FR2945837B1 - Rampe d'alimentation d'une chambre de combustion ou de post-combustion de turbomachine - Google Patents
Rampe d'alimentation d'une chambre de combustion ou de post-combustion de turbomachineInfo
- Publication number
- FR2945837B1 FR2945837B1 FR0902425A FR0902425A FR2945837B1 FR 2945837 B1 FR2945837 B1 FR 2945837B1 FR 0902425 A FR0902425 A FR 0902425A FR 0902425 A FR0902425 A FR 0902425A FR 2945837 B1 FR2945837 B1 FR 2945837B1
- Authority
- FR
- France
- Prior art keywords
- combustion
- turbomachine
- post
- supply ramp
- 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 2
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
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/22—Fuel supply systems
- F02C7/222—Fuel flow conduits, e.g. manifolds
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
- F02K3/105—Heating the by-pass flow
-
- 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
- F05D2250/00—Geometry
- F05D2250/70—Shape
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Fuel-Injection Apparatus (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0902425A FR2945837B1 (fr) | 2009-05-19 | 2009-05-19 | Rampe d'alimentation d'une chambre de combustion ou de post-combustion de turbomachine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0902425A FR2945837B1 (fr) | 2009-05-19 | 2009-05-19 | Rampe d'alimentation d'une chambre de combustion ou de post-combustion de turbomachine |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2945837A1 FR2945837A1 (fr) | 2010-11-26 |
FR2945837B1 true FR2945837B1 (fr) | 2015-02-27 |
Family
ID=41566422
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0902425A Active FR2945837B1 (fr) | 2009-05-19 | 2009-05-19 | Rampe d'alimentation d'une chambre de combustion ou de post-combustion de turbomachine |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2945837B1 (fr) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3084449B1 (fr) * | 2018-07-25 | 2020-07-17 | Safran Aircraft Engines | Dispositif d'injection de carburant multipoint |
FR3106374B1 (fr) * | 2020-01-21 | 2022-01-21 | Safran Aircraft Engines | Circuit d’alimentation en carburant pour une chambre de combustion d’une turbomachine |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4862693A (en) * | 1987-12-10 | 1989-09-05 | Sundstrand Corporation | Fuel injector for a turbine engine |
US5119636A (en) * | 1989-12-21 | 1992-06-09 | Sundstrand Corporation | Fuel injector for a turbine engine |
US5211005A (en) * | 1992-04-16 | 1993-05-18 | Avco Corporation | High density fuel injection manifold |
US7607226B2 (en) * | 2006-03-03 | 2009-10-27 | Pratt & Whitney Canada Corp. | Internal fuel manifold with turned channel having a variable cross-sectional area |
-
2009
- 2009-05-19 FR FR0902425A patent/FR2945837B1/fr active Active
Also Published As
Publication number | Publication date |
---|---|
FR2945837A1 (fr) | 2010-11-26 |
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Legal Events
Date | Code | Title | Description |
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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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CD | Change of name or company name |
Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20170719 |
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PLFP | Fee payment |
Year of fee payment: 10 |
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PLFP | Fee payment |
Year of fee payment: 11 |
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PLFP | Fee payment |
Year of fee payment: 12 |
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PLFP | Fee payment |
Year of fee payment: 13 |
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PLFP | Fee payment |
Year of fee payment: 14 |
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PLFP | Fee payment |
Year of fee payment: 15 |
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PLFP | Fee payment |
Year of fee payment: 16 |