GB727617A - Improvements in an exhaust gas turbine driven supercharger assembly for internal combustion engines - Google Patents
Improvements in an exhaust gas turbine driven supercharger assembly for internal combustion enginesInfo
- Publication number
- GB727617A GB727617A GB2757/53A GB275753A GB727617A GB 727617 A GB727617 A GB 727617A GB 2757/53 A GB2757/53 A GB 2757/53A GB 275753 A GB275753 A GB 275753A GB 727617 A GB727617 A GB 727617A
- Authority
- GB
- United Kingdom
- Prior art keywords
- driven supercharger
- grid
- exhaust gas
- gas turbine
- blower
- 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
Classifications
-
- 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
Abstract
727,617. Centrifugal fans. SOC. D'ETUDES DE MACHINES THIRMIQUES. July 11, 1951 [July 19, 1950], No. 2757/53. Divided out of 16452/51. Classes 110 (1). An exhaust gas turbine-driven supercharger for an internal-combustion engine has a blower body comprising at least one volute casing with a flared outlet pipe and grid means at the end of said pipe. The grid means may be a bank of cooler tubes. The turbine driven supercharger shown, Fig. 1, comprises a vertical shaft 1 journalled in bearings 2, 3. The shaft 1 carries two blower wheels 4, 5 to which air is supplied through a port 6 which acts as a silencer. The blower body comprises two volutes 8, Fig. 2, which are flared to a considerable extent, leading to two members 10 which direct the air to the inlet end of the second blower wheel 5. The members 10 are fitted with a grid of rods 11 which is is stated prevent the break-away of the fluid flow from the walls of the flared portion of the volute. The grid may be formed by a bank of cooler tubes.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1023864T | 1950-07-19 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB727617A true GB727617A (en) | 1955-04-06 |
Family
ID=9578516
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2757/53A Expired GB727617A (en) | 1950-07-19 | 1951-07-11 | Improvements in an exhaust gas turbine driven supercharger assembly for internal combustion engines |
Country Status (2)
Country | Link |
---|---|
FR (1) | FR1023864A (en) |
GB (1) | GB727617A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3316803A1 (en) * | 1983-04-23 | 1984-10-31 | Pohle + Rehling Gmbh, 4353 Oer-Erkenschwick | Underground tanker vehicle |
WO2000001935A1 (en) * | 1998-07-02 | 2000-01-13 | Alliedsignal Inc. | Low speed high pressure ratio turbocharger |
EP1191206A2 (en) | 2000-09-21 | 2002-03-27 | Caterpillar Inc. | Interstage cooling system of a multi-compressor turbocharger, engine and turbocharger comprising such a cooling system, and method of operating the turbocharger |
EP3318762A1 (en) * | 2016-11-03 | 2018-05-09 | Honeywell International Inc. | Two-stage compressor with asymmetric second-stage inlet duct |
EP2524144B1 (en) * | 2010-01-15 | 2018-10-10 | Dresser-Rand Company | Integral compressor-expander |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CH447979A (en) * | 1966-11-21 | 1967-11-30 | Charmilles Sa Ateliers | Hydraulic machine |
-
1950
- 1950-07-19 FR FR1023864D patent/FR1023864A/en not_active Expired
-
1951
- 1951-07-11 GB GB2757/53A patent/GB727617A/en not_active Expired
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3316803A1 (en) * | 1983-04-23 | 1984-10-31 | Pohle + Rehling Gmbh, 4353 Oer-Erkenschwick | Underground tanker vehicle |
WO2000001935A1 (en) * | 1998-07-02 | 2000-01-13 | Alliedsignal Inc. | Low speed high pressure ratio turbocharger |
EP1191206A2 (en) | 2000-09-21 | 2002-03-27 | Caterpillar Inc. | Interstage cooling system of a multi-compressor turbocharger, engine and turbocharger comprising such a cooling system, and method of operating the turbocharger |
EP2524144B1 (en) * | 2010-01-15 | 2018-10-10 | Dresser-Rand Company | Integral compressor-expander |
EP3318762A1 (en) * | 2016-11-03 | 2018-05-09 | Honeywell International Inc. | Two-stage compressor with asymmetric second-stage inlet duct |
CN108019362A (en) * | 2016-11-03 | 2018-05-11 | 霍尼韦尔国际公司 | Double-stage compressor with asymmetric second level inlet tube |
Also Published As
Publication number | Publication date |
---|---|
FR1023864A (en) | 1953-03-25 |
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