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 PDF

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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
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France
Prior art keywords
turbomachine
selector
fuel injection
constant volume
volume combustion
Prior art date
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Active
Application number
FR1856432A
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French (fr)
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FR3083823A1 (en
Inventor
Matthieu Leyko
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 SA
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Safran 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
Application filed by Safran SA filed Critical Safran SA
Priority to FR1856432A priority Critical patent/FR3083823B1/en
Priority to PCT/FR2019/051709 priority patent/WO2020012112A1/en
Publication of FR3083823A1 publication Critical patent/FR3083823A1/en
Application granted granted Critical
Publication of FR3083823B1 publication Critical patent/FR3083823B1/en
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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C5/00Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
    • F02C5/12Gas-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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R7/00Intermittent 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).

FR1856432A 2018-07-12 2018-07-12 FUEL INJECTION SYSTEM OF A CONSTANT VOLUME COMBUSTION SYSTEM FOR TURBOMACHINE Active FR3083823B1 (en)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Also Published As

Publication number Publication date
WO2020012112A1 (en) 2020-01-16
FR3083823A1 (en) 2020-01-17

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