CN100422510C - 可变喷嘴涡轮增压器的改进叶片 - Google Patents
可变喷嘴涡轮增压器的改进叶片 Download PDFInfo
- Publication number
- CN100422510C CN100422510C CNB02800079XA CN02800079A CN100422510C CN 100422510 C CN100422510 C CN 100422510C CN B02800079X A CNB02800079X A CN B02800079XA CN 02800079 A CN02800079 A CN 02800079A CN 100422510 C CN100422510 C CN 100422510C
- Authority
- CN
- China
- Prior art keywords
- blade
- vane
- axial
- variable geometry
- post
- 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.)
- Expired - Lifetime
Links
- 230000001105 regulatory effect Effects 0.000 claims description 18
- 230000007935 neutral effect Effects 0.000 claims description 5
- 230000008676 import Effects 0.000 claims description 4
- 239000007789 gas Substances 0.000 description 13
- 230000007246 mechanism Effects 0.000 description 8
- 239000002912 waste gas Substances 0.000 description 5
- 239000000463 material Substances 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 230000009471 action Effects 0.000 description 2
- 230000008859 change Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000006872 improvement Effects 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 238000002485 combustion reaction Methods 0.000 description 1
- 230000001143 conditioned effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
- F02B37/12—Control of the pumps
- F02B37/22—Control of the pumps by varying cross-section of exhaust passages or air passages, e.g. by throttling turbine inlets or outlets or by varying effective number of guide conduits
-
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/141—Shape, i.e. outer, aerodynamic form
-
- 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
- F01D17/00—Regulating or controlling by varying flow
- F01D17/10—Final actuators
- F01D17/12—Final actuators arranged in stator parts
- F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
- F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
- F01D17/165—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for radial flow, i.e. the vanes turning around axes which are essentially parallel to the rotor centre line
-
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
- F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
- F02C6/10—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output supplying working fluid to a user, e.g. a chemical process, which returns working fluid to a turbine of the plant
- F02C6/12—Turbochargers, i.e. plants for augmenting mechanical power output of internal-combustion piston engines by increase of charge pressure
-
- 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
- F05D2220/00—Application
- F05D2220/40—Application in turbochargers
-
- 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
- F05D2250/40—Movement of components
- F05D2250/41—Movement of components with one degree of freedom
- F05D2250/411—Movement of components with one degree of freedom in rotation
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Chemical Kinetics & Catalysis (AREA)
- General Chemical & Material Sciences (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Supercharger (AREA)
- Control Of Turbines (AREA)
Abstract
Description
Claims (6)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/761,277 | 2001-01-16 | ||
US09/761,277 US6419464B1 (en) | 2001-01-16 | 2001-01-16 | Vane for variable nozzle turbocharger |
Publications (2)
Publication Number | Publication Date |
---|---|
CN1455843A CN1455843A (zh) | 2003-11-12 |
CN100422510C true CN100422510C (zh) | 2008-10-01 |
Family
ID=25061745
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CNB02800079XA Expired - Lifetime CN100422510C (zh) | 2001-01-16 | 2002-01-16 | 可变喷嘴涡轮增压器的改进叶片 |
