RU2017121565A3 - - Google Patents

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Publication number
RU2017121565A3
RU2017121565A3 RU2017121565A RU2017121565A RU2017121565A3 RU 2017121565 A3 RU2017121565 A3 RU 2017121565A3 RU 2017121565 A RU2017121565 A RU 2017121565A RU 2017121565 A RU2017121565 A RU 2017121565A RU 2017121565 A3 RU2017121565 A3 RU 2017121565A3
Authority
RU
Russia
Application number
RU2017121565A
Other languages
Russian (ru)
Other versions
RU2017121565A (en
RU2693202C2 (en
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 filed Critical
Publication of RU2017121565A publication Critical patent/RU2017121565A/en
Publication of RU2017121565A3 publication Critical patent/RU2017121565A3/ru
Application granted granted Critical
Publication of RU2693202C2 publication Critical patent/RU2693202C2/en

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D2206/00Burners for specific applications
    • F23D2206/10Turbines

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Nozzles For Spraying Of Liquid Fuel (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
RU2017121565A 2014-11-21 2015-11-20 Tubular injector for fuel injection into combustion chamber of gas turbine RU2693202C2 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
ITMI2014A002019 2014-11-21
ITMI20142019 2014-11-21
PCT/IB2015/059018 WO2016079720A1 (en) 2014-11-21 2015-11-20 Lance injector for injecting fuel into a combustion chamber of a gas turbine

Publications (3)

Publication Number Publication Date
RU2017121565A RU2017121565A (en) 2018-12-21
RU2017121565A3 true RU2017121565A3 (en) 2019-05-21
RU2693202C2 RU2693202C2 (en) 2019-07-01

Family

ID=52463031

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2017121565A RU2693202C2 (en) 2014-11-21 2015-11-20 Tubular injector for fuel injection into combustion chamber of gas turbine

Country Status (4)

Country Link
EP (1) EP3221642B1 (en)
CN (1) CN107110504B (en)
RU (1) RU2693202C2 (en)
WO (1) WO2016079720A1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114543118B (en) * 2022-02-21 2023-04-25 中国航发贵阳发动机设计研究所 Centrifugal starting nozzle

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB648699A (en) * 1947-10-17 1951-01-10 Arthur Holmes Fletcher Improvements in or relating to gas-turbine engine fuel systems and liquid fuel injectors therefor
US6357222B1 (en) * 2000-04-07 2002-03-19 General Electric Company Method and apparatus for reducing thermal stresses within turbine engines
US7703287B2 (en) * 2006-10-31 2010-04-27 Delavan Inc Dynamic sealing assembly to accommodate differential thermal growth of fuel injector components
RU2375597C2 (en) * 2008-02-12 2009-12-10 Открытое акционерное общество "Научно-производственное объединение "Сатурн" (ОАО "НПО "Сатурн") Gas turbine engine combustion chamber fuel manifold
US8443608B2 (en) * 2008-02-26 2013-05-21 Delavan Inc Feed arm for a multiple circuit fuel injector
EP2270398A1 (en) * 2009-06-30 2011-01-05 Siemens Aktiengesellschaft Burner, especially for gas turbines
US20130180261A1 (en) * 2012-01-13 2013-07-18 General Electric Company Combustor and method for reducing thermal stresses in a combustor

Also Published As

Publication number Publication date
RU2017121565A (en) 2018-12-21
CN107110504A (en) 2017-08-29
EP3221642A1 (en) 2017-09-27
CN107110504B (en) 2019-11-26
EP3221642B1 (en) 2018-09-05
WO2016079720A1 (en) 2016-05-26
RU2693202C2 (en) 2019-07-01

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