GB0816393D0 - Turbomachine - Google Patents

Turbomachine

Info

Publication number
GB0816393D0
GB0816393D0 GBGB0816393.3A GB0816393A GB0816393D0 GB 0816393 D0 GB0816393 D0 GB 0816393D0 GB 0816393 A GB0816393 A GB 0816393A GB 0816393 D0 GB0816393 D0 GB 0816393D0
Authority
GB
United Kingdom
Prior art keywords
turbomachine
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
GBGB0816393.3A
Other versions
GB2463453B (en
GB2463453A (en
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.)
Cummins Turbo Technologies Ltd
Original Assignee
Cummins Turbo Technologies 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 Cummins Turbo Technologies Ltd filed Critical Cummins Turbo Technologies Ltd
Priority to GB0816393.3A priority Critical patent/GB2463453B/en
Publication of GB0816393D0 publication Critical patent/GB0816393D0/en
Priority to CN200910221464.4A priority patent/CN101709667A/en
Publication of GB2463453A publication Critical patent/GB2463453A/en
Application granted granted Critical
Publication of GB2463453B publication Critical patent/GB2463453B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/027—Arrangements for balancing
    • 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
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B39/00—Component parts, details, or accessories relating to, driven charging or scavenging pumps, not provided for in groups F02B33/00 - F02B37/00
    • F02B39/02—Drives of pumps; Varying pump drive gear ratio
    • F02B39/12—Drives characterised by use of couplings or clutches therein
    • 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
    • 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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
    • 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)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • General Chemical & Material Sciences (AREA)
  • Supercharger (AREA)
GB0816393.3A 2008-09-06 2008-09-06 Turbomachine Expired - Fee Related GB2463453B (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB0816393.3A GB2463453B (en) 2008-09-06 2008-09-06 Turbomachine
CN200910221464.4A CN101709667A (en) 2008-09-06 2009-09-07 Turbomachine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB0816393.3A GB2463453B (en) 2008-09-06 2008-09-06 Turbomachine

Publications (3)

Publication Number Publication Date
GB0816393D0 true GB0816393D0 (en) 2008-10-15
GB2463453A GB2463453A (en) 2010-03-17
GB2463453B GB2463453B (en) 2012-08-08

Family

ID=39888990

Family Applications (1)

Application Number Title Priority Date Filing Date
GB0816393.3A Expired - Fee Related GB2463453B (en) 2008-09-06 2008-09-06 Turbomachine

Country Status (2)

Country Link
CN (1) CN101709667A (en)
GB (1) GB2463453B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113423920A (en) * 2018-12-07 2021-09-21 赛峰直升机引擎公司 Turbomachine rotor with damping nut

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8529192B2 (en) * 2010-09-15 2013-09-10 Hamilton Sundstrand Corporation Thrust bearing shaft for thrust and journal air bearing cooling in a compressor
US8622620B2 (en) * 2010-09-15 2014-01-07 Hamilton Sundstrand Corporation Shaft for air bearing and motor cooling in compressor
WO2013074393A1 (en) * 2011-11-15 2013-05-23 Borgwarner Inc. Flow rotor, in particular turbine wheel
CN103842667B (en) * 2011-12-27 2016-05-18 三菱重工业株式会社 The axial rolling bearing of booster
JP5916377B2 (en) * 2011-12-27 2016-05-11 三菱重工業株式会社 Turbocharger turbine and supercharger assembly method
CN102562263A (en) * 2012-01-18 2012-07-11 潍坊富源增压器有限公司 Turbocharger
CN103362860A (en) * 2012-04-02 2013-10-23 珠海格力电器股份有限公司 High-speed fluid dynamic machine, and rotor forming method and assembling method thereof
CN105003302B (en) 2014-04-18 2017-04-12 松下知识产权经营株式会社 Turbomachine
US9771946B2 (en) * 2014-08-01 2017-09-26 Caterpillar Inc. Turbocharger compressor oil deflector and method
CN104696062B (en) * 2015-03-13 2017-05-24 费传华 One-shaft two-unit horizontal turbocharger for vehicle
CN105252201B (en) * 2015-10-19 2017-06-30 中航湖南通用航空发动机有限公司 A kind of unqualified rescue method of dynamic balancing of essence casting integral power turbine wheel
US10451085B2 (en) * 2016-10-05 2019-10-22 Borgwarner Inc. Assembly methods for the connection of a turbine wheel to a shaft
JP7261697B2 (en) * 2018-09-06 2023-04-20 エトスエナジー・イタリア・ソシエタ・ペル・アチオニ Method for repairing the rotor of a multi-stage axial compressor of a gas turbine

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB595669A (en) * 1942-04-27 1947-12-12 Power Jets Ltd Rotor assembly
DE3039961A1 (en) * 1980-10-23 1982-06-03 Volkswagenwerk Ag, 3180 Wolfsburg Exhaust turbocharger with ceramic turbine shaft - has ceramic shaft connected to metal compressor shaft with radial bearings
JPS6140879A (en) * 1984-08-03 1986-02-27 日本碍子株式会社 Metal ceramic bonded body and manufacture
DE3625996A1 (en) * 1986-07-31 1988-02-04 Kuehnle Kopp Kausch Ag Rotor for an exhaust turbocharger
JP3386559B2 (en) * 1993-05-11 2003-03-17 マツダ株式会社 Engine supercharger
KR100291057B1 (en) * 1997-08-29 2001-09-17 이계안 Exhaust turbine supercharger
US6499969B1 (en) * 2000-05-10 2002-12-31 General Motors Corporation Conically jointed turbocharger rotor
KR100373021B1 (en) * 2000-09-05 2003-02-25 현대자동차주식회사 Turbo-charger wherein a transmission is equiped
EP1353041A1 (en) * 2002-04-12 2003-10-15 ABB Turbo Systems AG Turbocharger with means on the shaft to axially restrain said shaft in the event of the compressor bursting
US6896479B2 (en) * 2003-04-08 2005-05-24 General Motors Corporation Turbocharger rotor

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113423920A (en) * 2018-12-07 2021-09-21 赛峰直升机引擎公司 Turbomachine rotor with damping nut
CN113423920B (en) * 2018-12-07 2023-08-11 赛峰直升机引擎公司 Turbine rotor with damping nut

Also Published As

Publication number Publication date
GB2463453B (en) 2012-08-08
GB2463453A (en) 2010-03-17
CN101709667A (en) 2010-05-19

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 20200906