RU2012158330A - Газотурбинный двигатель и способ направления воздуха - Google Patents

Газотурбинный двигатель и способ направления воздуха Download PDF

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Publication number
RU2012158330A
RU2012158330A RU2012158330/06A RU2012158330A RU2012158330A RU 2012158330 A RU2012158330 A RU 2012158330A RU 2012158330/06 A RU2012158330/06 A RU 2012158330/06A RU 2012158330 A RU2012158330 A RU 2012158330A RU 2012158330 A RU2012158330 A RU 2012158330A
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RU
Russia
Prior art keywords
air
chamber
gas turbine
turbine engine
passage
Prior art date
Application number
RU2012158330/06A
Other languages
English (en)
Russian (ru)
Inventor
Лукас Джон СТОЙЯ
Патрик Бенедикт МЕЛТОН
Предраг Пея ПОПОВИЧ
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 RU2012158330A publication Critical patent/RU2012158330A/ru

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F23R3/045—Air inlet arrangements using pipes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/26—Controlling the air flow

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Control Of Turbines (AREA)
  • Supercharger (AREA)
RU2012158330/06A 2012-01-03 2012-12-27 Газотурбинный двигатель и способ направления воздуха RU2012158330A (ru)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/342,587 2012-01-03
US13/342,587 US9010082B2 (en) 2012-01-03 2012-01-03 Turbine engine and method for flowing air in a turbine engine

Publications (1)

Publication Number Publication Date
RU2012158330A true RU2012158330A (ru) 2014-07-10

Family

ID=47603023

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2012158330/06A RU2012158330A (ru) 2012-01-03 2012-12-27 Газотурбинный двигатель и способ направления воздуха

Country Status (5)

Country Link
US (1) US9010082B2 (enExample)
EP (1) EP2613085B1 (enExample)
JP (1) JP6134508B2 (enExample)
CN (1) CN103184899B (enExample)
RU (1) RU2012158330A (enExample)

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JP3125279B2 (ja) 1991-02-25 2001-01-15 東海カーボン株式会社 真空蒸着用黒鉛ルツボ
US9097424B2 (en) * 2012-03-12 2015-08-04 General Electric Company System for supplying a fuel and working fluid mixture to a combustor
US9151500B2 (en) 2012-03-15 2015-10-06 General Electric Company System for supplying a fuel and a working fluid through a liner to a combustion chamber
US9284888B2 (en) * 2012-04-25 2016-03-15 General Electric Company System for supplying fuel to late-lean fuel injectors of a combustor
US9376961B2 (en) * 2013-03-18 2016-06-28 General Electric Company System for controlling a flow rate of a compressed working fluid to a combustor fuel injector
CA2933539C (en) 2013-12-23 2022-01-18 General Electric Company Fuel nozzle with flexible support structures
US10451282B2 (en) 2013-12-23 2019-10-22 General Electric Company Fuel nozzle structure for air assist injection
US9803555B2 (en) * 2014-04-23 2017-10-31 General Electric Company Fuel delivery system with moveably attached fuel tube
CN104374438B (zh) * 2014-10-27 2017-09-19 哈尔滨汽轮机厂有限责任公司 轻型燃气轮机燃烧室喷嘴的气流检测方法
CN104481927A (zh) * 2014-12-12 2015-04-01 常州环能涡轮动力股份有限公司 具有双面离心压轮微型涡轮喷气发动机的导流环
US10788212B2 (en) * 2015-01-12 2020-09-29 General Electric Company System and method for an oxidant passageway in a gas turbine system with exhaust gas recirculation
US10253690B2 (en) 2015-02-04 2019-04-09 General Electric Company Turbine system with exhaust gas recirculation, separation and extraction
US10030538B2 (en) 2015-11-05 2018-07-24 General Electric Company Gas turbine engine with a vane having a cooling air turning nozzle
IT201600127713A1 (it) * 2016-12-16 2018-06-16 Ansaldo Energia Spa Gruppo bruciatore per un impianto a turbina a gas, impianto a turbina a gas comprendente detto gruppo bruciatore e metodo per operare detto impianto
CN109945234A (zh) * 2019-04-17 2019-06-28 新奥能源动力科技（上海）有限公司 一种单筒燃烧室及燃气轮机
KR102164620B1 (ko) * 2019-06-19 2020-10-12 두산중공업 주식회사 연소기 및 이를 포함하는 가스터빈
US11261803B2 (en) * 2020-03-05 2022-03-01 General Electric Company Method and system for fuel nozzle cleaning during engine operation
DE102020204920A1 (de) 2020-04-17 2021-10-21 Rolls-Royce Deutschland Ltd & Co Kg Brennkammerbaugruppe mit einem druckgesteuerten Verstellelement an einer äußeren Brennkammerwandung für die Beeinflussung einer Verbrennungsluftmenge
US11371709B2 (en) * 2020-06-30 2022-06-28 General Electric Company Combustor air flow path

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Also Published As

Publication number Publication date
EP2613085A1 (en) 2013-07-10
EP2613085B1 (en) 2017-05-31
CN103184899B (zh) 2016-10-05
US9010082B2 (en) 2015-04-21
JP2013140003A (ja) 2013-07-18
US20130167547A1 (en) 2013-07-04
JP6134508B2 (ja) 2017-05-24
CN103184899A (zh) 2013-07-03

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Legal Events

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FA93 Acknowledgement of application withdrawn (no request for examination)

Effective date: 20151228