DE69914199D1 - Langsamlaufender hochdruckturbolader - Google Patents
Langsamlaufender hochdruckturboladerInfo
- Publication number
- DE69914199D1 DE69914199D1 DE69914199T DE69914199T DE69914199D1 DE 69914199 D1 DE69914199 D1 DE 69914199D1 DE 69914199 T DE69914199 T DE 69914199T DE 69914199 T DE69914199 T DE 69914199T DE 69914199 D1 DE69914199 D1 DE 69914199D1
- Authority
- DE
- Germany
- Prior art keywords
- booler
- high pressure
- slow running
- running high
- slow
- 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
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
- F04D29/26—Rotors specially for elastic fluids
- F04D29/28—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D25/00—Pumping installations or systems
- F04D25/02—Units comprising pumps and their driving means
- F04D25/024—Units comprising pumps and their driving means the driving means being assisted by a power recovery turbine
-
- 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
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/28—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
- F04D29/284—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for compressors
- F04D29/286—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for compressors multi-stage rotors
-
- 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
- F04D29/4206—Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- General Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Supercharger (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US109538 | 1998-07-02 | ||
US09/109,538 US6062028A (en) | 1998-07-02 | 1998-07-02 | Low speed high pressure ratio turbocharger |
PCT/US1999/014938 WO2000001935A1 (en) | 1998-07-02 | 1999-06-30 | Low speed high pressure ratio turbocharger |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69914199D1 true DE69914199D1 (de) | 2004-02-19 |
DE69914199T2 DE69914199T2 (de) | 2004-08-05 |
Family
ID=22328203
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69914199T Expired - Lifetime DE69914199T2 (de) | 1998-07-02 | 1999-06-30 | Langsamlaufender hochdruckturbolader |
Country Status (9)
Country | Link |
---|---|
US (1) | US6062028A (de) |
EP (1) | EP1092085B1 (de) |
JP (1) | JP4317327B2 (de) |
KR (1) | KR100588824B1 (de) |
AU (1) | AU4729899A (de) |
BR (1) | BR9911807A (de) |
CA (1) | CA2337790C (de) |
DE (1) | DE69914199T2 (de) |
WO (1) | WO2000001935A1 (de) |
Families Citing this family (66)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20080029888A1 (en) * | 1999-11-01 | 2008-02-07 | International Business Machines Corporation | Solder Interconnect Joints For A Semiconductor Package |
US6354815B1 (en) * | 2000-05-10 | 2002-03-12 | General Motors Corporation | Turbocharger thermal isolation connection |
US6293103B1 (en) * | 2000-09-21 | 2001-09-25 | Caterpillar Inc. | Turbocharger system to inhibit reduced pressure in intake manifold |
US6434943B1 (en) | 2000-10-03 | 2002-08-20 | George Washington University | Pressure exchanging compressor-expander and methods of use |
US7134093B2 (en) | 2001-04-18 | 2006-11-07 | International Business Machines Corporation | Graphical user interface for direct control of display of data |
