FR1031608A - Dispositif d'allumage pour appareils de combustion de turbo-moteurs à gaz - Google Patents
Dispositif d'allumage pour appareils de combustion de turbo-moteurs à gazInfo
- Publication number
- FR1031608A FR1031608A FR1031608DA FR1031608A FR 1031608 A FR1031608 A FR 1031608A FR 1031608D A FR1031608D A FR 1031608DA FR 1031608 A FR1031608 A FR 1031608A
- Authority
- FR
- France
- Prior art keywords
- engines
- ignition device
- combustion devices
- gas turbo
- turbo
- 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
- 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
- F23R3/30—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices
- F23R3/32—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices being tubular
-
- 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
- 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
- F23R3/283—Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances
-
- 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
-
- 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
- F23R3/46—Combustion chambers comprising an annular arrangement of several essentially tubular flame tubes within a common annular casing or within individual casings
- F23R3/48—Flame tube interconnectors, e.g. cross-over tubes
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Nozzles For Spraying Of Liquid Fuel (AREA)
- Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US295489XA | 1949-10-22 | 1949-10-22 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| FR1031608A true FR1031608A (fr) | 1953-06-25 |
Family
ID=21849594
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR1031608D Expired FR1031608A (fr) | 1949-10-22 | 1950-10-19 | Dispositif d'allumage pour appareils de combustion de turbo-moteurs à gaz |
Country Status (4)
| Country | Link |
|---|---|
| CH (1) | CH295489A (fr) |
| DE (1) | DE852790C (fr) |
| FR (1) | FR1031608A (fr) |
| GB (1) | GB693846A (fr) |
Families Citing this family (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1064760B (de) * | 1955-03-28 | 1959-09-03 | Snecma | Zuendeinrichtung fuer Brennkammern von Rueckstossantrieben |
| FR1166154A (fr) * | 1957-02-01 | 1958-11-04 | Snecma | Brûleur à semi-vaporisation |
| US3009321A (en) * | 1958-05-21 | 1961-11-21 | Rodney A Jones | Ceramic-lined pilots for turbo-jet combustors |
| US4301656A (en) * | 1979-09-28 | 1981-11-24 | General Motors Corporation | Lean prechamber outflow combustor with continuous pilot flow |
| CN107975822B (zh) * | 2017-12-19 | 2023-03-14 | 中国科学院工程热物理研究所 | 一种燃气轮机的燃烧室及使用其的燃气轮机 |
| US11608783B2 (en) | 2020-11-04 | 2023-03-21 | Delavan, Inc. | Surface igniter cooling system |
| US11473505B2 (en) | 2020-11-04 | 2022-10-18 | Delavan Inc. | Torch igniter cooling system |
| US11692488B2 (en) | 2020-11-04 | 2023-07-04 | Delavan Inc. | Torch igniter cooling system |
| US11635027B2 (en) | 2020-11-18 | 2023-04-25 | Collins Engine Nozzles, Inc. | Fuel systems for torch ignition devices |
| US11421602B2 (en) | 2020-12-16 | 2022-08-23 | Delavan Inc. | Continuous ignition device exhaust manifold |
| US11754289B2 (en) | 2020-12-17 | 2023-09-12 | Delavan, Inc. | Axially oriented internally mounted continuous ignition device: removable nozzle |
| US11635210B2 (en) | 2020-12-17 | 2023-04-25 | Collins Engine Nozzles, Inc. | Conformal and flexible woven heat shields for gas turbine engine components |
| US11486309B2 (en) | 2020-12-17 | 2022-11-01 | Delavan Inc. | Axially oriented internally mounted continuous ignition device: removable hot surface igniter |
| US12092333B2 (en) | 2020-12-17 | 2024-09-17 | Collins Engine Nozzles, Inc. | Radially oriented internally mounted continuous ignition device |
| US11680528B2 (en) | 2020-12-18 | 2023-06-20 | Delavan Inc. | Internally-mounted torch igniters with removable igniter heads |
| US11209164B1 (en) | 2020-12-18 | 2021-12-28 | Delavan Inc. | Fuel injector systems for torch igniters |
-
1950
- 1950-10-16 CH CH295489D patent/CH295489A/fr unknown
- 1950-10-19 FR FR1031608D patent/FR1031608A/fr not_active Expired
- 1950-10-22 DE DEC3314A patent/DE852790C/de not_active Expired
- 1950-10-23 GB GB25759/50A patent/GB693846A/en not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| GB693846A (en) | 1953-07-08 |
| CH295489A (fr) | 1953-12-31 |
| DE852790C (de) | 1952-10-20 |
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