FR2360751A1 - Turbine a gaz, notamment turbosoufflante de suralimentation - Google Patents

Turbine a gaz, notamment turbosoufflante de suralimentation

Info

Publication number
FR2360751A1
FR2360751A1 FR7723219A FR7723219A FR2360751A1 FR 2360751 A1 FR2360751 A1 FR 2360751A1 FR 7723219 A FR7723219 A FR 7723219A FR 7723219 A FR7723219 A FR 7723219A FR 2360751 A1 FR2360751 A1 FR 2360751A1
Authority
FR
France
Prior art keywords
turbine
distributor
remove
gas turbine
order
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.)
Granted
Application number
FR7723219A
Other languages
English (en)
Other versions
FR2360751B1 (fr
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries Ltd
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 Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Publication of FR2360751A1 publication Critical patent/FR2360751A1/fr
Application granted granted Critical
Publication of FR2360751B1 publication Critical patent/FR2360751B1/fr
Granted legal-status Critical Current

Links

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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • 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)
  • Exhaust Silencers (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

Turbine à gaz. Elle comporte un corps de tubulure d'arrivée des gaz moteurs en deux parties de forme générale cylindrique 1A et 1B montées à coulissement l'une dans l'autre, le distributeur 2 de la turbine comportant les ailettes 3 de rotor étant supporté par la partie intérieure 1B en étant fixé par des boulons 32, de sorte que pour enlever le distributeur, il suffit de démonter les boulons d'assemblage 31 fixant la partie intérieure 1B à la partie extérieure 1A pour sortir le distributeur solidairement sans qu'il soit nécessaire de démonter les autres organes de la turbosoufflante pour le nettoyage ou l'entretien. Convient en particulier pour une turbosoufflante de suralimentation fonctionnant aux gaz d'échappement pour moteur Diesel.
FR7723219A 1976-08-03 1977-07-28 Turbine a gaz, notamment turbosoufflante de suralimentation Granted FR2360751A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP51092045A JPS58564B2 (ja) 1976-08-03 1976-08-03 排気タ−ビン過給機

Publications (2)

Publication Number Publication Date
FR2360751A1 true FR2360751A1 (fr) 1978-03-03
FR2360751B1 FR2360751B1 (fr) 1981-10-30

Family

ID=14043537

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7723219A Granted FR2360751A1 (fr) 1976-08-03 1977-07-28 Turbine a gaz, notamment turbosoufflante de suralimentation

Country Status (7)

Country Link
US (1) US4184812A (fr)
JP (1) JPS58564B2 (fr)
CH (1) CH622318A5 (fr)
DE (1) DE2734840A1 (fr)
DK (1) DK144195C (fr)
FR (1) FR2360751A1 (fr)
GB (1) GB1534850A (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0646699A1 (fr) * 1993-09-03 1995-04-05 ABB Management AG Procédé et appareil pour adapter la turbine radiale d'un turbocompresseur sur un moteur à combustion interne

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4850820A (en) * 1988-05-17 1989-07-25 Allied-Signal Inc. Exhaust gas driven turbocharger
DE19618314A1 (de) * 1996-05-08 1997-11-13 Asea Brown Boveri Abgasturbine eines Abgasturboladers
DE19618313B4 (de) * 1996-05-08 2005-07-21 Abb Turbo Systems Ag Axialturbine eines Abgasturboladers
JP4247214B2 (ja) * 2004-10-29 2009-04-02 三菱重工業株式会社 排気タービン過給機
DE102009045167A1 (de) 2009-09-30 2011-04-07 Man Diesel & Turbo Se Turbine eines Abgasturbolader
US8468826B2 (en) 2010-04-19 2013-06-25 Honeywell International Inc. Axial turbine wheel
US8353161B2 (en) 2010-04-19 2013-01-15 Honeywell International Inc. High diffusion turbine wheel with hub bulb
US8850813B2 (en) 2010-04-19 2014-10-07 Honeywell International Inc. Bearing housing shroud
US8453448B2 (en) 2010-04-19 2013-06-04 Honeywell International Inc. Axial turbine
US8453445B2 (en) 2010-04-19 2013-06-04 Honeywell International Inc. Axial turbine with parallel flow compressor
US9181855B2 (en) * 2013-01-31 2015-11-10 Electro-Motive Diesel, Inc. Turbocharger with axial turbine stage
EP3159504B1 (fr) * 2013-06-20 2021-03-03 Mitsubishi Heavy Industries, Ltd. Turbine axiale de type radiale et turbocompresseur de suralimentation
CN104863643B (zh) * 2015-04-22 2017-03-08 上海理工大学 径向离心透平
CN106801621B (zh) * 2015-11-25 2019-08-20 熵零股份有限公司 一种对转叶轮机构
CN106930786B (zh) * 2017-04-27 2020-07-28 西安交通大学 一种多级径流式对转涡轮结构
JP2019183716A (ja) * 2018-04-06 2019-10-24 トヨタ自動車株式会社 内燃機関
JP6939682B2 (ja) * 2018-04-06 2021-09-22 トヨタ自動車株式会社 内燃機関

