FR3111669B1 - Injecteur multipoint pour une chambre de combustion de turbomachine. - Google Patents
Injecteur multipoint pour une chambre de combustion de turbomachine. Download PDFInfo
- Publication number
- FR3111669B1 FR3111669B1 FR2006329A FR2006329A FR3111669B1 FR 3111669 B1 FR3111669 B1 FR 3111669B1 FR 2006329 A FR2006329 A FR 2006329A FR 2006329 A FR2006329 A FR 2006329A FR 3111669 B1 FR3111669 B1 FR 3111669B1
- Authority
- FR
- France
- Prior art keywords
- primary
- combustion chamber
- turbomachine combustion
- multipoint injector
- injector
- 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
- 239000007921 spray Substances 0.000 abstract 2
- 239000000446 fuel Substances 0.000 abstract 1
- 230000002093 peripheral effect Effects 0.000 abstract 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
- F23R3/36—Supply of different fuels
-
- 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
- F23D11/24—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space by pressurisation of the fuel before a nozzle through which it is sprayed by a substantial pressure reduction into a space
-
- 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
- F23D11/36—Details, e.g. burner cooling means, noise reduction means
- F23D11/38—Nozzles; Cleaning devices therefor
-
- 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
- F23K5/14—Details thereof
- F23K5/147—Valves
-
- 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
- F23R3/283—Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances
-
- 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
- F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
- F23R2900/00017—Assembling combustion chamber liners or subparts
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Nozzles (AREA)
- Fuel-Injection Apparatus (AREA)
Abstract
L’invention concerne un injecteur multipoint (36) pour une chambre de combustion de turbomachine, comprenant un corps axial (46) comportant une pluralité de buses (50) de pulvérisation primaires périphériques entourant une buse de pulvérisation (52) secondaire centrale, alimentées par des chambres primaire (56) et secondaire (58) elles-mêmes alimentées par des conduits primaire externe (62) et secondaire (66) interne d’une canalisation coaxiale (40) caractérisé en ce que les chambres primaire (56) et secondaire (58) logent des clapets anti-retour de carburant respectifs primaire (70) et secondaire (72). Figure pour l'abrégé : Figure 5.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR2006329A FR3111669B1 (fr) | 2020-06-17 | 2020-06-17 | Injecteur multipoint pour une chambre de combustion de turbomachine. |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR2006329A FR3111669B1 (fr) | 2020-06-17 | 2020-06-17 | Injecteur multipoint pour une chambre de combustion de turbomachine. |
FR2006329 | 2020-06-17 |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3111669A1 FR3111669A1 (fr) | 2021-12-24 |
FR3111669B1 true FR3111669B1 (fr) | 2022-08-05 |
Family
ID=72644376
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR2006329A Active FR3111669B1 (fr) | 2020-06-17 | 2020-06-17 | Injecteur multipoint pour une chambre de combustion de turbomachine. |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR3111669B1 (fr) |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19843607C1 (de) * | 1998-09-23 | 2000-03-09 | Buderus Heiztechnik Gmbh | Ölbrenner |
RU2285204C2 (ru) * | 2004-05-12 | 2006-10-10 | Александр Логинович Буга | Способ подачи топлива в основную камеру сгорания и устройство для его осуществления |
US8291707B2 (en) * | 2008-08-18 | 2012-10-23 | Delavan Inc | Multi-stage check valve |
JP2010242672A (ja) * | 2009-04-08 | 2010-10-28 | Toyota Motor Corp | ガスタービンの燃料供給装置 |
JP5631223B2 (ja) * | 2011-01-14 | 2014-11-26 | 三菱重工業株式会社 | 燃料ノズル、これを備えたガスタービン燃焼器およびこれを備えたガスタービン |
US9400104B2 (en) * | 2012-09-28 | 2016-07-26 | United Technologies Corporation | Flow modifier for combustor fuel nozzle tip |
-
2020
- 2020-06-17 FR FR2006329A patent/FR3111669B1/fr active Active
Also Published As
Publication number | Publication date |
---|---|
FR3111669A1 (fr) | 2021-12-24 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 2 |
|
PLSC | Publication of the preliminary search report |
Effective date: 20211224 |
|
PLFP | Fee payment |
Year of fee payment: 3 |
|
PLFP | Fee payment |
Year of fee payment: 4 |
|
PLFP | Fee payment |
Year of fee payment: 5 |