GB1510070A - Two-stage exhaust-gas turbocharger with two coaxial shafts one inside the other - Google Patents
Two-stage exhaust-gas turbocharger with two coaxial shafts one inside the otherInfo
- Publication number
- GB1510070A GB1510070A GB42897/76A GB4289776A GB1510070A GB 1510070 A GB1510070 A GB 1510070A GB 42897/76 A GB42897/76 A GB 42897/76A GB 4289776 A GB4289776 A GB 4289776A GB 1510070 A GB1510070 A GB 1510070A
- Authority
- GB
- United Kingdom
- Prior art keywords
- shaft
- compressor
- turbine
- bearings
- carrying
- 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
Links
- 230000000712 assembly Effects 0.000 abstract 2
- 238000000429 assembly Methods 0.000 abstract 2
- 230000003584 silencer Effects 0.000 abstract 1
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
- F04D17/00—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
- F04D17/08—Centrifugal pumps
- F04D17/10—Centrifugal pumps for compressing or evacuating
- F04D17/12—Multi-stage pumps
- F04D17/122—Multi-stage pumps the individual rotor discs being, one for each stage, on a common shaft and axially spaced, e.g. conventional centrifugal multi- stage compressors
- F04D17/125—Multi-stage pumps the individual rotor discs being, one for each stage, on a common shaft and axially spaced, e.g. conventional centrifugal multi- stage compressors the casing being vertically split
-
- 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
- F02B37/004—Engines characterised by provision of pumps driven at least for part of the time by exhaust with exhaust drives arranged in series
-
- 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
- F02B37/007—Engines characterised by provision of pumps driven at least for part of the time by exhaust with exhaust-driven pumps arranged in parallel, e.g. at least one pump supplying alternatively
-
- 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
- F02B37/013—Engines characterised by provision of pumps driven at least for part of the time by exhaust with exhaust-driven pumps arranged in series
-
- 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
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
- Chemical Kinetics & Catalysis (AREA)
- General Chemical & Material Sciences (AREA)
- Supercharger (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH1348975A CH594132A5 (ja) | 1975-10-17 | 1975-10-17 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1510070A true GB1510070A (en) | 1978-05-10 |
Family
ID=4392877
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB42897/76A Expired GB1510070A (en) | 1975-10-17 | 1976-10-15 | Two-stage exhaust-gas turbocharger with two coaxial shafts one inside the other |
Country Status (6)
Country | Link |
---|---|
JP (1) | JPS5250412A (ja) |
CH (1) | CH594132A5 (ja) |
DE (1) | DE2550054A1 (ja) |
DK (1) | DK456476A (ja) |
FR (1) | FR2328122A1 (ja) |
GB (1) | GB1510070A (ja) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2277129A (en) * | 1993-04-13 | 1994-10-19 | Daimler Benz Ag | Exhaust gas turbocharger |
GB2305974A (en) * | 1995-06-10 | 1997-04-23 | Adrian Graham Alford | Reducing turbocharger lag |
GB2349427A (en) * | 1999-04-21 | 2000-11-01 | Alstom Gas Turbines Ltd | Multi-stage turbocharger having coaxial shafts |
EP1191216A2 (en) * | 2000-09-21 | 2002-03-27 | Caterpillar Inc. | Turbocharger with exhaust gas recirculation |
EP1394380B1 (de) * | 2002-08-30 | 2009-04-08 | Borgwarner, Inc. | Aufladesystem für eine Brennkraftmaschine |
US7571607B2 (en) | 2006-03-06 | 2009-08-11 | Honeywell International Inc. | Two-shaft turbocharger |
CN105264199A (zh) * | 2013-06-05 | 2016-01-20 | 曼柴油机和涡轮机欧洲股份公司 | 用于增压设备的组合系统以及增压设备 |
US9458800B2 (en) | 2012-03-12 | 2016-10-04 | Jaguar Land Rover Limited | Turbo pump |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS58184357U (ja) * | 1982-06-04 | 1983-12-08 | 三菱重工業株式会社 | 充電装置 |
JPH01146702U (ja) * | 1988-03-16 | 1989-10-11 | ||
DE19948220A1 (de) * | 1999-10-06 | 2001-01-25 | Daimler Chrysler Ag | Brennkraftmaschine mit zwei Abgasturboladern |
DE102005056797A1 (de) * | 2005-11-29 | 2007-05-31 | Man Diesel Se | Zweistufiges Aufladungssystem |
DE102007017843A1 (de) * | 2007-04-16 | 2008-11-06 | Siemens Ag | Turboladeranordnung |
DE102017006974A1 (de) | 2017-07-22 | 2019-01-24 | Daimler Ag | Abgasturboladervorrichtung für eine Verbrennungskraftmaschine |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR870710A (fr) * | 1940-03-09 | 1942-03-23 | Bmw Flugmotorenbau Gmbh | Turbine à gaz d'échappement pour la commande d'un compresseur de charge en combinaison avec un moteur d'avion pour vol d'altitude |
USRE24810E (en) * | 1952-04-30 | 1960-04-19 | Alfred Buchi | Turbine driven multi-stage blower or pump |
US2839005A (en) * | 1953-10-14 | 1958-06-17 | Herbert E Means | Turbine driven pump |
FR1199567A (fr) * | 1957-03-15 | 1959-12-15 | Daimler Benz Ag | Compresseur axial |
FR1431473A (fr) * | 1965-04-14 | 1966-03-11 | Prvni Brnenska Strojirna Zd Y | Turbocompresseur avec turbine radiale |
-
1975
- 1975-10-17 CH CH1348975A patent/CH594132A5/xx not_active IP Right Cessation
- 1975-11-07 DE DE19752550054 patent/DE2550054A1/de not_active Withdrawn
-
1976
- 1976-10-11 DK DK456476A patent/DK456476A/da unknown
- 1976-10-15 GB GB42897/76A patent/GB1510070A/en not_active Expired
- 1976-10-15 JP JP51123025A patent/JPS5250412A/ja active Pending
- 1976-10-15 FR FR7631180A patent/FR2328122A1/fr active Pending
Cited By (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2277129A (en) * | 1993-04-13 | 1994-10-19 | Daimler Benz Ag | Exhaust gas turbocharger |
US5406796A (en) * | 1993-04-13 | 1995-04-18 | Mercedes-Benz Ag | Exhaust gas turbocharger for a supercharged internal combustion engine |
GB2277129B (en) * | 1993-04-13 | 1997-11-05 | Daimler Benz Ag | Exhaust gas turbocharger for an internal combustion engine |
GB2305974A (en) * | 1995-06-10 | 1997-04-23 | Adrian Graham Alford | Reducing turbocharger lag |
GB2305974B (en) * | 1995-06-10 | 1999-08-11 | Adrian Graham Alford | Device for improving turbocharger dynamic characteristics |
GB2349427A (en) * | 1999-04-21 | 2000-11-01 | Alstom Gas Turbines Ltd | Multi-stage turbocharger having coaxial shafts |
EP1191216A2 (en) * | 2000-09-21 | 2002-03-27 | Caterpillar Inc. | Turbocharger with exhaust gas recirculation |
EP1191216A3 (en) * | 2000-09-21 | 2003-08-13 | Caterpillar Inc. | Turbocharger with exhaust gas recirculation |
EP1394380B1 (de) * | 2002-08-30 | 2009-04-08 | Borgwarner, Inc. | Aufladesystem für eine Brennkraftmaschine |
US7571607B2 (en) | 2006-03-06 | 2009-08-11 | Honeywell International Inc. | Two-shaft turbocharger |
US9458800B2 (en) | 2012-03-12 | 2016-10-04 | Jaguar Land Rover Limited | Turbo pump |
CN105264199A (zh) * | 2013-06-05 | 2016-01-20 | 曼柴油机和涡轮机欧洲股份公司 | 用于增压设备的组合系统以及增压设备 |
CN105264199B (zh) * | 2013-06-05 | 2018-01-02 | 曼柴油机和涡轮机欧洲股份公司 | 用于增压设备的组合系统以及增压设备 |
Also Published As
Publication number | Publication date |
---|---|
DE2550054A1 (de) | 1977-04-21 |
JPS5250412A (en) | 1977-04-22 |
FR2328122A1 (fr) | 1977-05-13 |
CH594132A5 (ja) | 1977-12-30 |
DK456476A (da) | 1977-04-18 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
PCNP | Patent ceased through non-payment of renewal fee |