FR1150640A - Improvements to combustion chambers, in particular for aircraft - Google Patents
Improvements to combustion chambers, in particular for aircraftInfo
- Publication number
- FR1150640A FR1150640A FR1150640DA FR1150640A FR 1150640 A FR1150640 A FR 1150640A FR 1150640D A FR1150640D A FR 1150640DA FR 1150640 A FR1150640 A FR 1150640A
- Authority
- FR
- France
- Prior art keywords
- aircraft
- combustion chambers
- chambers
- combustion
- 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
- F23R3/002—Wall structures
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
- F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
-
- 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
-
- 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
- F23R3/346—Feeding into different combustion zones for staged 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
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1150640T | 1956-05-18 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1150640A true FR1150640A (en) | 1958-01-16 |
Family
ID=9647489
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1150640D Expired FR1150640A (en) | 1956-05-18 | 1956-05-18 | Improvements to combustion chambers, in particular for aircraft |
Country Status (2)
Country | Link |
---|---|
FR (1) | FR1150640A (en) |
GB (1) | GB812317A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2124141A1 (en) * | 1971-02-09 | 1972-09-22 | Snecma | |
FR2587414A1 (en) * | 1985-09-17 | 1987-03-20 | Aerospatiale | Ramjet with guidance of the air/fuel mixture and missile provided with such a ramjet |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5341640A (en) * | 1993-03-30 | 1994-08-30 | Faulkner Robie L | Turbojet engine with afterburner and thrust augmentation ejectors |
EP2107310A1 (en) * | 2008-04-01 | 2009-10-07 | Siemens Aktiengesellschaft | Burner |
EP2107309A1 (en) | 2008-04-01 | 2009-10-07 | Siemens Aktiengesellschaft | Quarls in a burner |
EP2107313A1 (en) * | 2008-04-01 | 2009-10-07 | Siemens Aktiengesellschaft | Fuel staging in a burner |
EP2107312A1 (en) | 2008-04-01 | 2009-10-07 | Siemens Aktiengesellschaft | Pilot combustor in a burner |
EP2107311A1 (en) * | 2008-04-01 | 2009-10-07 | Siemens Aktiengesellschaft | Size scaling of a burner |
-
1956
- 1956-05-18 FR FR1150640D patent/FR1150640A/en not_active Expired
-
1957
- 1957-05-17 GB GB15721/57A patent/GB812317A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2124141A1 (en) * | 1971-02-09 | 1972-09-22 | Snecma | |
FR2587414A1 (en) * | 1985-09-17 | 1987-03-20 | Aerospatiale | Ramjet with guidance of the air/fuel mixture and missile provided with such a ramjet |
Also Published As
Publication number | Publication date |
---|---|
GB812317A (en) | 1959-04-22 |
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