RU2357088C2 - Диффузор, имеющий возможность струйного исполнительного регулирования - Google Patents
Диффузор, имеющий возможность струйного исполнительного регулирования Download PDFInfo
- Publication number
- RU2357088C2 RU2357088C2 RU2003133190/06A RU2003133190A RU2357088C2 RU 2357088 C2 RU2357088 C2 RU 2357088C2 RU 2003133190/06 A RU2003133190/06 A RU 2003133190/06A RU 2003133190 A RU2003133190 A RU 2003133190A RU 2357088 C2 RU2357088 C2 RU 2357088C2
- Authority
- RU
- Russia
- Prior art keywords
- diffuser
- wall
- opening
- inlet
- additional
- Prior art date
Links
- 230000000694 effects Effects 0.000 claims abstract description 10
- 238000002347 injection Methods 0.000 claims description 44
- 239000007924 injection Substances 0.000 claims description 44
- 230000033228 biological regulation Effects 0.000 claims description 17
- 239000012530 fluid Substances 0.000 claims description 14
- 238000011144 upstream manufacturing Methods 0.000 claims description 12
- 238000005188 flotation Methods 0.000 claims description 8
- 238000012423 maintenance Methods 0.000 abstract description 2
- 239000000126 substance Substances 0.000 abstract 1
- 238000010926 purge Methods 0.000 description 60
- 238000011084 recovery Methods 0.000 description 37
- 238000000926 separation method Methods 0.000 description 35
- 239000003570 air Substances 0.000 description 29
- 230000003068 static effect Effects 0.000 description 17
- 238000010586 diagram Methods 0.000 description 15
- 230000033001 locomotion Effects 0.000 description 12
- 238000013461 design Methods 0.000 description 11
- 230000008901 benefit Effects 0.000 description 7
- 238000009826 distribution Methods 0.000 description 7
- 230000004323 axial length Effects 0.000 description 6
- 238000005094 computer simulation Methods 0.000 description 6
- 230000007423 decrease Effects 0.000 description 6
- 238000009792 diffusion process Methods 0.000 description 6
- 238000005516 engineering process Methods 0.000 description 6
- 238000004088 simulation Methods 0.000 description 6
- 230000003993 interaction Effects 0.000 description 4
- 238000002156 mixing Methods 0.000 description 4
- 238000012546 transfer Methods 0.000 description 4
- 239000012080 ambient air Substances 0.000 description 3
- 239000000498 cooling water Substances 0.000 description 3
- 238000002474 experimental method Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 238000004458 analytical method Methods 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 238000000576 coating method Methods 0.000 description 2
- 230000001427 coherent effect Effects 0.000 description 2
- 238000011161 development Methods 0.000 description 2
- 230000018109 developmental process Effects 0.000 description 2
- 238000000605 extraction Methods 0.000 description 2
- 238000012360 testing method Methods 0.000 description 2
- 238000013022 venting Methods 0.000 description 2
- 238000007664 blowing Methods 0.000 description 1
- 238000004364 calculation method Methods 0.000 description 1
- 230000015556 catabolic process Effects 0.000 description 1
- 239000013256 coordination polymer Substances 0.000 description 1
- 238000006731 degradation reaction Methods 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000013383 initial experiment Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- QSHDDOUJBYECFT-UHFFFAOYSA-N mercury Chemical compound [Hg] QSHDDOUJBYECFT-UHFFFAOYSA-N 0.000 description 1
