FR2952702B1 - GUIDING AN IGNITION CANDLE IN A COMBUSTION CHAMBER - Google Patents
GUIDING AN IGNITION CANDLE IN A COMBUSTION CHAMBERInfo
- Publication number
- FR2952702B1 FR2952702B1 FR0905556A FR0905556A FR2952702B1 FR 2952702 B1 FR2952702 B1 FR 2952702B1 FR 0905556 A FR0905556 A FR 0905556A FR 0905556 A FR0905556 A FR 0905556A FR 2952702 B1 FR2952702 B1 FR 2952702B1
- Authority
- FR
- France
- Prior art keywords
- guiding
- combustion chamber
- ignition candle
- candle
- ignition
- 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
- 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
- F23R3/60—Support structures; Attaching or mounting means
-
- 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
- F02C7/264—Ignition
- F02C7/266—Electric
-
- 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
- F23R3/06—Arrangement of apertures along the flame tube
-
- 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
- F05D2250/20—Three-dimensional
- F05D2250/23—Three-dimensional prismatic
- F05D2250/231—Three-dimensional prismatic cylindrical
-
- 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
- F05D2250/20—Three-dimensional
- F05D2250/23—Three-dimensional prismatic
- F05D2250/232—Three-dimensional prismatic conical
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D2207/00—Ignition devices associated with burner
-
- 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
- F23R2900/00012—Details of sealing devices
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0905556A FR2952702B1 (en) | 2009-11-19 | 2009-11-19 | GUIDING AN IGNITION CANDLE IN A COMBUSTION CHAMBER |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0905556A FR2952702B1 (en) | 2009-11-19 | 2009-11-19 | GUIDING AN IGNITION CANDLE IN A COMBUSTION CHAMBER |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2952702A1 FR2952702A1 (en) | 2011-05-20 |
FR2952702B1 true FR2952702B1 (en) | 2013-05-10 |
Family
ID=42543168
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0905556A Active FR2952702B1 (en) | 2009-11-19 | 2009-11-19 | GUIDING AN IGNITION CANDLE IN A COMBUSTION CHAMBER |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2952702B1 (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3030741B1 (en) * | 2014-12-23 | 2017-07-21 | Snecma | CANDLE GUIDE ASSEMBLY FOR TEST BENCH |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2693082A (en) * | 1951-04-04 | 1954-11-02 | Gen Motors Corp | Gas turbine fuel igniter |
US3048015A (en) * | 1959-07-08 | 1962-08-07 | Gen Motors Corp | Combustion chamber support and igniter |
US3990834A (en) * | 1973-09-17 | 1976-11-09 | General Electric Company | Cooled igniter |
US6715279B2 (en) * | 2002-03-04 | 2004-04-06 | General Electric Company | Apparatus for positioning an igniter within a liner port of a gas turbine engine |
US7546739B2 (en) * | 2005-07-05 | 2009-06-16 | General Electric Company | Igniter tube and method of assembling same |
US8479490B2 (en) * | 2007-03-30 | 2013-07-09 | Honeywell International Inc. | Combustors with impingement cooled igniters and igniter tubes for improved cooling of igniters |
FR2926329B1 (en) * | 2008-01-15 | 2013-01-04 | Snecma | ARRANGEMENT OF A SEMICONDUCTOR TYPE CANDLE IN A COMBUSTION CHAMBER OF A GAS TURBINE ENGINE. |
-
2009
- 2009-11-19 FR FR0905556A patent/FR2952702B1/en active Active
Also Published As
Publication number | Publication date |
---|---|
FR2952702A1 (en) | 2011-05-20 |
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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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Year of fee payment: 13 |
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PLFP | Fee payment |
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Year of fee payment: 15 |