US7048520B1 (en) * | 2002-04-16 | 2006-05-23 | Mccarthy James | Multistage sealed coolant pump |
US6792755B2 (en) | 2002-07-30 | 2004-09-21 | Honeywell International Inc. | High-pressure ratio turbocharger |
AU2003260101A1 (en) * | 2002-08-21 | 2004-03-11 | Honeywell International Inc. | Egr system for turbocharged engines |
US6651431B1 (en) | 2002-08-28 | 2003-11-25 | Ford Global Technologies, Llc | Boosted internal combustion engines and air compressors used therein |
US6920754B2 (en) * | 2003-05-05 | 2005-07-26 | Honeywell International, Inc. | High-pressure ratio turbocharger |
US7044718B1 (en) * | 2003-07-08 | 2006-05-16 | The Regents Of The University Of California | Radial-radial single rotor turbine |
US6834501B1 (en) | 2003-07-11 | 2004-12-28 | Honeywell International, Inc. | Turbocharger compressor with non-axisymmetric deswirl vanes |
US6948314B2 (en) * | 2003-09-12 | 2005-09-27 | Honeywell International, Inc. | High response, compact turbocharger |
DE10347842A1 (de) * | 2003-10-10 | 2005-04-28 | Daimler Chrysler Ag | Verdichter- und Turbinenrad für eine Sekundärluftfördereinrichtung |
US7128061B2 (en) * | 2003-10-31 | 2006-10-31 | Vortech Engineering, Inc. | Supercharger |
US7013879B2 (en) * | 2003-11-17 | 2006-03-21 | Honeywell International, Inc. | Dual and hybrid EGR systems for use with turbocharged engine |
US7014418B1 (en) * | 2004-12-03 | 2006-03-21 | Honeywell International, Inc. | Multi-stage compressor and housing therefor |
US7407364B2 (en) * | 2005-03-01 | 2008-08-05 | Honeywell International, Inc. | Turbocharger compressor having ported second-stage shroud, and associated method |
US20060254274A1 (en) * | 2005-05-14 | 2006-11-16 | Davorin Kapich | Hydraulic turbine assisted turbocharger system |
JP4947405B2 (ja) * | 2005-12-28 | 2012-06-06 | 株式会社Ihi | ターボ圧縮機 |
JP2007177695A (ja) * | 2005-12-28 | 2007-07-12 | Ishikawajima Harima Heavy Ind Co Ltd | ターボ圧縮機 |
US7600961B2 (en) * | 2005-12-29 | 2009-10-13 | Macro-Micro Devices, Inc. | Fluid transfer controllers having a rotor assembly with multiple sets of rotor blades arranged in proximity and about the same hub component and further having barrier components configured to form passages for routing fluid through the multiple sets of rotor blades |
US7758320B2 (en) * | 2007-05-03 | 2010-07-20 | Tank, Inc. | Two-stage hydrodynamic pump and method |
CN101680360B (zh) * | 2007-06-26 | 2012-09-05 | 博格华纳公司 | 涡轮增压器的扩散器 |
US8118570B2 (en) * | 2007-10-31 | 2012-02-21 | Honeywell International Inc. | Anisotropic bearing supports for turbochargers |
JP5136096B2 (ja) * | 2008-02-06 | 2013-02-06 | 株式会社Ihi | ターボ圧縮機及び冷凍機 |
US9353765B2 (en) | 2008-02-20 | 2016-05-31 | Trane International Inc. | Centrifugal compressor assembly and method |
US7856834B2 (en) * | 2008-02-20 | 2010-12-28 | 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 |
US20100175377A1 (en) * | 2009-01-12 | 2010-07-15 | Will Hippen | Cooling an electrically controlled turbocharger |
KR101645518B1 (ko) | 2009-04-20 | 2016-08-05 | 보르그워너 인코퍼레이티드 | 가변 볼류트 유동 체적들을 가지는 단순화된 가변 구조 터보차저 |
US8181462B2 (en) * | 2009-06-23 | 2012-05-22 | Honeywell International Inc. | Turbocharger with two-stage compressor, including a twin-wheel parallel-flow first stage |