Country Status (10)
Country | Link |
---|---|
US (2) | US6419464B1 (zh) |
EP (1) | EP1352157B1 (zh) |
JP (1) | JP2004518062A (zh) |
KR (1) | KR20020084114A (zh) |
CN (1) | CN100422510C (zh) |
CZ (1) | CZ20022873A3 (zh) |
HU (1) | HUP0300055A2 (zh) |
MX (1) | MXPA02007528A (zh) |
PL (1) | PL357217A1 (zh) |
WO (1) | WO2002057599A1 (zh) |
Families Citing this family (75)
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US6887046B2 (en) * | 1996-02-26 | 2005-05-03 | Flowork Systems Ii Llc | Coolant pump, mainly for automotive use |
US6729134B2 (en) * | 2001-01-16 | 2004-05-04 | Honeywell International Inc. | Variable geometry turbocharger having internal bypass exhaust gas flow |
DE60331373D1 (de) * | 2003-03-21 | 2010-04-01 | Honeywell Int Inc | Schwingschaufelkonzept für vnt-turbolader |
GB2400633B (en) * | 2003-04-15 | 2005-03-09 | Honeywell Int Inc | Variable flow nozzle for a turbocharger |
US7059129B2 (en) * | 2003-09-25 | 2006-06-13 | Honeywell International, Inc. | Variable geometry turbocharger |
CN100400799C (zh) * | 2003-09-25 | 2008-07-09 | 霍尼韦尔国际公司 | 几何形状可变的涡轮增压器 |
US7147433B2 (en) * | 2003-11-19 | 2006-12-12 | Honeywell International, Inc. | Profiled blades for turbocharger turbines, compressors, and the like |
US20050123394A1 (en) * | 2003-12-03 | 2005-06-09 | Mcardle Nathan J. | Compressor diffuser |
US7255530B2 (en) * | 2003-12-12 | 2007-08-14 | Honeywell International Inc. | Vane and throat shaping |
CN100400798C (zh) * | 2003-12-31 | 2008-07-09 | 洪尼维尔国际公司 | 用于涡轮增压器的曲面叶片 |
GB0407978D0 (en) * | 2004-04-08 | 2004-05-12 | Holset Engineering Co | Variable geometry turbine |
US7137778B2 (en) * | 2004-04-12 | 2006-11-21 | Borgwarner Inc. | Variable turbine geometry turbocharger |
US6925806B1 (en) * | 2004-04-21 | 2005-08-09 | Honeywell International, Inc. | Variable geometry assembly for turbochargers |
US7124582B2 (en) * | 2004-07-26 | 2006-10-24 | International Engine Intellectual Property Company, Llc | Method and apparatus for determining turbocharger boost |
KR101070903B1 (ko) * | 2004-08-19 | 2011-10-06 | 삼성테크윈 주식회사 | 가변 베인형 터빈 |
WO2006053579A1 (en) * | 2004-11-16 | 2006-05-26 | Honeywell International Inc. | Variable nozzle turbocharger |
US7305826B2 (en) * | 2005-02-16 | 2007-12-11 | Honeywell International , Inc. | Axial loading management in turbomachinery |
US8016551B2 (en) * | 2005-11-03 | 2011-09-13 | Honeywell International, Inc. | Reverse curved nozzle for radial inflow turbines |
KR20070060383A (ko) * | 2005-12-08 | 2007-06-13 | 현대자동차주식회사 | 베인의 최소 유로 확보가 가능한 가변 용량 제어 터보차저구조 |
JP2007205306A (ja) * | 2006-02-03 | 2007-08-16 | Mazda Motor Corp | 過給機付きエンジン |
WO2008023034A1 (de) * | 2006-08-24 | 2008-02-28 | Abb Turbo Systems Ag | Diffusor eines radialverdichters |
US7559199B2 (en) * | 2006-09-22 | 2009-07-14 | Honeywell International Inc. | Variable-nozzle cartridge for a turbocharger |
US8500395B2 (en) * | 2007-02-15 | 2013-08-06 | Borgwarner Inc. | Turbocharger vane |
WO2008124758A1 (en) * | 2007-04-10 | 2008-10-16 | Elliott Company | Centrifugal compressor having adjustable inlet guide vanes |
US20090067978A1 (en) * | 2007-05-24 | 2009-03-12 | Suljak Jr George T | Variable area turbine vane arrangement |
US8007229B2 (en) * | 2007-05-24 | 2011-08-30 | United Technologies Corporation | Variable area turbine vane arrangement |
KR101316400B1 (ko) * | 2007-07-27 | 2013-10-08 | 현대자동차주식회사 | 터보 차져 배기소음 감소장치 |
US20090133399A1 (en) * | 2007-11-27 | 2009-05-28 | Caterpillar Inc. | Turbocharger system implementing real time speed limiting |
US8257035B2 (en) * | 2007-12-05 | 2012-09-04 | Siemens Energy, Inc. | Turbine vane for a gas turbine engine |