- 229910052753 mercury Inorganic materials 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000004904 shortening Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000009827 uniform distribution Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04F—PUMPING OF FLUID BY DIRECT CONTACT OF ANOTHER FLUID OR BY USING INERTIA OF FLUID TO BE PUMPED; SIPHONS
- F04F5/00—Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow
- F04F5/54—Installations characterised by use of jet pumps, e.g. combinations of two or more jet pumps of different type
-
- 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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/30—Exhaust heads, chambers, or the like
-
- 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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/30—Exhaust heads, chambers, or the like
- F01D25/305—Exhaust heads, chambers, or the like with fluid, e.g. liquid injection
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15D—FLUID DYNAMICS, i.e. METHODS OR MEANS FOR INFLUENCING THE FLOW OF GASES OR LIQUIDS
- F15D1/00—Influencing flow of fluids
- F15D1/02—Influencing flow of fluids in pipes or conduits
- F15D1/06—Influencing flow of fluids in pipes or conduits by influencing the boundary layer
-
- 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
- F05D2250/00—Geometry
- F05D2250/30—Arrangement of components
- F05D2250/32—Arrangement of components according to their shape
- F05D2250/324—Arrangement of components according to their shape divergent
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S415/00—Rotary kinetic fluid motors or pumps
- Y10S415/914—Device to control boundary layer
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Supercharger (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Jet Pumps And Other Pumps (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US10/065,727 US6896475B2 (en) | 2002-11-13 | 2002-11-13 | Fluidic actuation for improved diffuser performance |
| US10/065,727 | 2002-11-13 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| RU2003133190A RU2003133190A (ru) | 2005-04-27 |
| RU2357088C2 true RU2357088C2 (ru) | 2009-05-27 |
Family
ID=29731624
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2003133190/06A RU2357088C2 (ru) | 2002-11-13 | 2003-11-12 | Диффузор, имеющий возможность струйного исполнительного регулирования |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US6896475B2 (enExample) |
| JP (1) | JP4527965B2 (enExample) |
| FR (1) | FR2847617B1 (enExample) |
| GB (3) | GB2429245B (enExample) |
| RU (1) | RU2357088C2 (enExample) |
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| US7477966B1 (en) * | 2004-02-20 | 2009-01-13 | Lockheed Martin Corporation | Propellant management system and method for multiple booster rockets |
| US7610179B2 (en) * | 2004-09-24 | 2009-10-27 | United Technologies Corporation | Coupled parametric design of flow control and duct shape |
| US7698116B2 (en) * | 2005-05-23 | 2010-04-13 | 3M Innovative Properties Company | Manifolds for delivering fluids having a desired mass flow profile and methods for designing the same |
| US7901614B2 (en) * | 2005-05-23 | 2011-03-08 | 3M Innovative Properties Company | Methods and apparatus for meltblowing of polymeric material utilizing fluid flow from an auxiliary manifold |
| GB2442422B8 (en) * | 2005-08-04 | 2015-12-16 | Rolls Royce Power Eng | Gas turbine exhaust diffuser |
| US8171732B2 (en) * | 2006-09-08 | 2012-05-08 | General Electric Company | Turbocharger for a vehicle with a coanda device |
| US7731475B2 (en) * | 2007-05-17 | 2010-06-08 | Elliott Company | Tilted cone diffuser for use with an exhaust system of a turbine |