CN102072200A (zh) * | 2010-12-31 | 2011-05-25 | 中国兵器工业集团第七○研究所 | 一种涡轮增压器压气机双层蜗壳结构 |
DE102011004345A1 (de) | 2011-02-17 | 2012-08-23 | Bayerische Motoren Werke Aktiengesellschaft | Abgasturbolader für eine Brennkraftmaschine |
EP2703620B1 (de) * | 2011-04-26 | 2015-07-01 | Toyota Jidosha Kabushiki Kaisha | Turbinengehäuse für einen turbolader |
US8888449B2 (en) | 2011-05-12 | 2014-11-18 | General Electric Company | System, transition conduit, and article of manufacture for delivering a fluid flow |
US8764376B2 (en) * | 2011-05-16 | 2014-07-01 | Honeywell International Inc. | Diffuser divider |
JP2012251528A (ja) * | 2011-06-07 | 2012-12-20 | Daikin Industries Ltd | 多段遠心圧縮機 |
CN102691678B (zh) * | 2012-06-11 | 2015-08-19 | 康跃科技股份有限公司 | 连续增压压气机 |
CN102840169B (zh) * | 2012-09-26 | 2015-03-18 | 北京理工大学 | 一种用于产生两种不同压比的离心压气机 |
US9631625B2 (en) * | 2013-02-01 | 2017-04-25 | Honeywell International Inc. | Axial turbine with statorless inlet formed by meridionally divided turbine housing and heat shroud |
US9726185B2 (en) | 2013-05-14 | 2017-08-08 | Honeywell International Inc. | Centrifugal compressor with casing treatment for surge control |
DE102013216608B4 (de) * | 2013-08-22 | 2017-05-11 | Ford Global Technologies, Llc | Abgasturboaufgeladene Brennkraftmaschine umfassend einen Verdichter mit zwei Laufrädern |
US10006290B2 (en) | 2013-08-27 | 2018-06-26 | Honeywell International Inc. | Functionally asymmetric two-sided turbocharger wheel and diffuser |
US10233756B2 (en) * | 2013-08-27 | 2019-03-19 | Garrett Transportation I Inc. | Two-sided turbocharger wheel with differing blade parameters |
US20150198163A1 (en) * | 2014-01-15 | 2015-07-16 | Honeywell International Inc. | Turbocharger With Twin Parallel Compressor Impellers And Having Center Housing Features For Conditioning Flow In The Rear Impeller |
WO2015195343A1 (en) * | 2014-06-20 | 2015-12-23 | Borgwarner Inc. | Turbocharger comprising a modular construction compressor housing |
US20170241433A1 (en) * | 2014-10-17 | 2017-08-24 | Nuovo Pignone Srl | Centrifugal turbomachine with two stages arranged back-to-back and with an annular transfer duct between the stages |
DE102014224283A1 (de) * | 2014-11-27 | 2016-06-02 | Robert Bosch Gmbh | Verdichter mit einem Dichtkanal |
DE102014224285A1 (de) * | 2014-11-27 | 2016-06-02 | Robert Bosch Gmbh | Verdichter mit einem Dichtkanal |
DE102014224757A1 (de) * | 2014-12-03 | 2016-06-09 | Robert Bosch Gmbh | Verdichter mit einem Dichtkanal |
US9856886B2 (en) * | 2015-01-08 | 2018-01-02 | Honeywell International Inc. | Multistage radial compressor baffle |
US9957975B2 (en) * | 2015-06-01 | 2018-05-01 | Corey B. Kuhns | Angular velocity stepping and methods of use in turbomachinery |
US9816512B2 (en) * | 2015-07-15 | 2017-11-14 | Borgwarner Inc. | Separated opposed flow single coupling compressor stage |
US9745992B2 (en) | 2015-08-30 | 2017-08-29 | Honeywell International Inc. | Turbocharger bearing damper assembly |
US10208986B2 (en) | 2016-01-15 | 2019-02-19 | Great Source Innovations Llc | Evaporative fluid cooling apparatuses and methods thereof |
US10030877B2 (en) | 2016-01-15 | 2018-07-24 | Gerald McDonnell | Air handler apparatuses for evaporative fluid cooling and methods thereof |