US8105019B2 (en) * | 2007-12-10 | 2012-01-31 | United Technologies Corporation | 3D contoured vane endwall for variable area turbine vane arrangement |
US8807926B2 (en) * | 2008-11-05 | 2014-08-19 | Ihi Corporation | Turbocharger |
GB0822474D0 (en) * | 2008-12-10 | 2009-01-14 | Cummins Turbo Tech Ltd | Variable geometry turbine nozzle ring |
CN101634233B (zh) * | 2009-08-20 | 2011-07-20 | 康跃科技股份有限公司 | 可变几何涡轮增压器的气动喷嘴 |
WO2011026018A2 (en) * | 2009-08-30 | 2011-03-03 | Steven Don Arnold | Variable volute turbine |
US8480357B2 (en) | 2009-11-09 | 2013-07-09 | Honeywell International Inc. | Variable geometry turbocharger with guide pins |
US8511981B2 (en) * | 2010-07-19 | 2013-08-20 | Cameron International Corporation | Diffuser having detachable vanes with positive lock |
WO2012036328A1 (ko) * | 2010-09-15 | 2012-03-22 | (주)계양정밀 | 가변 노즐 장치 및 이를 구비한 터보차져 |
DE102010047251A1 (de) * | 2010-10-04 | 2011-12-01 | Voith Patent Gmbh | Leitapparat |
KR101046205B1 (ko) * | 2010-12-14 | 2011-07-04 | 한국기계연구원 | 가변 베인형 터빈 |
US8653687B2 (en) * | 2011-04-04 | 2014-02-18 | Ebara International Corporation | Liquefied gas expander nozzle ring having adjustable guide vanes |
CN102383871B (zh) * | 2011-07-21 | 2014-12-03 | 常州新瑞汽车配件制造有限公司 | 涡轮增压器的工作方法 |
CN102297016B (zh) * | 2011-08-15 | 2012-12-12 | 无锡凯迪增压器配件有限公司 | 双叶片喷嘴系统的涡轮增压器 |
US8919119B2 (en) | 2011-08-16 | 2014-12-30 | Ford Global Technologies, Llc | Sliding vane geometry turbines |
US8985943B2 (en) * | 2011-09-30 | 2015-03-24 | Honeywell International Inc. | Turbocharger variable-nozzle assembly with vane sealing arrangement |
CN103089344B (zh) * | 2011-11-04 | 2015-06-17 | 萍乡市德博科技发展有限公司 | 拨动盘双向定位叶片双支撑可变截面喷嘴环组件 |
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KR20140063474A (ko) * | 2012-11-16 | 2014-05-27 | 에이비비 터보 시스템즈 아게 | 노즐 링 |
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JP5836317B2 (ja) * | 2013-05-16 | 2015-12-24 | 株式会社豊田自動織機 | 可変ノズルターボチャージャ |
KR101484415B1 (ko) * | 2013-10-29 | 2015-01-19 | 현대위아 주식회사 | 가변 지오메트리 터보 차저용 베인 카트리지 장치 |
KR20150050673A (ko) * | 2013-10-30 | 2015-05-11 | 현대자동차주식회사 | 가변 지오메트리 터보 시스템 |
WO2015118562A2 (en) * | 2014-02-07 | 2015-08-13 | Turbo Energy Limited | An improved vane for variable turbine geometry turbochargers |
CN105081760B (zh) * | 2014-04-30 | 2020-02-18 | 西门子公司 | 组装喷嘴环的方法 |
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US10253648B2 (en) | 2016-03-04 | 2019-04-09 | General Electric Company | Modulated hybrid variable area turbine nozzle for gas turbine engine |
ITUA20164308A1 (it) | 2016-06-13 | 2017-12-13 | Nuovo Pignone Tecnologie Srl | Assieme a geometria variabile per turbomacchina e turbomacchina comprendente detto assieme |
CN112096514B (zh) | 2016-08-24 | 2022-05-31 | 株式会社Ihi | 可变容量型增压器 |
IT201600127428A1 (it) * | 2016-12-16 | 2018-06-16 | Cusani Alberto Bartorelli | Nuova proteina ricombinante uk 114 in forma stabile polimerica per uso nella terapia, nella diagnostica e nella prevenzione di neoplasie maligne |
CN107269386B (zh) * | 2017-08-21 | 2019-04-16 | 安徽江淮汽车集团股份有限公司 | 涡轮增压器 |
CN107559086B (zh) * | 2017-08-21 | 2019-06-28 | 安徽江淮汽车集团股份有限公司 | 涡轮增压器 |
US10480326B2 (en) * | 2017-09-11 | 2019-11-19 | United Technologies Corporation | Vane for variable area turbine |
CN115573938A (zh) | 2017-09-25 | 2023-01-06 | 江森自控泰科知识产权控股有限责任合伙公司 | 紧凑可变几何形状的扩散器机构 |
CN107701296B (zh) * | 2017-09-25 | 2019-08-06 | 安徽江淮汽车集团股份有限公司 | 一种涡轮增压器进气调节装置 |
US10883379B2 (en) * | 2018-05-11 | 2021-01-05 | Rolls-Royce Corporation | Variable diffuser having a respective penny for each vane |
DE102018211673A1 (de) * | 2018-07-12 | 2020-01-16 | Continental Automotive Gmbh | Leitschaufel und mit einer solchen versehene Turbinenanordnung |