| US20080315042A1 (en) * | 2007-06-20 | 2008-12-25 | General Electric Company | Thrust generator for a propulsion system |
| NO327504B1 (no) | 2007-10-26 | 2009-07-27 | Ntnu Technology Transfer As | En ejektor for fluider |
| US8257025B2 (en) * | 2008-04-21 | 2012-09-04 | Siemens Energy, Inc. | Combustion turbine including a diffuser section with cooling fluid passageways and associated methods |
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| US8668449B2 (en) * | 2009-06-02 | 2014-03-11 | Siemens Energy, Inc. | Turbine exhaust diffuser with region of reduced flow area and outer boundary gas flow |
| US8647057B2 (en) * | 2009-06-02 | 2014-02-11 | Siemens Energy, Inc. | Turbine exhaust diffuser with a gas jet producing a coanda effect flow control |
| US8328513B2 (en) * | 2009-12-31 | 2012-12-11 | General Electric Company | Systems and apparatus relating to compressor stator blades and diffusers in turbine engines |
| JP5331715B2 (ja) * | 2010-01-07 | 2013-10-30 | 株式会社日立製作所 | ガスタービン,排気ディフューザおよびガスタービンプラントの改造方法 |
| EP2412941A1 (en) * | 2010-07-26 | 2012-02-01 | Siemens Aktiengesellschaft | Exhaust diffuser for a gas turbine, and method thereof |
| US9249687B2 (en) * | 2010-10-27 | 2016-02-02 | General Electric Company | Turbine exhaust diffusion system and method |
| US20120186261A1 (en) * | 2011-01-20 | 2012-07-26 | General Electric Company | System and method for a gas turbine exhaust diffuser |
| US8919127B2 (en) | 2011-05-24 | 2014-12-30 | General Electric Company | System and method for flow control in gas turbine engine |
| US20130022444A1 (en) * | 2011-07-19 | 2013-01-24 | Sudhakar Neeli | Low pressure turbine exhaust diffuser with turbulators |
| US20130064638A1 (en) | 2011-09-08 | 2013-03-14 | Moorthi Subramaniyan | Boundary Layer Blowing Using Steam Seal Leakage Flow |
| US9115602B2 (en) | 2011-10-19 | 2015-08-25 | Siemens Aktiengesellschaft | Exhaust diffuser including flow mixing ramp for a gas turbine engine |
| US8756936B2 (en) * | 2011-10-19 | 2014-06-24 | Siemens Aktiengesellschaft | Exhaust diffuser adjustment system for a gas turbine engine |
| US9995181B2 (en) * | 2011-11-30 | 2018-06-12 | Lockheed Martin Corporation | Exhaust impingement cooling |
| US9032721B2 (en) * | 2011-12-14 | 2015-05-19 | Siemens Energy, Inc. | Gas turbine engine exhaust diffuser including circumferential vane |
| US20130174534A1 (en) * | 2012-01-05 | 2013-07-11 | General Electric Company | System and device for controlling fluid flow through a gas turbine exhaust |
| US20130174553A1 (en) * | 2012-01-11 | 2013-07-11 | General Electric Company | Diffuser having fluidic actuation |
| US9109467B2 (en) * | 2012-07-05 | 2015-08-18 | General Electric Company | Exhaust system for use with a turbine and method of assembling same |
| CN104781519B (zh) * | 2012-11-28 | 2017-06-23 | 博格华纳公司 | 具有流量放大器的涡流增压器的压缩机级 |
| CN203441604U (zh) * | 2013-02-15 | 2014-02-19 | 通用电气公司 | 用于降低燃气涡轮系统中的背压的系统 |
| JP5766739B2 (ja) * | 2013-04-04 | 2015-08-19 | 株式会社東芝 | ディフューザ |
| WO2014175763A1 (en) * | 2013-04-25 | 2014-10-30 | Siemens Aktiengesellschaft | Turbo-machine and waste heat utilization device |
| US11732892B2 (en) | 2013-08-14 | 2023-08-22 | General Electric Company | Gas turbomachine diffuser assembly with radial flow splitters |
| US9541030B2 (en) * | 2013-11-27 | 2017-01-10 | Lockheed Martin Corporation | Exhaust plume cooling using periodic interruption of exhaust gas flow to form ambient air entraining vortices |
| US9741575B2 (en) * | 2014-03-10 | 2017-08-22 | Taiwan Semiconductor Manufacturing Co., Ltd. | CVD apparatus with gas delivery ring |
