SU419147A1 - Turbocharger - Google Patents
TurbochargerInfo
- Publication number
- SU419147A1 SU419147A1 SU1896452A SU1896452A SU419147A1 SU 419147 A1 SU419147 A1 SU 419147A1 SU 1896452 A SU1896452 A SU 1896452A SU 1896452 A SU1896452 A SU 1896452A SU 419147 A1 SU419147 A1 SU 419147A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- turbocharger
- gas
- turbine
- bearing support
- flange
- Prior art date
Links
- 238000002485 combustion reaction Methods 0.000 description 1
- 230000008030 elimination Effects 0.000 description 1
- 238000003379 elimination reaction Methods 0.000 description 1
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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- General Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Supercharger (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Description
1one
Изобретение относитс к турбомашиностроекию , а именно к конструкции турбокомпрессоров ДЛЯ наддува двигателей Енутреннего сгорани .The invention relates to a turbomachine building, namely to the design of turbochargers for pressurization of engines of internal combustion.
Известны турбокомпрессоры с газоприемным неохлаждаемым корпусом, содержащие рабочие колеса турбины и компрессора, установленные в подшипниковых опорах, размещенных на концах общего вала.Known turbocompressors with gas-cooled uncooled housing, containing turbine and compressor impellers mounted in bearing supports located at the ends of the common shaft.
Предлагаемый турбокомпрессор отличаетс от известных тем, что подщипникова опора со стороны турбины соединена с фланцем газоприемного корпуса при помощи жестких радиальных элементов .The proposed turbocharger differs from the known ones in that the bearing support on the turbine side is connected to the flange of the gas receiving unit by means of rigid radial elements.
Такое вьшолненне турбокомпрессора позволит повысить его надежность.Such a complete turbocharger will improve its reliability.
На фиг. 1 схематически изображен описьюаемый турбокомпрессор, продольный разрез; на фиг. 2 - вид по стрелке А на фиг. 1.FIG. 1 shows a schematic view of a turbocharger to be described, longitudinal section; in fig. 2 is a view along arrow A in FIG. one.
Описьтаемый турбокомпрессор с газоприемным неохлаждаемым корпусом 1 содержит рабочие колеса 2 и 3 турбины и компрессора соответственно , установленные в подлшшнкковых опорах 4 и 5, размещенных на концах общего вала 6. Подшипникова опора 4 со стороны турбины соединена с фланцем 1 газоприемного корпуса 1 при помощи жестких радиальных элементов 8. Эти элементы предотвращают возникновение перекосов и несоосности подшипниковой опоры, что повышает надежность турбокомпрессора вследствие исключени возможности передачи тепловых деформаций корпуса 1 наподнпшниковуюопору 4.The described turbocharger with a gas-intake non-cooled body 1 contains impellers 2 and 3 of the turbine and compressor, respectively, mounted in podshlinkkovyh supports 4 and 5, placed at the ends of the common shaft 6. Bearing support 4 from the turbine side is connected to the flange 1 of the gas-receiving housing 1 by means of rigid radial elements 8. These elements prevent the occurrence of distortions and misalignment of the bearing support, which increases the reliability of the turbocharger due to the elimination of the possibility of transferring thermal deformations to rpusa 1 podnapshnikovuyu support 4.
Форму.ч а изобретени Form.h and inventions
15Турбокомпрессор с газоприемным неохлаждаемым корпусом, содержащий рабочие колеса турбины и компрессора, установленные в подщипниковых опорах, размещегпгые на концах общего вала, отличающийс тем, что, с целью повыщени 15Turbocompressor with a gas-inlet non-cooled housing, containing turbine and compressor impellers installed in support bearings, placed at the ends of the common shaft, characterized in that, in order to increase
20 надежности, подшипникова опора со стороны турбины соещетена с фланцем газоприемного корпуса при помощи жестких радиальных элементов.20 reliability, bearing support from the side of the turbine is connected with the flange of the gas receiving housing with the help of rigid radial elements.
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU1896452A SU419147A1 (en) | 1973-04-04 | 1973-04-04 | Turbocharger |
DE19742407855 DE2407855A1 (en) | 1973-04-04 | 1974-02-19 | TURBO COMPRESSOR |
CS225674A CS165275B1 (en) | 1973-04-04 | 1974-03-29 | |
FR7411110A FR2224653B1 (en) | 1973-04-04 | 1974-03-29 | |
IT4998174A IT1035532B (en) | 1973-04-04 | 1974-04-02 | TURBODOMPRESSOR |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU1896452A SU419147A1 (en) | 1973-04-04 | 1973-04-04 | Turbocharger |
Publications (1)
Publication Number | Publication Date |
---|---|
SU419147A1 true SU419147A1 (en) | 1976-09-05 |
Family
ID=20546299
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU1896452A SU419147A1 (en) | 1973-04-04 | 1973-04-04 | Turbocharger |
Country Status (5)
Country | Link |
---|---|
CS (1) | CS165275B1 (en) |
DE (1) | DE2407855A1 (en) |
FR (1) | FR2224653B1 (en) |
IT (1) | IT1035532B (en) |
SU (1) | SU419147A1 (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS58564B2 (en) * | 1976-08-03 | 1983-01-07 | 三菱重工業株式会社 | exhaust turbine supercharger |
US4149832A (en) * | 1977-08-11 | 1979-04-17 | Sivolap Georgy P | Turbocompressor |
DE102015209365A1 (en) * | 2015-05-21 | 2016-11-24 | Bosch Mahle Turbo Systems Gmbh & Co. Kg | turbocharger |
-
1973
- 1973-04-04 SU SU1896452A patent/SU419147A1/en active
-
1974
- 1974-02-19 DE DE19742407855 patent/DE2407855A1/en active Pending
- 1974-03-29 CS CS225674A patent/CS165275B1/cs unknown
- 1974-03-29 FR FR7411110A patent/FR2224653B1/fr not_active Expired
- 1974-04-02 IT IT4998174A patent/IT1035532B/en active
Also Published As
Publication number | Publication date |
---|---|
FR2224653B1 (en) | 1976-06-25 |
IT1035532B (en) | 1979-10-20 |
FR2224653A1 (en) | 1974-10-31 |
CS165275B1 (en) | 1975-12-22 |
DE2407855A1 (en) | 1974-10-17 |
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