |
KR (1) | KR100767886B1 (tr) |
CN (1) | CN1214191C (tr) |
AU (1) | AU759980B2 (tr) |
CA (1) | CA2384017C (tr) |
DE (1) | DE60016937T2 (tr) |
HK (1) | HK1051715A1 (tr) |
IL (1) | IL148394A0 (tr) |
MX (1) | MXPA02002479A (tr) |
NO (1) | NO20021110L (tr) |
TR (1) | TR200200584T2 (tr) |
WO (1) | WO2001018404A1 (tr) |
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 |
FR2920032B1 (fr) * | 2007-08-13 | 2014-08-22 | Snecma | Diffuseur d'une turbomachine |
FR2920033B1 (fr) * | 2007-08-13 | 2014-08-22 | Snecma | Turbomachine avec diffuseur |
FR2922939B1 (fr) * | 2007-10-26 | 2014-04-25 | Snecma | Turbomachine comprenant un diffuseur |
US7975506B2 (en) | 2008-02-20 | 2011-07-12 | Trane International, Inc. | Coaxial economizer assembly and method |
US8037713B2 (en) | 2008-02-20 | 2011-10-18 | Trane International, Inc. | Centrifugal compressor assembly and method |
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 |
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 |
EP2964960B1 (en) * | 2013-03-08 | 2019-06-12 | 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 |
US9926942B2 (en) | 2015-10-27 | 2018-03-27 | Pratt & Whitney Canada Corp. | Diffuser pipe with vortex generators |
US10570925B2 (en) | 2015-10-27 | 2020-02-25 | Pratt & Whitney Canada Corp. | Diffuser pipe with splitter vane |
US10030581B2 (en) | 2016-02-24 | 2018-07-24 | Pratt & Whitney Canada Corp. | Air intake with scroll portion and strutted portion for gas turbine engine |
US10087839B2 (en) | 2016-02-24 | 2018-10-02 | Pratt & Whitney Canada Corp. | Air intake for turboprop 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 |
US11939070B2 (en) | 2020-02-21 | 2024-03-26 | General Electric Company | Engine-mounting links that have an adjustable inclination angle |
US11970279B2 (en) | 2020-02-21 | 2024-04-30 | General Electric Company | Control system and methods of controlling an engine-mounting link system |
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 |
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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 IL IL14839400A patent/IL148394A0/xx not_active IP Right Cessation
- 2000-08-10 KR KR1020027002962A patent/KR100767886B1/ko not_active IP Right Cessation
- 2000-08-10 MX MXPA02002479A patent/MXPA02002479A/es active IP Right Grant
- 2000-08-10 JP JP2001521908A patent/JP4679017B2/ja not_active Expired - Fee Related
- 2000-08-10 CN CNB008149496A patent/CN1214191C/zh not_active Expired - Fee Related
- 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 EP EP00955443A patent/EP1214522B1/en not_active Expired - Lifetime
- 2000-08-10 DE DE60016937T patent/DE60016937T2/de not_active Expired - Lifetime
- 2000-08-10 AU AU67651/00A patent/AU759980B2/en not_active Ceased
- 2000-08-10 TR TR2002/00584T patent/TR200200584T2/tr unknown
-
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 |
---|---|
NO20021110L (no) | 2002-05-06 |
MXPA02002479A (es) | 2002-08-28 |
KR20020039343A (ko) | 2002-05-25 |
EP1214522B1 (en) | 2004-12-22 |
HK1051715A1 (en) | 2003-08-15 |
IL148394A0 (en) | 2002-09-12 |
JP2003508690A (ja) | 2003-03-04 |
NO20021110D0 (no) | 2002-03-06 |
AU759980B2 (en) | 2003-05-01 |
CA2384017A1 (en) | 2001-03-15 |
US6279322B1 (en) | 2001-08-28 |
CN1384902A (zh) | 2002-12-11 |
DE60016937T2 (de) | 2005-12-15 |
JP4679017B2 (ja) | 2011-04-27 |
EP1214522A1 (en) | 2002-06-19 |
CN1214191C (zh) | 2005-08-10 |
CA2384017C (en) | 2008-11-18 |
WO2001018404A1 (en) | 2001-03-15 |
KR100767886B1 (ko) | 2007-10-17 |
DE60016937D1 (de) | 2005-01-27 |
AU6765100A (en) | 2001-04-10 |
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