FR3085720B1 (fr) * | 2018-09-06 | 2020-08-07 | Liebherr-Aerospace Toulouse Sas | Distributeur d'une turbine radiale de turbomachine, turbomachine comprenant un tel distributeur et systeme de conditionnement d'air comprenant une telle turbomachine |
CN109209525B (zh) * | 2018-11-23 | 2021-11-26 | 府谷科创源能源科技股份有限公司 | 一种高背压蒸汽轮机组 |
US10927702B1 (en) | 2019-03-30 | 2021-02-23 | Savant Holdings LLC | Turbocharger or turbocharger component |
DE112020002877T5 (de) * | 2019-06-14 | 2022-03-10 | Ihi Corporation | Turbolader |
US10995684B1 (en) * | 2019-11-21 | 2021-05-04 | Internatinal Engine Intellectual Property Company, LLC. | Smart actuator learn command process |
EP3929407A1 (de) * | 2020-06-23 | 2021-12-29 | ABB Schweiz AG | Modularer düsenring für eine turbinenstufe einer strömungsmaschine |
US11530615B1 (en) * | 2022-03-01 | 2022-12-20 | Garrett Transportation I Inc. | Method for constructing a fixed-vane ring for a nozzle of a turbocharger turbine |
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2001
- 2001-01-16 US US09/761,277 patent/US6419464B1/en not_active Expired - Lifetime
-
2002
- 2002-01-16 JP JP2002557646A patent/JP2004518062A/ja active Pending
- 2002-01-16 CN CNB02800079XA patent/CN100422510C/zh not_active Expired - Lifetime
- 2002-01-16 EP EP02713429.5A patent/EP1352157B1/en not_active Expired - Lifetime
- 2002-01-16 WO PCT/US2002/001397 patent/WO2002057599A1/en not_active Application Discontinuation
- 2002-01-16 KR KR1020027010145A patent/KR20020084114A/ko not_active Application Discontinuation
- 2002-01-16 MX MXPA02007528A patent/MXPA02007528A/es active IP Right Grant
- 2002-01-16 HU HU0300055A patent/HUP0300055A2/hu unknown
- 2002-01-16 PL PL02357217A patent/PL357217A1/xx unknown
- 2002-01-16 CZ CZ20022873A patent/CZ20022873A3/cs unknown
- 2002-03-04 US US10/090,864 patent/US6672059B2/en not_active Expired - Fee Related
Patent Citations (8)
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GB731822A (en) * | 1952-03-14 | 1955-06-15 | Power Jets Res & Dev Ltd | Improvements relating to turbines or compressors for operation with gaseous fluids |
US4300869A (en) * | 1980-02-11 | 1981-11-17 | Swearingen Judson S | Method and apparatus for controlling clamping forces in fluid flow control assemblies |
US4502836A (en) * | 1982-07-02 | 1985-03-05 | Swearingen Judson S | Method for nozzle clamping force control |
US4679984A (en) * | 1985-12-11 | 1987-07-14 | The Garrett Corporation | Actuation system for variable nozzle turbine |
US4804316A (en) * | 1985-12-11 | 1989-02-14 | Allied-Signal Inc. | Suspension for the pivoting vane actuation mechanism of a variable nozzle turbocharger |
US5931636A (en) * | 1997-08-28 | 1999-08-03 | General Electric Company | Variable area turbine nozzle |
FR2767862A1 (fr) * | 1997-09-03 | 1999-03-05 | Air Liquide | Turbine cryogenique a aubage variable |
US5851104A (en) * | 1997-12-15 | 1998-12-22 | Atlas Copco Rotoflow, Inc. | Nozzle adjusting mechanism |
Also Published As
Publication number | Publication date |
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PL357217A1 (en) | 2004-07-26 |
US20020094284A1 (en) | 2002-07-18 |
MXPA02007528A (es) | 2003-03-27 |
KR20020084114A (ko) | 2002-11-04 |
HUP0300055A2 (en) | 2003-04-28 |
US6672059B2 (en) | 2004-01-06 |
JP2004518062A (ja) | 2004-06-17 |
EP1352157A1 (en) | 2003-10-15 |
EP1352157B1 (en) | 2013-07-10 |
US6419464B1 (en) | 2002-07-16 |
US20020187061A1 (en) | 2002-12-12 |
WO2002057599A1 (en) | 2002-07-25 |
CZ20022873A3 (cs) | 2003-04-16 |
CN1455843A (zh) | 2003-11-12 |
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