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE970089C (de) * 1948-08-11 1958-08-21 Geraetebau Eberspaecher O H G Abgasturbolader fuer Kolbenmotoren mit Schutz gegen Waermeuebertragung
FR1017782A (fr) * 1949-03-08 1952-12-18 Napier & Son Ltd Perfectionnements aux pompes pour liquide
GB730870A (en) * 1951-05-05 1955-06-01 Walter Eberspacher Turbine-driven compressor
US2646210A (en) * 1951-05-05 1953-07-21 Eberspaecher J Turbocompressor
FR1225788A (fr) * 1959-02-18 1960-07-04 Perfectionnements apportés aux turbo-machines, notamment aux turbo-compresseurs, mues par des gaz d'échappement d'un moteur à combustion interne
NL126996C (fr) * 1964-03-16
SU419147A1 (ru) * 1973-04-04 1976-09-05 Специальное Конструкторское Бюро Турбонагнетателей Министерства Тяжолого Энергетического И Транспортного Машиностроения Ссср Турбокомпрессор

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0646699A1 (fr) * 1993-09-03 1995-04-05 ABB Management AG Procédé et appareil pour adapter la turbine radiale d'un turbocompresseur sur un moteur à combustion interne
RU2128779C1 (ru) * 1993-09-03 1999-04-10 Асеа Браун Бовери АГ Способ и устройство для совмещения радиальной турбины турбонагнетателя с двигателем внутреннего сгорания

Also Published As

Publication number Publication date
DE2734840A1 (de) 1978-02-09
CH622318A5 (fr) 1981-03-31
JPS58564B2 (ja) 1983-01-07
GB1534850A (en) 1978-12-06
DK144195C (da) 1982-08-09
US4184812A (en) 1980-01-22
DK144195B (da) 1982-01-11
FR2360751B1 (fr) 1981-10-30
JPS5317818A (en) 1978-02-18
DK347577A (da) 1978-02-04

Similar Documents

Publication Publication Date Title
FR2359973A1 (fr) Moteur a explosion muni d'un turbocompresseur de suralimentation a gaz d'echappement
FR2393999A1 (fr) Soupape de frein sur echappement
FR2444801A1 (fr) Structure de support pour le moyen d'etancheite entourant les ailettes du rotor d'un moteur a turbine a gaz
FR2440474A1 (fr) Moteur a turbine a gaz dont les elements critiques du rotor sont proteges contre le contact direct des gaz chauds
ES2055506T3 (es) Filtro de admision de aire para motores de combustion interna.
SE8400573L (sv) Reglerbar smorjmedelspump
FR2402060A1 (fr) Aube de turbomachine a dispositif de refroidissement perfectionne
FR2392226A1 (fr) Silencieux pour moteurs a combustion interne
AU3736495A (en) Resonance exhaust silencer
AU5981900A (en) Exhaust gas manifold
FR2528112B1 (fr) Dispositif de suralimentation pour moteur a combustion interne
FR2370896A1 (fr) Dispositif d'accouplement hydraulique a controle par temperature
DE3867318D1 (de) Abgasanlage mit schalldaempfer fuer eine brennkraftmaschine.
FR2431096A1 (fr) Dome de chambre de combustion de moteur a turbine a gaz
SE8904359D0 (sv) Skruvkompressor foer foerbraenningsmotorer
FR2433110A1 (fr) Diviseur de flux reglable pour turbomachines, notamment pour moteurs a reaction a turbines a gaz
FR2373673A1 (fr) Arbre de commande de moteur a combustion interne
FR2410136A2 (fr) Moteur a combustion a bruit reduit
FR2381910A2 (fr) Moteur a combustion a bruit reduit
DE3667522D1 (de) Turbokompressor fuer brennkraftmaschine.
ES2091534T3 (es) Disposicion de valvula para una retroalimentacion de gases de escape en un motor de combustion interna.
FR2369497A1 (fr) Dispositif d'accouplement de tuyauterie a compensation de dilatation thermique
FR2388140A1 (fr) Piston pour moteurs a explosion a pistons alternatifs, en particulier pour moteurs diesel
FR3117531B1 (fr) Ensemble de turbine
GB1506514A (en) Bearing assembly