FR3083823B1 - FUEL INJECTION SYSTEM OF A CONSTANT VOLUME COMBUSTION SYSTEM FOR TURBOMACHINE - Google Patents
FUEL INJECTION SYSTEM OF A CONSTANT VOLUME COMBUSTION SYSTEM FOR TURBOMACHINE Download PDFInfo
- Publication number
- FR3083823B1 FR3083823B1 FR1856432A FR1856432A FR3083823B1 FR 3083823 B1 FR3083823 B1 FR 3083823B1 FR 1856432 A FR1856432 A FR 1856432A FR 1856432 A FR1856432 A FR 1856432A FR 3083823 B1 FR3083823 B1 FR 3083823B1
- Authority
- FR
- France
- Prior art keywords
- turbomachine
- selector
- fuel injection
- constant volume
- volume combustion
- 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
Classifications
-
- 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
- F02C5/00—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
- F02C5/12—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion the combustion chambers having inlet or outlet valves, e.g. Holzwarth gas-turbine plants
-
- 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
- F23R7/00—Intermittent or explosive combustion chambers
Abstract
Un système (1) de combustion à volume constant pour turbomachine comprenant une pluralité de chambres de combustion (2) réparties de manière annulaire autour d'un axe principal (θ ), lesdites chambres de combustion (2) comprenant des orifices d'admission (21) et des orifices d'échappement (22), le système (1) comprenant un sélecteur (3) mobile en rotation autour de l'axe principal (θ ) qui est configuré pour obturer et ouvrir sélectivement les orifices d'admission (21) et les orifices d'échappement (22) lors de la rotation dudit sélecteur (3), caractérisé en ce qu'au moins un canal d'injection de carburant (34) est formé dans ledit sélecteur (3) pour injecter sélectivement le carburant dans les chambres de combustion (2) lors de la rotation dudit sélecteur (3).A constant volume combustion system (1) for a turbomachine comprising a plurality of combustion chambers (2) distributed annularly around a main axis (θ), said combustion chambers (2) comprising intake orifices ( 21) and exhaust ports (22), the system (1) comprising a selector (3) movable in rotation around the main axis (θ) which is configured to selectively close and open the intake ports (21 ) and the exhaust ports (22) during rotation of said selector (3), characterized in that at least one fuel injection channel (34) is formed in said selector (3) for selectively injecting fuel in the combustion chambers (2) during the rotation of said selector (3).
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1856432A FR3083823B1 (en) | 2018-07-12 | 2018-07-12 | FUEL INJECTION SYSTEM OF A CONSTANT VOLUME COMBUSTION SYSTEM FOR TURBOMACHINE |
PCT/FR2019/051709 WO2020012112A1 (en) | 2018-07-12 | 2019-07-09 | Fuel injection system of a constant-volume combustion system for a turbomachine |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1856432A FR3083823B1 (en) | 2018-07-12 | 2018-07-12 | FUEL INJECTION SYSTEM OF A CONSTANT VOLUME COMBUSTION SYSTEM FOR TURBOMACHINE |
FR1856432 | 2018-07-12 |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3083823A1 FR3083823A1 (en) | 2020-01-17 |
FR3083823B1 true FR3083823B1 (en) | 2020-09-25 |
Family
ID=63491760
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1856432A Active FR3083823B1 (en) | 2018-07-12 | 2018-07-12 | FUEL INJECTION SYSTEM OF A CONSTANT VOLUME COMBUSTION SYSTEM FOR TURBOMACHINE |
Country Status (2)
Country | Link |
---|---|
FR (1) | FR3083823B1 (en) |
WO (1) | WO2020012112A1 (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3068075B1 (en) * | 2017-06-23 | 2019-08-09 | Safran | CONSTANT VOLUME COMBUSTION SYSTEM COMPRISING A SEGMENTED LIGHTING ROTATING ELEMENT |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2579321A (en) * | 1948-04-09 | 1951-12-18 | Nina K Guercken | Apparatus for producing gas under pressure |
US2937498A (en) * | 1953-01-13 | 1960-05-24 | Fritz A F Schmidt | Mechanically controlled multistage combustion chambers for gas-impulsetype engines and improved discharge control therefor |
FR3032025B1 (en) * | 2015-01-26 | 2018-06-15 | Safran | COMBUSTION MODULE WITH CONSTANT VOLUME FOR A TURBOMACHINE |
FR3032781B1 (en) * | 2015-02-17 | 2018-07-06 | Safran Helicopter Engines | CONSTANT VOLUME COMBUSTION SYSTEM FOR AIRCRAFT ENGINE TURBOMACHINE |
-
2018
- 2018-07-12 FR FR1856432A patent/FR3083823B1/en active Active
-
2019
- 2019-07-09 WO PCT/FR2019/051709 patent/WO2020012112A1/en active Application Filing
Also Published As
Publication number | Publication date |
---|---|
WO2020012112A1 (en) | 2020-01-16 |
FR3083823A1 (en) | 2020-01-17 |
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Legal Events
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Effective date: 20200117 |
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PLFP | Fee payment |
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