RU2665837C1 - Многоканальное устройство впрыска для авиационного двигателя - Google Patents

Многоканальное устройство впрыска для авиационного двигателя Download PDF

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Publication number
RU2665837C1
RU2665837C1 RU2016124222A RU2016124222A RU2665837C1 RU 2665837 C1 RU2665837 C1 RU 2665837C1 RU 2016124222 A RU2016124222 A RU 2016124222A RU 2016124222 A RU2016124222 A RU 2016124222A RU 2665837 C1 RU2665837 C1 RU 2665837C1
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RU
Russia
Prior art keywords
injection
channel
along
purge
pipe
Prior art date
Application number
RU2016124222A
Other languages
English (en)
Russian (ru)
Other versions
RU2016124222A (ru
Inventor
Себастьен ШАЛО
Original Assignee
Сафран Эркрафт Энджинз
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
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Application filed by Сафран Эркрафт Энджинз filed Critical Сафран Эркрафт Энджинз
Publication of RU2016124222A publication Critical patent/RU2016124222A/ru
Application granted granted Critical
Publication of RU2665837C1 publication Critical patent/RU2665837C1/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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34—Feeding into different combustion zones
    • 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
    • F02C7/22—Fuel supply systems
    • F02C7/228—Dividing fuel between various burners
    • 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
    • F02C7/22—Fuel supply systems
    • F02C7/232—Fuel valves; Draining valves or systems
    • 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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • F02C9/32—Control of fuel supply characterised by throttling of fuel
    • F02C9/34—Joint control of separate flows to main and auxiliary burners
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23K—FEEDING FUEL TO COMBUSTION APPARATUS
    • F23K5/00—Feeding or distributing other fuel to combustion apparatus
    • F23K5/02—Liquid fuel
    • F23K5/06—Liquid fuel from a central source to a plurality of burners
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D2209/00—Safety arrangements
    • F23D2209/30—Purging
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23K—FEEDING FUEL TO COMBUSTION APPARATUS
    • F23K2203/00—Feeding arrangements
    • F23K2203/10—Supply line fittings
    • F23K2203/105—Flow splitting devices to feed a plurality of burners
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23K—FEEDING FUEL TO COMBUSTION APPARATUS
    • F23K2300/00—Pretreatment and supply of liquid fuel
    • F23K2300/20—Supply line arrangements
    • F23K2300/203—Purging

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)
RU2016124222A 2013-11-20 2014-11-20 Многоканальное устройство впрыска для авиационного двигателя RU2665837C1 (ru)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1361428 2013-11-20
FR1361428A FR3013421B1 (fr) 2013-11-20 2013-11-20 Dispositif d'injection multipoint pour moteur d'aeronef
PCT/FR2014/052980 WO2015075389A1 (fr) 2013-11-20 2014-11-20 Dispositif d'injection multipoint pour moteur d'aéronef

Publications (2)

Publication Number Publication Date
RU2016124222A RU2016124222A (ru) 2017-12-22
RU2665837C1 true RU2665837C1 (ru) 2018-09-04

Family

ID=50029074

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2016124222A RU2665837C1 (ru) 2013-11-20 2014-11-20 Многоканальное устройство впрыска для авиационного двигателя

Country Status (8)

Country Link
US (1) US10465910B2 (enExample)
EP (1) EP3071886B1 (enExample)
CN (1) CN105745498B (enExample)
BR (1) BR112016011333B1 (enExample)
CA (1) CA2930368C (enExample)
FR (1) FR3013421B1 (enExample)
RU (1) RU2665837C1 (enExample)
WO (1) WO2015075389A1 (enExample)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA2921241C (fr) * 2013-08-20 2022-06-21 Snecma Procede et systeme d'injection de carburant dans une chambre de combustion d'un moteur
GB2557602B (en) * 2016-12-09 2019-05-22 Rolls Royce Plc Gas turbine engine fuel supply system having de-priming and re-priming ecology valve
GB2557599B (en) * 2016-12-09 2019-05-15 Rolls Royce Plc Gas turbine engine fuel supply system having de-priming and re-priming sub-systems
CN109611247B (zh) * 2018-11-21 2020-12-29 中国航发西安动力控制科技有限公司 一种防止发动机燃油泄漏的燃油收集装置
US20200362760A1 (en) * 2019-05-15 2020-11-19 Pratt & Whitney Canada Corp. System and method for purging a fuel manifold of a gas turbine engine using an accumulator
US11536201B2 (en) 2019-05-15 2022-12-27 Pratt & Whitney Canada Corp. System and method for purging a fuel manifold of a gas turbine engine through a flow divider valve

