PL431661A1 - Układ i sposób działania komory spalania z wieloma paliwami ciekłymi - Google Patents

Układ i sposób działania komory spalania z wieloma paliwami ciekłymi

Info

Publication number
PL431661A1
PL431661A1 PL431661A PL43166119A PL431661A1 PL 431661 A1 PL431661 A1 PL 431661A1 PL 431661 A PL431661 A PL 431661A PL 43166119 A PL43166119 A PL 43166119A PL 431661 A1 PL431661 A1 PL 431661A1
Authority
PL
Poland
Prior art keywords
gas turbine
turbine system
liquid fuel
fuel
during
Prior art date
Application number
PL431661A
Other languages
English (en)
Inventor
Jesus Daniel Castillo
Ely Edgardo Tejeda
Rene Graziano Torres
Joe Floyd Schornick
Tuy Cam HUYNH
Mirosław Paweł Babiuch
Original Assignee
General Electric Company
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 General Electric Company filed Critical General Electric Company
Priority to PL431661A priority Critical patent/PL431661A1/pl
Priority to CN202080073731.2A priority patent/CN114599867A/zh
Priority to JP2022520081A priority patent/JP2023500432A/ja
Priority to EP20804127.7A priority patent/EP4051892A1/en
Priority to US17/755,306 priority patent/US20220389876A1/en
Priority to PCT/US2020/056870 priority patent/WO2021086715A1/en
Publication of PL431661A1 publication Critical patent/PL431661A1/pl

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26Control of fuel supply
    • F02C9/40Control of fuel supply specially adapted to the use of a special fuel or a plurality of fuels
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/22Fuel supply systems
    • F02C7/236Fuel delivery systems comprising two or more pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00Application
    • F05D2220/30Application in turbines
    • F05D2220/32Application in turbines in gas turbines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00Components
    • F05D2240/35Combustors or associated equipment
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/60Fluid transfer

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Feeding And Controlling Fuel (AREA)

Abstract

Układy i sposoby przedstawione tutaj są skonfigurowane do przejścia od pierwszego paliwa ciekłego (38a) dostarczanego do komory spalania (14) układu (10) turbiny gazowej do drugiego paliwa ciekłego (38b) dostarczonego do komory spalania (14) z zastosowaniem pompy paliwa (42) skonfigurowanej do doprowadzania obu paliw (38a, 38b) z pompy paliwa (42) podczas okresu przejściowego, bez wyłączania układu (10) turbiny gazowej. Wykorzystując pompę paliwa (42) i dostosowując działanie pompy paliwa (42) w okresie przejściowym, można uniknąć zwiększonych kosztów, gabarytów i złożoności operacyjnej związanych z wieloma zespołami paliw płynnych w celu ułatwienia działania układu (10) turbiny gazowej z wieloma paliwami ciekłymi (38). Wykorzystanie wielu paliw ciekłych (38) podczas pracy układu (10) turbiny gazowej zwiększa elastyczność operacyjną układu (10) turbiny gazowej poprzez umożliwienie wykorzystania zróżnicowanych źródeł paliwa ciekłego i/lub lokalnych źródeł paliwa ciekłego w trakcie operacji w stanie stabilnym, przy jednoczesnym wykorzystaniu standaryzowanych źródeł paliwa w procedurach rozruchu lub wyłączania.
PL431661A 2019-10-30 2019-10-30 Układ i sposób działania komory spalania z wieloma paliwami ciekłymi PL431661A1 (pl)

Priority Applications (6)

Application Number Priority Date Filing Date Title
PL431661A PL431661A1 (pl) 2019-10-30 2019-10-30 Układ i sposób działania komory spalania z wieloma paliwami ciekłymi
CN202080073731.2A CN114599867A (zh) 2019-10-30 2020-10-22 用于操作具有多种液体燃料的燃烧器的系统和方法
JP2022520081A JP2023500432A (ja) 2019-10-30 2020-10-22 複数の液体燃料を有する燃焼器を動作させるためのシステムおよび方法
EP20804127.7A EP4051892A1 (en) 2019-10-30 2020-10-22 System and method for operating a combustor with multiple liquid fuels
US17/755,306 US20220389876A1 (en) 2019-10-30 2020-10-22 System and method for operating a combustor with multiple liquid fuels
PCT/US2020/056870 WO2021086715A1 (en) 2019-10-30 2020-10-22 System and method for operating a combustor with multiple liquid fuels

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PL431661A PL431661A1 (pl) 2019-10-30 2019-10-30 Układ i sposób działania komory spalania z wieloma paliwami ciekłymi

Publications (1)

Publication Number Publication Date
PL431661A1 true PL431661A1 (pl) 2021-05-04

Family

ID=73198539

Family Applications (1)

Application Number Title Priority Date Filing Date
PL431661A PL431661A1 (pl) 2019-10-30 2019-10-30 Układ i sposób działania komory spalania z wieloma paliwami ciekłymi

Country Status (6)

Country Link
US (1) US20220389876A1 (pl)
EP (1) EP4051892A1 (pl)
JP (1) JP2023500432A (pl)
CN (1) CN114599867A (pl)
PL (1) PL431661A1 (pl)
WO (1) WO2021086715A1 (pl)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20240084743A1 (en) * 2022-09-13 2024-03-14 General Electric Company Liquid fuel system for a turbomachine

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3766734A (en) * 1972-03-01 1973-10-23 Gen Electric Dual fuel control system for a gas turbine
US5490387A (en) * 1994-05-25 1996-02-13 Coltec Industries Inc Flame-out resistant fuel pumping system
US5469830A (en) * 1995-02-24 1995-11-28 The Cessna Aircraft Company Fuel blending system method and apparatus
US7216487B2 (en) * 2004-09-16 2007-05-15 Hamilton Sundstrand Metering demand fuel system for gas turbine engines
JP4865683B2 (ja) * 2007-11-15 2012-02-01 ヤンマー株式会社 燃料供給装置及び燃料供給方法
US20130074515A1 (en) * 2011-09-23 2013-03-28 General Electric Company Gas turbine engine system and method of providing a fuel supplied to one or more combustors in a gas turbine engine system
US20130089437A1 (en) * 2011-10-07 2013-04-11 Robert C. Kennedy Micro-sized fluid metering pump
US10156192B2 (en) * 2012-10-05 2018-12-18 General Electric Company Gas turbine engine with a multiple fuel delivery system
EP3051103B1 (en) * 2013-09-25 2019-03-27 IHI Corporation Fuel system
GB201420989D0 (en) * 2014-11-26 2015-01-07 Rolls Royce Plc Aircraft engine fuel system
GB201518624D0 (en) * 2015-10-21 2015-12-02 Rolls Royce Controls & Data Services Ltd Aero-engine low pressure pump
ES2698380T3 (es) * 2015-12-11 2019-02-04 Airbus Operations Sl Sistema de control de combustible para un motor de turbina de gas de una aeronave
US10487760B2 (en) * 2016-04-14 2019-11-26 Ford Global Technologies, Llc System and methods for reducing particulate matter emissions

Also Published As

Publication number Publication date
WO2021086715A1 (en) 2021-05-06
CN114599867A (zh) 2022-06-07
JP2023500432A (ja) 2023-01-06
EP4051892A1 (en) 2022-09-07
US20220389876A1 (en) 2022-12-08

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