FR3032010B1 - Dispositif d'alimentation d'une chambre de combustion d'un moteur d'aeronef - Google Patents
Dispositif d'alimentation d'une chambre de combustion d'un moteur d'aeronef Download PDFInfo
- Publication number
- FR3032010B1 FR3032010B1 FR1550618A FR1550618A FR3032010B1 FR 3032010 B1 FR3032010 B1 FR 3032010B1 FR 1550618 A FR1550618 A FR 1550618A FR 1550618 A FR1550618 A FR 1550618A FR 3032010 B1 FR3032010 B1 FR 3032010B1
- Authority
- FR
- France
- Prior art keywords
- supplying
- combustion chamber
- aircraft engine
- aircraft
- engine
- 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
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- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D37/00—Arrangements in connection with fuel supply for power plant
- B64D37/005—Accessories not provided for in the groups B64D37/02 - B64D37/28
-
- 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
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/20—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
-
- 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
- F02C7/26—Starting; Ignition
- F02C7/262—Restarting after flame-out
-
- 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
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/26—Control of fuel supply
- F02C9/40—Control of fuel supply specially adapted to the use of a special fuel or a plurality of fuels
-
- 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
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/26—Control of fuel supply
- F02C9/46—Emergency fuel control
-
- 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
- F05D2260/00—Function
- F05D2260/84—Redundancy
-
- 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
- F05D2270/00—Control
- F05D2270/01—Purpose of the control system
- F05D2270/09—Purpose of the control system to cope with emergencies
- F05D2270/092—Purpose of the control system to cope with emergencies in particular blow-out and relight
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Fuel-Injection Apparatus (AREA)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR1550618A FR3032010B1 (fr) | 2015-01-27 | 2015-01-27 | Dispositif d'alimentation d'une chambre de combustion d'un moteur d'aeronef |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR1550618A FR3032010B1 (fr) | 2015-01-27 | 2015-01-27 | Dispositif d'alimentation d'une chambre de combustion d'un moteur d'aeronef |
| FR1550618 | 2015-01-27 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| FR3032010A1 FR3032010A1 (fr) | 2016-07-29 |
| FR3032010B1 true FR3032010B1 (fr) | 2018-12-07 |
Family
ID=54014894
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR1550618A Active FR3032010B1 (fr) | 2015-01-27 | 2015-01-27 | Dispositif d'alimentation d'une chambre de combustion d'un moteur d'aeronef |
Country Status (1)
| Country | Link |
|---|---|
| FR (1) | FR3032010B1 (fr) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP6978855B2 (ja) | 2017-05-16 | 2021-12-08 | 川崎重工業株式会社 | ガスタービン燃焼器およびその運転方法 |
| GB202219423D0 (en) * | 2022-12-21 | 2023-02-01 | Rolls Royce Plc | Staged combustor |
| GB202219422D0 (en) * | 2022-12-21 | 2023-02-01 | Rolls Royce Plc | A method of operating a gas turbine engine |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2771741A (en) * | 1952-05-16 | 1956-11-27 | Standard Oil Co | Low-temperature starting of gas turbine engines |
| US2940253A (en) * | 1954-03-26 | 1960-06-14 | Phillips Petroleum Co | Removal of carbon deposits from jet engines |
| US4777793A (en) * | 1986-04-14 | 1988-10-18 | Allied-Signal Inc. | Emergency power unit |
| US20120036866A1 (en) * | 2010-08-11 | 2012-02-16 | Hamilton Sundstrand Corporation | Auxiliary power unit with multiple fuel sources |
-
2015
- 2015-01-27 FR FR1550618A patent/FR3032010B1/fr active Active
Also Published As
| Publication number | Publication date |
|---|---|
| FR3032010A1 (fr) | 2016-07-29 |
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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: 20160729 |
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| PLFP | Fee payment |
Year of fee payment: 3 |
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| CD | Change of name or company name |
Owner name: SNECMA, FR Effective date: 20170713 |
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| PLFP | Fee payment |
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