EA201190075A1 - Турбокомпрессор с выхлопным патрубком увеличивающегося поперечного сечения и способ турбонаддува - Google Patents

Турбокомпрессор с выхлопным патрубком увеличивающегося поперечного сечения и способ турбонаддува

Info

Publication number
EA201190075A1
EA201190075A1 EA201190075A EA201190075A EA201190075A1 EA 201190075 A1 EA201190075 A1 EA 201190075A1 EA 201190075 A EA201190075 A EA 201190075A EA 201190075 A EA201190075 A EA 201190075A EA 201190075 A1 EA201190075 A1 EA 201190075A1
Authority
EA
Eurasian Patent Office
Prior art keywords
turbocharger
turbo
surgery
transverse section
external tube
Prior art date
Application number
EA201190075A
Other languages
English (en)
Other versions
EA022179B1 (ru
Inventor
Дэниель Эдвард Лорингер
Энтони Холмс Фёрман
Кендалл Роджер Суэнсон
Дейл Уильям Ладун
Original Assignee
Дженерал Электрик Компани
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 Дженерал Электрик Компани filed Critical Дженерал Электрик Компани
Publication of EA201190075A1 publication Critical patent/EA201190075A1/ru
Publication of EA022179B1 publication Critical patent/EA022179B1/ru

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
    • 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
    • F01D9/026—Scrolls for radial machines or engines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/40—Application in turbochargers

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • General Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Supercharger (AREA)

Abstract

Предложена турбокомпрессорная установка (10), содержащая компрессор (26), турбину (28), вал (30), соединяющий компрессор с турбиной, и турбинный кожух (56), выполненный с возможностью улучшения восстановления давления и имеющий несимметричную геометрическую конфигурацию, которая обеспечивает улучшение потока, протекающего по направлению к выхлопному отверстию (83).
EA201190075A 2009-01-15 2010-01-11 Турбокомпрессор с выхлопным патрубком увеличивающегося поперечного сечения и способ турбонаддува EA022179B1 (ru)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US12/354,623 US20100178164A1 (en) 2009-01-15 2009-01-15 System and method for turbocharging an engine
PCT/US2010/020627 WO2010083126A1 (en) 2009-01-15 2010-01-11 A turbocharger with a increasing cross-section exhaust casing and a method for turbocharging

Publications (2)

Publication Number Publication Date
EA201190075A1 true EA201190075A1 (ru) 2012-02-28
EA022179B1 EA022179B1 (ru) 2015-11-30

Family

ID=42062005

Family Applications (1)

Application Number Title Priority Date Filing Date
EA201190075A EA022179B1 (ru) 2009-01-15 2010-01-11 Турбокомпрессор с выхлопным патрубком увеличивающегося поперечного сечения и способ турбонаддува

Country Status (7)

Country Link
US (2) US20100178164A1 (ru)
EP (1) EP2387657B1 (ru)
CN (1) CN102282345A (ru)
AU (1) AU2010204902C1 (ru)
BR (1) BRPI1004915B1 (ru)
EA (1) EA022179B1 (ru)
WO (1) WO2010083126A1 (ru)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8959913B2 (en) 2011-09-15 2015-02-24 General Electric Company Systems and apparatus for transferring fluid flow
US9771864B2 (en) * 2012-05-31 2017-09-26 General Electric Company Gas turbine compressor inlet pressurization and flow control system
US9181855B2 (en) * 2013-01-31 2015-11-10 Electro-Motive Diesel, Inc. Turbocharger with axial turbine stage
JP5870083B2 (ja) 2013-12-27 2016-02-24 三菱重工業株式会社 タービン
US9689397B2 (en) 2014-06-13 2017-06-27 GM Global Technology Operations LLC Turbine outlet diffuser
CN104500156B (zh) * 2014-12-29 2017-05-17 无锡康明斯涡轮增压技术有限公司 蜗壳出口结构
DE102016205257A1 (de) * 2015-04-09 2016-10-13 Borgwarner Inc., Patent Department Abgas-zuführanordnung eines abgasturboladers
CN109563770B (zh) * 2016-12-28 2021-05-18 三菱重工发动机和增压器株式会社 涡轮机及涡轮增压器

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2465846A (en) * 1944-12-01 1949-03-29 Cons Vultee Aircraft Corp Hood structure for aircraft engine turbosuperchargers
BE473291A (ru) * 1946-05-10
US3355878A (en) * 1965-08-30 1967-12-05 Birmann Rudolph Turbocompressor system
US5011371A (en) * 1987-04-29 1991-04-30 General Motors Corporation Centrifugal compressor/pump with fluid dynamically variable geometry diffuser
US6302647B1 (en) * 2000-05-10 2001-10-16 General Motors Corporation Turbine inlet scroll
US7207176B2 (en) * 2002-11-19 2007-04-24 Cummins Inc. Method of controlling the exhaust gas temperature for after-treatment systems on a diesel engine using a variable geometry turbine
EP1625291B1 (en) * 2003-05-15 2009-03-18 Volvo Lastvagnar Ab Turbo compressor system for an internal combustion engine comprising a compressor of radial type and provides with an impeller with backswept blades
US6945748B2 (en) * 2004-01-22 2005-09-20 Electro-Motive Diesel, Inc. Centrifugal compressor with channel ring defined inlet recirculation channel
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
US20080229742A1 (en) * 2007-03-21 2008-09-25 Philippe Renaud Extended Leading-Edge Compressor Wheel
US8328506B2 (en) 2008-12-04 2012-12-11 General Electric Company Optimized turbocharger bearing system

Also Published As

Publication number Publication date
AU2010204902A1 (en) 2011-07-28
WO2010083126A1 (en) 2010-07-22
US20100178164A1 (en) 2010-07-15
BRPI1004915B1 (pt) 2020-07-21
BRPI1004915A2 (pt) 2016-06-28
US20130052054A1 (en) 2013-02-28
CN102282345A (zh) 2011-12-14
EP2387657A1 (en) 2011-11-23
US9003790B2 (en) 2015-04-14
EA022179B1 (ru) 2015-11-30
EP2387657B1 (en) 2019-01-02
AU2010204902C1 (en) 2013-07-25
AU2010204902B2 (en) 2013-02-28

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