US10190596B2 (en) | 2016-11-03 | 2019-01-29 | Garrett Transportation I Inc. | Two-stage compressor with asymmetric second-stage inlet duct |
CN106382258A (zh) * | 2016-12-06 | 2017-02-08 | 深圳福世达动力科技有限公司 | 离心对转冲压压气机 |
US10458432B2 (en) * | 2017-04-25 | 2019-10-29 | Garrett Transportation I Inc. | Turbocharger compressor assembly with vaned divider |
CN107044434B (zh) * | 2017-05-09 | 2019-01-22 | 福建东亚环保科技股份有限公司 | 一种小型高压离心鼓风机 |
DE102017114232A1 (de) * | 2017-06-27 | 2018-12-27 | Ebm-Papst Mulfingen Gmbh & Co. Kg | Rückführgeometrie eines Turboverdichters |
DE102017218295B4 (de) * | 2017-10-12 | 2020-08-20 | Vitesco Technologies GmbH | Verdichter für einen Turbolader einer Brennkraftmaschine sowie Turbolader für eine Brennkraftmaschine |
DE102021127331A1 (de) * | 2021-10-21 | 2023-04-27 | Ihi Charging Systems International Gmbh | Aufladesystem einer Brennstoffzelle |
US11885349B1 (en) * | 2022-08-18 | 2024-01-30 | Pratt & Whitney Canada Corp. | Compressor having a dual-impeller |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1023864A (fr) * | 1950-07-19 | 1953-03-25 | Turbo-soufflante de suralimentation pour des moteurs à combustion et son procédé de montage | |
GB1082792A (en) * | 1963-05-20 | 1967-09-13 | British Ship Res Ass | A supercharger for an internal combustion engine |
US3751178A (en) * | 1971-10-06 | 1973-08-07 | Warren Pumps Inc | Pump |
CH584351A5 (de) * | 1974-12-18 | 1977-01-31 | Bbc Brown Boveri & Cie | |
US4155684A (en) * | 1975-10-17 | 1979-05-22 | Bbc Brown Boveri & Company Limited | Two-stage exhaust-gas turbocharger |
US4231702A (en) * | 1979-08-24 | 1980-11-04 | Borg-Warner Corporation | Two-stage turbo compressor |
DE3041093A1 (de) * | 1980-10-31 | 1982-06-09 | Atlas Copco AB, Nacka | Rotor fuer einen zweistufigen oder mehr als zweistufigen radialverdichter |
US5697767A (en) * | 1991-08-23 | 1997-12-16 | Boeing North American, Inc. | Integrated turbine and pump assembly |
-
1998
- 1998-07-02 US US09/109,538 patent/US6062028A/en not_active Expired - Lifetime
-
1999
- 1999-06-30 BR BR9911807-6A patent/BR9911807A/pt not_active IP Right Cessation
- 1999-06-30 DE DE69914199T patent/DE69914199T2/de not_active Expired - Lifetime
- 1999-06-30 AU AU47298/99A patent/AU4729899A/en not_active Abandoned
- 1999-06-30 WO PCT/US1999/014938 patent/WO2000001935A1/en active IP Right Grant
- 1999-06-30 KR KR1020017000006A patent/KR100588824B1/ko not_active IP Right Cessation
- 1999-06-30 EP EP99930851A patent/EP1092085B1/de not_active Expired - Lifetime
- 1999-06-30 CA CA002337790A patent/CA2337790C/en not_active Expired - Fee Related
- 1999-06-30 JP JP2000558303A patent/JP4317327B2/ja not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
CA2337790C (en) | 2007-10-09 |
KR20010053362A (ko) | 2001-06-25 |
JP2002519581A (ja) | 2002-07-02 |
CA2337790A1 (en) | 2000-01-13 |
US6062028A (en) | 2000-05-16 |
BR9911807A (pt) | 2002-03-12 |
EP1092085A1 (de) | 2001-04-18 |
EP1092085B1 (de) | 2004-01-14 |
WO2000001935A1 (en) | 2000-01-13 |
AU4729899A (en) | 2000-01-24 |
DE69914199T2 (de) | 2004-08-05 |
JP4317327B2 (ja) | 2009-08-19 |
KR100588824B1 (ko) | 2006-06-13 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |