GB1315307A - Turbo superchargers for internal combustion engines - Google Patents
Turbo superchargers for internal combustion enginesInfo
- Publication number
- GB1315307A GB1315307A GB1315307DA GB1315307A GB 1315307 A GB1315307 A GB 1315307A GB 1315307D A GB1315307D A GB 1315307DA GB 1315307 A GB1315307 A GB 1315307A
- Authority
- GB
- United Kingdom
- Prior art keywords
- casing
- compressor
- turbine
- air
- parts
- 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
- 238000002485 combustion reaction Methods 0.000 title abstract 2
- 229910052581 Si3N4 Inorganic materials 0.000 abstract 1
- HQVNEWCFYHHQES-UHFFFAOYSA-N silicon nitride Chemical compound N12[Si]34N5[Si]62N3[Si]51N64 HQVNEWCFYHHQES-UHFFFAOYSA-N 0.000 abstract 1
Classifications
-
- 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
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
-
- 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
- F01D25/18—Lubricating arrangements
- F01D25/22—Lubricating arrangements using working-fluid or other gaseous fluid as lubricant
-
- 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
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)
Abstract
1315307 Turbo-superchargers CAV Ltd 10 Aug 1970 [21 Aug 1969] 41798/69 Heading F1G The invention relates to a turbo supercharger for an internal combustion engine and comprises a radial inward flow turbine 12 and a centrifugal compressor 14, the turbine rotor 19 and the compressor rotor being mounted at the ends of shaft 20. The shaft is mounted in a bearing housing 24 which is formed with an annular recess 25 to which air under pressure is supplied through ducts 29 in the compressor casing, the air passing through passages in a bearing sleeve 23 so as to form an air journal bearing; air also passes from the recess 25 to the rearward sides of the turbine and compressor rotors so as to form air thrust bearings. The bearing housing 24 is received within a casing 27 which is formed in two parts, one part comprising part of the turbine casing 13 and the other part comprising part of the compressor casing 15. The bearing housing is formed with stepped end portions which are received by corresponding portions of the casing parts. The casing parts 27 are held together by an annular clip 28 engaging flange portions of the casing parts. The turbine casing is formed with an axial outlet 16 and the compressor casing with an axial inlet 17. The turbine rotor blades and the bearing sleeve are formed of silicon nitride.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB4179869 | 1969-08-21 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1315307A true GB1315307A (en) | 1973-05-02 |
Family
ID=10421416
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1315307D Expired GB1315307A (en) | 1969-08-21 | 1969-08-21 | Turbo superchargers for internal combustion engines |
Country Status (2)
Country | Link |
---|---|
FR (1) | FR2059032A5 (en) |
GB (1) | GB1315307A (en) |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2948398A1 (en) * | 1979-12-01 | 1981-06-04 | Skf Kugellagerfabriken Gmbh, 8720 Schweinfurt | EXHAUST TURBOCHARGER |
DE3328022A1 (en) * | 1982-08-27 | 1984-03-01 | Nissan Motor Co., Ltd., Yokohama, Kanagawa | TURBOCHARGER |
US5403165A (en) * | 1992-11-30 | 1995-04-04 | Societe Europeenne De Propulsion | Compact high power turbopump for a rocket engine |
US5465482A (en) * | 1993-09-03 | 1995-11-14 | Abb Management Ag | Method for matching the flow capacity of a radial turbine of a turbocharger to a capacity of an internal combustion engine |
US5567129A (en) * | 1995-05-25 | 1996-10-22 | Bonardi; G. Fonda | Thrust control system for gas-bearing turbocompressors |
WO2002086293A1 (en) * | 2001-04-19 | 2002-10-31 | Honeywell International Inc. | Improved turbocharger bearing system |
EP1394366A1 (en) * | 2002-09-02 | 2004-03-03 | BorgWarner Inc. | Turbomachine housing |
WO2004046519A1 (en) * | 2002-11-20 | 2004-06-03 | Honeywell International Inc. | Sequential turbocharging system and a method for sequential turbocharging of an internal combustion engine |
WO2005045201A1 (en) | 2003-11-04 | 2005-05-19 | Mann + Hummel Gmbh | Non-positive-displacement machine comprising a spiral channel provided in the housing middle part |
DE102008057729A1 (en) * | 2008-11-17 | 2010-05-27 | Bosch Mahle Turbo Systems Gmbh & Co. Kg | Exhaust gas turbo-charger for internal combustion engine in motor vehicle, has rotor supported in stator via pneumatic radial bearing and axial bearing, where radial bearing is pneumatically loaded by rotor, during operation of charger |
CN102650296A (en) * | 2012-06-11 | 2012-08-29 | 重庆江增船舶重工有限公司 | High-speed and small-flow centrifugal type compressor set |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4474007A (en) * | 1980-09-29 | 1984-10-02 | Ab Volvo | Turbocharging device for an internal combustion engine |
FR2533627B1 (en) * | 1982-09-28 | 1985-10-25 | Chausson Usines Sa | TURBO-MACHINE DRIVEN BY THE EXHAUST GASES OF A THERMAL ENGINE SUPPLIED TO THE SAID MACHINE BY TWO SEPARATE EXHAUST MANIFOLDS |
GB2153437A (en) * | 1984-01-07 | 1985-08-21 | Rolls Royce | Improvements in or relating to gas turbine power plant |
-
1969
- 1969-08-21 GB GB1315307D patent/GB1315307A/en not_active Expired
-
1970
- 1970-08-20 FR FR7030573A patent/FR2059032A5/fr not_active Expired
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2948398A1 (en) * | 1979-12-01 | 1981-06-04 | Skf Kugellagerfabriken Gmbh, 8720 Schweinfurt | EXHAUST TURBOCHARGER |
DE3328022A1 (en) * | 1982-08-27 | 1984-03-01 | Nissan Motor Co., Ltd., Yokohama, Kanagawa | TURBOCHARGER |
US5403165A (en) * | 1992-11-30 | 1995-04-04 | Societe Europeenne De Propulsion | Compact high power turbopump for a rocket engine |
US5465482A (en) * | 1993-09-03 | 1995-11-14 | Abb Management Ag | Method for matching the flow capacity of a radial turbine of a turbocharger to a capacity of an internal combustion engine |
US5567129A (en) * | 1995-05-25 | 1996-10-22 | Bonardi; G. Fonda | Thrust control system for gas-bearing turbocompressors |
WO2002086293A1 (en) * | 2001-04-19 | 2002-10-31 | Honeywell International Inc. | Improved turbocharger bearing system |
EP1394366A1 (en) * | 2002-09-02 | 2004-03-03 | BorgWarner Inc. | Turbomachine housing |
WO2004046519A1 (en) * | 2002-11-20 | 2004-06-03 | Honeywell International Inc. | Sequential turbocharging system and a method for sequential turbocharging of an internal combustion engine |
WO2005045201A1 (en) | 2003-11-04 | 2005-05-19 | Mann + Hummel Gmbh | Non-positive-displacement machine comprising a spiral channel provided in the housing middle part |
US8062006B2 (en) | 2003-11-04 | 2011-11-22 | Mann + Hummel Gmbh | Non-positive-displacement machine comprising a spiral channel provided in the housing middle part |
DE102008057729A1 (en) * | 2008-11-17 | 2010-05-27 | Bosch Mahle Turbo Systems Gmbh & Co. Kg | Exhaust gas turbo-charger for internal combustion engine in motor vehicle, has rotor supported in stator via pneumatic radial bearing and axial bearing, where radial bearing is pneumatically loaded by rotor, during operation of charger |
CN102650296A (en) * | 2012-06-11 | 2012-08-29 | 重庆江增船舶重工有限公司 | High-speed and small-flow centrifugal type compressor set |
Also Published As
Publication number | Publication date |
---|---|
FR2059032A5 (en) | 1971-05-28 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US6062028A (en) | Low speed high pressure ratio turbocharger | |
US4490622A (en) | Turbocharger and adaptations thereof | |
US3526092A (en) | Gas turbine engine having improved bearing support means for concentric shafts | |
GB1436347A (en) | Turbocharger | |
GB1315307A (en) | Turbo superchargers for internal combustion engines | |
GB1463722A (en) | Gas turbine engines | |
GB1497006A (en) | Turbochargers | |
GB775454A (en) | Improvements in or relating to engine supercharging device | |
KR20030029992A (en) | Rotor and bearing system for electrically assisted turbocharger | |
GB1141816A (en) | Improvements in turbofan engines having contra-rotating compressors | |
GB1497477A (en) | Gas turbine engine | |
GB905136A (en) | Improvements relating to gas turbine power units | |
GB609926A (en) | Improvements in or relating to internal-combustion turbines | |
GB1003740A (en) | Helicopter rotor | |
GB666416A (en) | Gas turbine power plant for jet propulsion | |
GB777582A (en) | Improvements in or relating to pressure chargers for internal combustion engines | |
GB1256486A (en) | ||
GB511597A (en) | Improvements in or relating to gas turbine driven blowers | |
US3179328A (en) | Turbo-compressors | |
GB1257497A (en) | ||
US3090546A (en) | Pressurized oil seal for rotating machinery | |
GB1018538A (en) | Gas turbine engine | |
US2700935A (en) | Rocket fuel pump and the like | |
GB1455942A (en) | Gas turbine engines | |
GB1141001A (en) | Improvements in gas turbine engines |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
PLNP | Patent lapsed through nonpayment of renewal fees |