FR1176289A - Ignition device for gas turbine engines and rocket engines - Google Patents
Ignition device for gas turbine engines and rocket enginesInfo
- Publication number
- FR1176289A FR1176289A FR1176289DA FR1176289A FR 1176289 A FR1176289 A FR 1176289A FR 1176289D A FR1176289D A FR 1176289DA FR 1176289 A FR1176289 A FR 1176289A
- Authority
- FR
- France
- Prior art keywords
- engines
- gas turbine
- ignition device
- rocket
- turbine engines
- 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.)
- Expired
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
- 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
-
- 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
- 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
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/34—Feeding into different combustion zones
- F23R3/343—Pilot flames, i.e. fuel nozzles or injectors using only a very small proportion of the total fuel to insure continuous combustion
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1694756A GB832771A (en) | 1956-06-01 | 1956-06-01 | Ignition of gas turbine and jet propulsion engines |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1176289A true FR1176289A (en) | 1959-04-08 |
Family
ID=10086532
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1176289D Expired FR1176289A (en) | 1956-06-01 | 1957-05-28 | Ignition device for gas turbine engines and rocket engines |
Country Status (2)
Country | Link |
---|---|
FR (1) | FR1176289A (en) |
GB (1) | GB832771A (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5257500A (en) * | 1992-07-27 | 1993-11-02 | General Electric Company | Aircraft engine ignition system |
US8474240B1 (en) | 2012-08-10 | 2013-07-02 | NW Licensing Company LLC | Regenerative gas generator |
CN113669161A (en) * | 2021-08-24 | 2021-11-19 | 中国航发贵阳发动机设计研究所 | Igniter with oxygen supplementing structure |
-
1956
- 1956-06-01 GB GB1694756A patent/GB832771A/en not_active Expired
-
1957
- 1957-05-28 FR FR1176289D patent/FR1176289A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
GB832771A (en) | 1960-04-13 |
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