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5881550A (en) * 1995-08-18 1999-03-16 Fuel Systems Textron, Inc. Staged fuel injection system with shuttle valve and fuel injector therefor
RU2368794C1 (ru) * 2008-03-26 2009-09-27 Открытое акционерное общество "Омское машиностроительное конструкторское бюро" Система топливоподачи газотурбинного двигателя
EP2138688A2 (en) * 2008-06-26 2009-12-30 Rolls-Royce plc A fuel control arrangement
US20100199681A1 (en) * 2006-04-24 2010-08-12 Pratt & Whitney Canada Corp. Fuel system of gas turbine engines
RU2431082C2 (ru) * 2006-01-09 2011-10-10 Снекма Многорежимное устройство впрыска топлива, камера сгорания и турбореактивный двигатель
US20120159953A1 (en) * 2010-12-22 2012-06-28 Rolls-Royce Goodrich Engine Control Systems Ltd. Fuel Staging System

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US5865609A (en) * 1996-12-20 1999-02-02 United Technologies Corporation Method of combustion with low acoustics
US6050081A (en) * 1997-02-12 2000-04-18 Jansens Aircraft Systems Controls Air purging fuel valve for turbine engine
US8104258B1 (en) * 2007-05-24 2012-01-31 Jansen's Aircraft Systems Controls, Inc. Fuel control system with metering purge valve for dual fuel turbine
US8448441B2 (en) * 2007-07-26 2013-05-28 General Electric Company Fuel nozzle assembly for a gas turbine engine
GB2460634B (en) * 2008-06-02 2010-07-07 Rolls Royce Plc Combustion apparatus
WO2013028562A1 (en) * 2011-08-19 2013-02-28 Woodward, Inc. Split control unit
US9068511B2 (en) * 2012-04-26 2015-06-30 Hamilton Sundstrand Corporation Pressure regulating valve
US9399953B2 (en) * 2012-09-19 2016-07-26 Hamilton Sundstrand Corporation Gas turbine engine fuel system pump sharing valve

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5881550A (en) * 1995-08-18 1999-03-16 Fuel Systems Textron, Inc. Staged fuel injection system with shuttle valve and fuel injector therefor
RU2431082C2 (ru) * 2006-01-09 2011-10-10 Снекма Многорежимное устройство впрыска топлива, камера сгорания и турбореактивный двигатель
US20100199681A1 (en) * 2006-04-24 2010-08-12 Pratt & Whitney Canada Corp. Fuel system of gas turbine engines
RU2368794C1 (ru) * 2008-03-26 2009-09-27 Открытое акционерное общество "Омское машиностроительное конструкторское бюро" Система топливоподачи газотурбинного двигателя
EP2138688A2 (en) * 2008-06-26 2009-12-30 Rolls-Royce plc A fuel control arrangement
US20120159953A1 (en) * 2010-12-22 2012-06-28 Rolls-Royce Goodrich Engine Control Systems Ltd. Fuel Staging System

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
EP 2138688 A2, 3012 4.2009. *

Also Published As

Publication number Publication date
BR112016011333B1 (pt) 2021-11-03
EP3071886B1 (fr) 2018-09-05
CA2930368A1 (fr) 2015-05-28
FR3013421A1 (fr) 2015-05-22
CN105745498B (zh) 2018-06-22
US10465910B2 (en) 2019-11-05
CN105745498A (zh) 2016-07-06
WO2015075389A1 (fr) 2015-05-28
CA2930368C (fr) 2021-09-07
BR112016011333A2 (enExample) 2017-08-08
EP3071886A1 (fr) 2016-09-28
US20160298850A1 (en) 2016-10-13
FR3013421B1 (fr) 2018-12-07
RU2016124222A (ru) 2017-12-22

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