| WO2016001002A1 (de) * | 2014-07-03 | 2016-01-07 | Abb Turbo Systems Ag | Abströmbereich einer turbine eines abgasturboladers |
| US10316696B2 (en) * | 2015-05-08 | 2019-06-11 | General Electric Company | System and method for improving exhaust energy recovery |
| JP2016217355A (ja) | 2015-05-22 | 2016-12-22 | ゼネラル・エレクトリック・カンパニイ | 流れ混合ローブを含むターボ機械ディフューザ及びその方法 |
| US20170022834A1 (en) * | 2015-07-22 | 2017-01-26 | John A. Orosa | High pressure compressor diffuser for an industrial gas turbine engine |
| CN106679926B (zh) * | 2016-12-29 | 2018-10-09 | 中国航天空气动力技术研究院 | 一种高超声速风洞薄膜冷却实验系统及实验方法 |
| KR101909595B1 (ko) | 2017-04-28 | 2018-12-19 | 두산중공업 주식회사 | 분사구, 흡입구를 포함하는 배기 디퓨저 및 이를 포함하는 가스터빈 |
| CN209638120U (zh) | 2017-10-20 | 2019-11-15 | 创科(澳门离岸商业服务)有限公司 | 风扇 |
| PL426033A1 (pl) | 2018-06-22 | 2020-01-02 | General Electric Company | Płynowe pompy strumieniowe parowe, a także układy i sposoby porywania płynu przy użyciu płynowych pomp strumieniowych parowych |
| KR102587329B1 (ko) * | 2018-12-10 | 2023-10-10 | 한화에어로스페이스 주식회사 | 기체의 유동 손실을 저감시키는 보조동력장치 |
| JP7346165B2 (ja) * | 2019-08-29 | 2023-09-19 | 三菱重工業株式会社 | クロスフローファン、これを備えた揚力発生装置およびこれを備えた航空機 |
| CN110685756B (zh) * | 2019-10-10 | 2022-03-15 | 中国船舶重工集团公司第七0五研究所 | 一种低流动压力损失异形渐变排气结构 |
| US12134987B2 (en) | 2020-03-26 | 2024-11-05 | Hamilton Sundstrand Corporation | Exhaust baffle component for an air turbine starter assembly |
| US11753997B2 (en) * | 2020-03-26 | 2023-09-12 | Hamilton Sundstrand Corporation | Exhaust baffle component for an air turbine assembly |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2812636A (en) * | 1950-06-16 | 1957-11-12 | Snecma | Process and device for deflecting jets |
| US3690786A (en) * | 1971-05-10 | 1972-09-12 | Westinghouse Electric Corp | Low pressure end diffuser for axial flow elastic fluid turbines |
| US3885891A (en) * | 1972-11-30 | 1975-05-27 | Rockwell International Corp | Compound ejector |
| RU2053373C1 (ru) * | 1989-02-13 | 1996-01-27 | Научно-производственное объединение "Турбоатом" | Выхлопная часть паровой турбины |
Family Cites Families (26)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3123285A (en) * | 1964-03-03 | Diffuser with boundary layer control | ||
| US2052869A (en) * | 1934-10-08 | 1936-09-01 | Coanda Henri | Device for deflecting a stream of elastic fluid projected into an elastic fluid |
| BE560119A (enExample) * | 1956-09-13 | |||
| US3719430A (en) * | 1971-08-24 | 1973-03-06 | Gen Electric | Diffuser |
| US4029430A (en) * | 1975-09-02 | 1977-06-14 | Fonda Bonardi Giusto | Short subsonic diffuser for large pressure ratios |
| IL48928A (en) * | 1976-01-29 | 1978-04-30 | Univ Ben Gurion | Wind-driven energy generating device |
| SU775355A1 (ru) | 1979-01-05 | 1980-10-30 | Предприятие П/Я В-2994 | Выхлопное устройство паровой турбины |
| SU832129A1 (ru) | 1979-07-04 | 1981-05-23 | Московский Ордена Ленина Энергети-Ческий Институт | Осерадиальный диффузор выхлопногопАТРубКА ТуРбОМАшиНы |
| SU857517A1 (ru) | 1979-09-25 | 1981-08-23 | Харьковский Ордена Ленина Политехнический Институт Им. В.И.Ленина | Выхлопной патрубок турбомашины |
| US4487366A (en) * | 1981-03-12 | 1984-12-11 | Rockwell International Corporation | Porous-wall compact laser diffuser |
| SU969919A1 (ru) | 1981-04-29 | 1982-10-30 | Московский Ордена Ленина И Ордена Октябрьской Революции Энергетический Институт | Выхлопной патрубок паровой турбины |
| US4448354A (en) * | 1982-07-23 | 1984-05-15 | The United States Of America As Represented By The Secretary Of The Air Force | Axisymmetric thrust augmenting ejector with discrete primary air slot nozzles |
