FR1124167A - Ignition device, particularly applicable to combustion chambers of engines and thrusters - Google Patents
Ignition device, particularly applicable to combustion chambers of engines and thrustersInfo
- Publication number
- FR1124167A FR1124167A FR1124167DA FR1124167A FR 1124167 A FR1124167 A FR 1124167A FR 1124167D A FR1124167D A FR 1124167DA FR 1124167 A FR1124167 A FR 1124167A
- Authority
- FR
- France
- Prior art keywords
- thrusters
- engines
- ignition device
- combustion chambers
- particularly applicable
- 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
- F02C7/262—Restarting after flame-out
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1124167T | 1955-03-28 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1124167A true FR1124167A (en) | 1956-10-05 |
Family
ID=9633663
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1124167D Expired FR1124167A (en) | 1955-03-28 | 1955-03-28 | Ignition device, particularly applicable to combustion chambers of engines and thrusters |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR1124167A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2958196A (en) * | 1959-01-02 | 1960-11-01 | Gen Electric | Flame igniter for gas turbine combustor |
DE1100390B (en) * | 1957-01-29 | 1961-02-23 | Bristol Siddeley Engines Ltd | Continuous radiant tube burner |
DE1139330B (en) * | 1957-12-20 | 1962-11-08 | Snecma | Burner device for jet engines working in direct current |
DE1198130B (en) * | 1958-08-22 | 1965-08-05 | Snecma | Burner for ring-shaped combustion chambers |
DE1208947B (en) * | 1961-08-17 | 1966-01-13 | Gen Electric | Supersonic burner for supersonic air flow in a supersonic recoil engine |
-
1955
- 1955-03-28 FR FR1124167D patent/FR1124167A/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1100390B (en) * | 1957-01-29 | 1961-02-23 | Bristol Siddeley Engines Ltd | Continuous radiant tube burner |
DE1139330B (en) * | 1957-12-20 | 1962-11-08 | Snecma | Burner device for jet engines working in direct current |
DE1198130B (en) * | 1958-08-22 | 1965-08-05 | Snecma | Burner for ring-shaped combustion chambers |
US2958196A (en) * | 1959-01-02 | 1960-11-01 | Gen Electric | Flame igniter for gas turbine combustor |
DE1208947B (en) * | 1961-08-17 | 1966-01-13 | Gen Electric | Supersonic burner for supersonic air flow in a supersonic recoil engine |
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