FR3031767B1 - Ensemble de combustion de turbomachine. - Google Patents

Ensemble de combustion de turbomachine. Download PDF

Info

Publication number
FR3031767B1
FR3031767B1 FR1550314A FR1550314A FR3031767B1 FR 3031767 B1 FR3031767 B1 FR 3031767B1 FR 1550314 A FR1550314 A FR 1550314A FR 1550314 A FR1550314 A FR 1550314A FR 3031767 B1 FR3031767 B1 FR 3031767B1
Authority
FR
France
Prior art keywords
turbomachine
combustion assembly
combustion
assembly
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.)
Active
Application number
FR1550314A
Other languages
English (en)
Other versions
FR3031767A1 (fr
Inventor
Lorenzo Huacan Hernandez
Nicolas Savary
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.)
Safran Helicopter Engines SAS
Original Assignee
Safran Helicopter Engines SAS
Turbomeca SA
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
Priority to FR1550314A priority Critical patent/FR3031767B1/fr
Application filed by Safran Helicopter Engines SAS, Turbomeca SA filed Critical Safran Helicopter Engines SAS
Priority to JP2017537358A priority patent/JP2018508733A/ja
Priority to RU2017127312A priority patent/RU2017127312A/ru
Priority to KR1020177021316A priority patent/KR20170104517A/ko
Priority to EP16701838.1A priority patent/EP3245452A1/fr
Priority to PCT/FR2016/050047 priority patent/WO2016113495A1/fr
Priority to CA2971988A priority patent/CA2971988A1/fr
Priority to US15/543,563 priority patent/US20170370591A1/en
Priority to CN201680005937.5A priority patent/CN107208897A/zh
Publication of FR3031767A1 publication Critical patent/FR3031767A1/fr
Application granted granted Critical
Publication of FR3031767B1 publication Critical patent/FR3031767B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

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
    • F23R3/38—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising rotary fuel injection means
    • 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
    • F23D11/04—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying action being obtained by centrifugal action
    • 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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/46—Combustion chambers comprising an annular arrangement of several essentially tubular flame tubes within a common annular casing or within individual casings
    • 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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/52—Toroidal combustion chambers
    • 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
    • F05D2240/00—Components
    • F05D2240/35—Combustors or associated equipment
FR1550314A 2015-01-15 2015-01-15 Ensemble de combustion de turbomachine. Active FR3031767B1 (fr)

Priority Applications (9)

Application Number Priority Date Filing Date Title
FR1550314A FR3031767B1 (fr) 2015-01-15 2015-01-15 Ensemble de combustion de turbomachine.
RU2017127312A RU2017127312A (ru) 2015-01-15 2016-01-12 Узел камеры сгорания газотурбинного двигателя
KR1020177021316A KR20170104517A (ko) 2015-01-15 2016-01-12 터빈 엔진 연소 조립체
EP16701838.1A EP3245452A1 (fr) 2015-01-15 2016-01-12 Ensemble de combustion de turbomachine
JP2017537358A JP2018508733A (ja) 2015-01-15 2016-01-12 タービンエンジン燃焼アセンブリ
PCT/FR2016/050047 WO2016113495A1 (fr) 2015-01-15 2016-01-12 Ensemble de combustion de turbomachine
CA2971988A CA2971988A1 (fr) 2015-01-15 2016-01-12 Ensemble de combustion de turbomachine
US15/543,563 US20170370591A1 (en) 2015-01-15 2016-01-12 Turbine engine combustion assembly
CN201680005937.5A CN107208897A (zh) 2015-01-15 2016-01-12 涡轮发动机燃烧组件

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1550314 2015-01-15
FR1550314A FR3031767B1 (fr) 2015-01-15 2015-01-15 Ensemble de combustion de turbomachine.

Publications (2)

Publication Number Publication Date
FR3031767A1 FR3031767A1 (fr) 2016-07-22
FR3031767B1 true FR3031767B1 (fr) 2018-10-19

Family

ID=53404641

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1550314A Active FR3031767B1 (fr) 2015-01-15 2015-01-15 Ensemble de combustion de turbomachine.

Country Status (9)

Country Link
US (1) US20170370591A1 (fr)
EP (1) EP3245452A1 (fr)
JP (1) JP2018508733A (fr)
KR (1) KR20170104517A (fr)
CN (1) CN107208897A (fr)
CA (1) CA2971988A1 (fr)
FR (1) FR3031767B1 (fr)
RU (1) RU2017127312A (fr)
WO (1) WO2016113495A1 (fr)

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE958165C (de) * 1942-08-28 1957-07-11 Karl Leist Dr Ing Brennkammer fuer kontinuierliche Verbrennung
BE507258A (fr) * 1950-12-02
US4040251A (en) * 1975-06-04 1977-08-09 Northern Research And Engineering Corporation Gas turbine combustion chamber arrangement
CN86200959U (zh) * 1986-02-21 1986-12-03 中国人民解放军第五七○六工厂 双重雾化内燃式重油燃烧器
US8776525B2 (en) * 2009-12-29 2014-07-15 Rolls-Royce North American Technologies, Inc. Gas turbine engine and combustor
CN103062797B (zh) * 2013-01-10 2014-12-10 北京航空航天大学 一种用于高高空低温低压环境下可靠点火的燃烧室中心旋流补氧结构
CN103411217B (zh) * 2013-08-10 2017-02-08 东营玺诺石油科技有限公司 一种燃油自动点火燃烧机

Also Published As

Publication number Publication date
EP3245452A1 (fr) 2017-11-22
JP2018508733A (ja) 2018-03-29
CA2971988A1 (fr) 2016-07-21
KR20170104517A (ko) 2017-09-15
WO2016113495A1 (fr) 2016-07-21
FR3031767A1 (fr) 2016-07-22
CN107208897A (zh) 2017-09-26
US20170370591A1 (en) 2017-12-28
RU2017127312A (ru) 2019-02-20

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