| US4515524A (en) * | 1982-09-27 | 1985-05-07 | Allis-Chalmers Corporation | Draft tube for hydraulic turbine |
| SU1109529A1 (ru) | 1982-10-06 | 1984-08-23 | Производственное объединение "Турбомоторный завод" | Выхлопной патрубок теплофикационной турбины |
| SU1222859A1 (ru) | 1984-10-30 | 1986-04-07 | Харьковский Ордена Ленина Политехнический Институт Им.В.И.Ленина | Выхлопной патрубок паровой турбины |
| SU1321847A1 (ru) | 1985-01-04 | 1987-07-07 | Производственное Объединение "Турмоторный Завод" Им.К.Е.Ворошилова | Выхлопной патрубок паровой турбины |
| SU1454991A1 (ru) | 1987-05-25 | 1989-01-30 | Харьковский политехнический институт им.В.И.Ленина | Выхлопна часть турбомашины |
| US5077967A (en) * | 1990-11-09 | 1992-01-07 | General Electric Company | Profile matched diffuser |
| FR2697287B1 (fr) * | 1992-10-26 | 1994-12-09 | Europ Gas Turbines Sa | Diffuseur d'échappement de turbine à gaz. |
| US5335501A (en) * | 1992-11-16 | 1994-08-09 | General Electric Company | Flow spreading diffuser |
| US5467591A (en) * | 1993-12-30 | 1995-11-21 | Combustion Engineering, Inc. | Gas turbine combined cycle system |
| RU2050440C1 (ru) | 1994-05-13 | 1995-12-20 | Аркадий Ефимович Зарянкин | Проточная часть низкого давления турбины |
| EP0796196A4 (en) * | 1994-12-30 | 1998-04-01 | Grumman Aerospace Corp | NOZZLE WITH A FLUID CONTROLLED DIRECTION |
| US5737915A (en) * | 1996-02-09 | 1998-04-14 | General Electric Co. | Tri-passage diffuser for a gas turbine |
| US5603605A (en) * | 1996-04-01 | 1997-02-18 | Fonda-Bonardi; G. | Diffuser |
| US6027305A (en) * | 1997-08-13 | 2000-02-22 | Virginia Tech Intellectual Properties, Inc. | Method and apparatus for reducing high-cycle fatigue and suppressing noise in rotating machinery |
-
2002
- 2002-11-13 US US10/065,727 patent/US6896475B2/en not_active Expired - Fee Related
-
2003
- 2003-11-10 FR FR0313195A patent/FR2847617B1/fr not_active Expired - Fee Related
- 2003-11-12 JP JP2003381984A patent/JP4527965B2/ja not_active Expired - Fee Related
- 2003-11-12 GB GB0621844A patent/GB2429245B/en not_active Expired - Fee Related
- 2003-11-12 GB GB0621845A patent/GB2429246B/en not_active Expired - Fee Related
- 2003-11-12 GB GB0326410A patent/GB2395757B/en not_active Expired - Fee Related
- 2003-11-12 RU RU2003133190/06A patent/RU2357088C2/ru not_active IP Right Cessation
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2812636A (en) * | 1950-06-16 | 1957-11-12 | Snecma | Process and device for deflecting jets |
| US3690786A (en) * | 1971-05-10 | 1972-09-12 | Westinghouse Electric Corp | Low pressure end diffuser for axial flow elastic fluid turbines |
| US3885891A (en) * | 1972-11-30 | 1975-05-27 | Rockwell International Corp | Compound ejector |
| RU2053373C1 (ru) * | 1989-02-13 | 1996-01-27 | Научно-производственное объединение "Турбоатом" | Выхлопная часть паровой турбины |
Also Published As
| Publication number | Publication date |
|---|---|
| JP4527965B2 (ja) | 2010-08-18 |
| GB2429246A (en) | 2007-02-21 |
| JP2004162715A (ja) | 2004-06-10 |
| FR2847617A1 (fr) | 2004-05-28 |
| GB2395757B (en) | 2007-01-24 |
| GB0326410D0 (en) | 2003-12-17 |
| GB2429245A (en) | 2007-02-21 |
| US6896475B2 (en) | 2005-05-24 |
| FR2847617B1 (fr) | 2010-02-26 |
| GB2429246B (en) | 2007-08-15 |
| GB2429245B (en) | 2007-08-15 |
| GB2395757A (en) | 2004-06-02 |
| GB0621845D0 (en) | 2006-12-13 |
| US20040091350A1 (en) | 2004-05-13 |
| GB0621844D0 (en) | 2006-12-13 |
| RU2003133190A (ru) | 2005-04-27 |
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