FR3038699B1 - Chambre de combustion coudee d'une turbomachine - Google Patents
Chambre de combustion coudee d'une turbomachine Download PDFInfo
- Publication number
- FR3038699B1 FR3038699B1 FR1556482A FR1556482A FR3038699B1 FR 3038699 B1 FR3038699 B1 FR 3038699B1 FR 1556482 A FR1556482 A FR 1556482A FR 1556482 A FR1556482 A FR 1556482A FR 3038699 B1 FR3038699 B1 FR 3038699B1
- Authority
- FR
- France
- Prior art keywords
- turbomachine
- combustion chamber
- bent
- bent combustion
- chamber
- 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
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
- F23R3/04—Air inlet arrangements
- F23R3/10—Air inlet arrangements for primary air
- F23R3/12—Air inlet arrangements for primary air inducing a vortex
- F23R3/14—Air inlet arrangements for primary air inducing a vortex by using swirl vanes
-
- 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
- F23R3/425—Combustion chambers comprising a tangential or helicoidal arrangement of the flame tubes
-
- 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
- F23R2900/03342—Arrangement of silo-type combustion chambers
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Fuel-Injection Apparatus (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1556482A FR3038699B1 (fr) | 2015-07-08 | 2015-07-08 | Chambre de combustion coudee d'une turbomachine |
CN201680040094.2A CN107735619B (zh) | 2015-07-08 | 2016-07-07 | 涡轮发动机的弯曲的燃烧腔室 |
PCT/FR2016/051735 WO2017006063A1 (fr) | 2015-07-08 | 2016-07-07 | Chambre de combustion coudée d'une turbomachine |
EP16748329.6A EP3320269B1 (fr) | 2015-07-08 | 2016-07-07 | Chambre de combustion coudée d'une turbomachine |
PL16748329T PL3320269T3 (pl) | 2015-07-08 | 2016-07-07 | Zagięta komora spalania maszyny wirowej |
US15/742,447 US11125435B2 (en) | 2015-07-08 | 2016-07-07 | Bent combustion chamber from a turbine engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1556482A FR3038699B1 (fr) | 2015-07-08 | 2015-07-08 | Chambre de combustion coudee d'une turbomachine |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3038699A1 FR3038699A1 (fr) | 2017-01-13 |
FR3038699B1 true FR3038699B1 (fr) | 2022-06-24 |
Family
ID=54199854
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1556482A Active FR3038699B1 (fr) | 2015-07-08 | 2015-07-08 | Chambre de combustion coudee d'une turbomachine |
Country Status (6)
Country | Link |
---|---|
US (1) | US11125435B2 (fr) |
EP (1) | EP3320269B1 (fr) |
CN (1) | CN107735619B (fr) |
FR (1) | FR3038699B1 (fr) |
PL (1) | PL3320269T3 (fr) |
WO (1) | WO2017006063A1 (fr) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3090747B1 (fr) * | 2018-12-21 | 2021-01-22 | Turbotech | Chambre de combustion d'une turbomachine |
CA3141179A1 (fr) * | 2019-06-07 | 2020-12-10 | Safran Helicopter Engines | Procede de fabrication d'un tube a flamme pour une turbomachine |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
BE535905A (fr) * | 1954-02-23 | |||
US3605405A (en) * | 1970-04-09 | 1971-09-20 | Gen Electric | Carbon elimination and cooling improvement to scroll type combustors |
US3648457A (en) * | 1970-04-30 | 1972-03-14 | Gen Electric | Combustion apparatus |
JPS548890B1 (fr) * | 1971-04-01 | 1979-04-19 | ||
US4081957A (en) * | 1976-05-03 | 1978-04-04 | United Technologies Corporation | Premixed combustor |
US4458481A (en) * | 1982-03-15 | 1984-07-10 | Brown Boveri Turbomachinery, Inc. | Combustor for regenerative open cycle gas turbine system |
FR2827367B1 (fr) * | 2001-07-16 | 2003-10-17 | Snecma Moteurs | Systeme d'injection aeromecanique a vrille primaire anti-retour |
US6834505B2 (en) * | 2002-10-07 | 2004-12-28 | General Electric Company | Hybrid swirler |
US7310952B2 (en) * | 2003-10-17 | 2007-12-25 | General Electric Company | Methods and apparatus for attaching swirlers to gas turbine engine combustors |
US7437876B2 (en) * | 2005-03-25 | 2008-10-21 | General Electric Company | Augmenter swirler pilot |
FR2886714B1 (fr) * | 2005-06-07 | 2007-09-07 | Snecma Moteurs Sa | Systeme d'injection anti-rotatif pour turbo-reacteur |
WO2007033306A2 (fr) * | 2005-09-13 | 2007-03-22 | Rolls-Royce Corporation, Ltd. | Systemes de combustion pour turbine a gaz |
US7716931B2 (en) * | 2006-03-01 | 2010-05-18 | General Electric Company | Method and apparatus for assembling gas turbine engine |
WO2007104587A2 (fr) * | 2006-03-15 | 2007-09-20 | Siemens Aktiengesellschaft | Turbine à gaz à enveloppe du mélangeur réglable |
CN201991616U (zh) * | 2011-01-25 | 2011-09-28 | 苏艾今 | 超燃双工质汽轮机 |
WO2012156631A1 (fr) * | 2011-05-17 | 2012-11-22 | Snecma | Chambre annulaire de combustion pour une turbomachine |
FR3035707B1 (fr) | 2015-04-29 | 2019-11-01 | Safran Aircraft Engines | Chambre de combustion coudee d'une turbomachine |
-
2015
- 2015-07-08 FR FR1556482A patent/FR3038699B1/fr active Active
-
2016
- 2016-07-07 US US15/742,447 patent/US11125435B2/en active Active
- 2016-07-07 EP EP16748329.6A patent/EP3320269B1/fr active Active
- 2016-07-07 PL PL16748329T patent/PL3320269T3/pl unknown
- 2016-07-07 CN CN201680040094.2A patent/CN107735619B/zh active Active
- 2016-07-07 WO PCT/FR2016/051735 patent/WO2017006063A1/fr active Application Filing
Also Published As
Publication number | Publication date |
---|---|
WO2017006063A1 (fr) | 2017-01-12 |
PL3320269T3 (pl) | 2019-07-31 |
CN107735619B (zh) | 2019-07-05 |
US20180209649A1 (en) | 2018-07-26 |
CN107735619A (zh) | 2018-02-23 |
EP3320269A1 (fr) | 2018-05-16 |
EP3320269B1 (fr) | 2019-03-13 |
FR3038699A1 (fr) | 2017-01-13 |
US11125435B2 (en) | 2021-09-21 |
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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: 20170113 |
|
PLFP | Fee payment |
Year of fee payment: 3 |
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PLFP | Fee payment |
Year of fee payment: 4 |
|
CD | Change of name or company name |
Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20180809 |
|
PLFP | Fee payment |
Year of fee payment: 6 |
|
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 |