FR3031767B1 - Ensemble de combustion de turbomachine. - Google Patents
Ensemble de combustion de turbomachine. Download PDFInfo
- 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
Links
- 238000002485 combustion reaction Methods 0.000 title 1
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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Fuel-Injection Apparatus (AREA)
- Nozzles For Spraying Of Liquid Fuel (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
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 |
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 |
EP16701838.1A EP3245452A1 (fr) | 2015-01-15 | 2016-01-12 | Ensemble de combustion de turbomachine |
KR1020177021316A KR20170104517A (ko) | 2015-01-15 | 2016-01-12 | 터빈 엔진 연소 조립체 |
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 |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1550314A FR3031767B1 (fr) | 2015-01-15 | 2015-01-15 | Ensemble de combustion de turbomachine. |
FR1550314 | 2015-01-15 |
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) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20200318549A1 (en) * | 2019-04-04 | 2020-10-08 | United Technologies Corporation | Non-axisymmetric combustor for improved durability |
Family Cites Families (7)
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 |
-
2015
- 2015-01-15 FR FR1550314A patent/FR3031767B1/fr active Active
-
2016
- 2016-01-12 KR KR1020177021316A patent/KR20170104517A/ko unknown
- 2016-01-12 US US15/543,563 patent/US20170370591A1/en not_active Abandoned
- 2016-01-12 CA CA2971988A patent/CA2971988A1/fr not_active Abandoned
- 2016-01-12 WO PCT/FR2016/050047 patent/WO2016113495A1/fr active Application Filing
- 2016-01-12 JP JP2017537358A patent/JP2018508733A/ja active Pending
- 2016-01-12 RU RU2017127312A patent/RU2017127312A/ru not_active Application Discontinuation
- 2016-01-12 CN CN201680005937.5A patent/CN107208897A/zh active Pending
- 2016-01-12 EP EP16701838.1A patent/EP3245452A1/fr not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
FR3031767A1 (fr) | 2016-07-22 |
CN107208897A (zh) | 2017-09-26 |
RU2017127312A (ru) | 2019-02-20 |
WO2016113495A1 (fr) | 2016-07-21 |
EP3245452A1 (fr) | 2017-11-22 |
JP2018508733A (ja) | 2018-03-29 |
CA2971988A1 (fr) | 2016-07-21 |
US20170370591A1 (en) | 2017-12-28 |
KR20170104517A (ko) | 2017-09-15 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 2 |
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PLSC | Publication of the preliminary search report |
Effective date: 20160722 |
|
PLFP | Fee payment |
Year of fee payment: 3 |
|
CD | Change of name or company name |
Owner name: SAFRAN HELICOPTER ENGINES, FR Effective date: 20170727 |
|
PLFP | Fee payment |
Year of fee payment: 4 |
|
PLFP | Fee payment |
Year of fee payment: 6 |
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PLFP | Fee payment |
Year of fee payment: 7 |
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PLFP | Fee payment |
Year of fee payment: 8 |
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PLFP | Fee payment |
Year of fee payment: 9 |
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PLFP | Fee payment |
Year of fee payment: 10 |