SU419147A1 - Turbocharger - Google Patents

Turbocharger

Info

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
Application number
SU1896452A
Other languages
Russian (ru)
Inventor
Г.П. Сиволап
В.А. Потанин
Original Assignee
Специальное Конструкторское Бюро Турбонагнетателей Министерства Тяжолого Энергетического И Транспортного Машиностроения Ссср
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Специальное Конструкторское Бюро Турбонагнетателей Министерства Тяжолого Энергетического И Транспортного Машиностроения Ссср filed Critical Специальное Конструкторское Бюро Турбонагнетателей Министерства Тяжолого Энергетического И Транспортного Машиностроения Ссср
Priority to SU1896452A priority Critical patent/SU419147A1/en
Priority to DE19742407855 priority patent/DE2407855A1/en
Priority to CS225674A priority patent/CS165275B1/cs
Priority to FR7411110A priority patent/FR2224653B1/fr
Priority to IT4998174A priority patent/IT1035532B/en
Application granted granted Critical
Publication of SU419147A1 publication Critical patent/SU419147A1/en

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

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.

SU1896452A 1973-04-04 1973-04-04 Turbocharger SU419147A1 (en)

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)

* Cited by examiner, † Cited by third party
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

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

Similar Documents

Publication Publication Date Title
US7946809B2 (en) Exhaust-gas-turbine casing
EP3168429B1 (en) Turbine nozzle cartridge for use with a turbocharger core
US3759038A (en) Self aligning combustor and transition structure for a gas turbine
US4032262A (en) Housing arrangement for a two-stage exhaust-gas turbocharger
EP0095853B1 (en) A variable inlet area turbine
ES2300544T3 (en) COMPRESSOR DOWNLOAD HOUSING.
GB1533515A (en) Support for concentric turbine blade shroud
SE7607542L (en) COLLECTOR FOR RECEIPT, DENIREMENT AND DELIVERY OF THE EXHAUST CURRENT FROM A GAS TURBINE TYPE OR OTHER GAS GENERATING SYSTEM
CH399074A (en) Supercharging installation with a compressor driven by an exhaust gas turbine of an internal combustion engine
US5201796A (en) Gas turbine engine arrangement
ES195737U (en) A turbocompressor device operated by exhaust gases for use in relation to internal combustión engines. (Machine-translation by Google Translate, not legally binding)
GB1426554A (en) Turbo superchargers for internal combustion engines
GB1128432A (en) Turbine housing for turbochargers
ES402257A1 (en) Guide blade ring
SU419147A1 (en) Turbocharger
JPH0457849B2 (en)
SE9000874L (en) EXHAUST RESTAURANTS FOR COMBUSTION ENGINES WITH V-FORM CYLINDER
US6318961B1 (en) Axial turbine
FR2356811A1 (en) INTERNAL COMBUSTION ENGINE
US3765791A (en) Turbine nozzle support
GB1510070A (en) Two-stage exhaust-gas turbocharger with two coaxial shafts one inside the other
GB2063366A (en) Turbocharger and adaptions thereof
GB2036883A (en) Turbine Casing of Small-sized Turbocharger
US3797236A (en) Annular combustion chamber with ceramic annular ring
JP2707134B2 (en) Centering device