FR1052475A - Combustion chambers particularly suitable for gas turbines - Google Patents
Combustion chambers particularly suitable for gas turbinesInfo
- Publication number
- FR1052475A FR1052475A FR1052475DA FR1052475A FR 1052475 A FR1052475 A FR 1052475A FR 1052475D A FR1052475D A FR 1052475DA FR 1052475 A FR1052475 A FR 1052475A
- Authority
- FR
- France
- Prior art keywords
- particularly suitable
- combustion chambers
- gas turbines
- chambers particularly
- turbines
- 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
- F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
- F23R3/50—Combustion chambers comprising an annular flame tube within an annular casing
-
- 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
- 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
- F23R3/10—Air inlet arrangements for primary air
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 |
---|---|---|---|
FR1052475T | 1952-03-15 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1052475A true FR1052475A (en) | 1954-01-25 |
Family
ID=9595317
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1052475D Expired FR1052475A (en) | 1952-03-15 | 1952-03-15 | Combustion chambers particularly suitable for gas turbines |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR1052475A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE961672C (en) * | 1953-01-19 | 1957-04-11 | Lucas Industries Ltd | Annular combustion chamber for jet engines, gas turbines or the like. |
DE1108516B (en) * | 1956-04-03 | 1961-06-08 | Bristol Siddeley Engines Ltd | Burning device |
EP1840466A1 (en) * | 2006-03-30 | 2007-10-03 | Snecma | Configuration of dilution openings in a wall of a turbomachine combustion chamber |
RU2626876C2 (en) * | 2012-05-25 | 2017-08-02 | Снекма | Turbomachine combustion chamber shell |
-
1952
- 1952-03-15 FR FR1052475D patent/FR1052475A/en not_active Expired
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE961672C (en) * | 1953-01-19 | 1957-04-11 | Lucas Industries Ltd | Annular combustion chamber for jet engines, gas turbines or the like. |
DE1108516B (en) * | 1956-04-03 | 1961-06-08 | Bristol Siddeley Engines Ltd | Burning device |
EP1840466A1 (en) * | 2006-03-30 | 2007-10-03 | Snecma | Configuration of dilution openings in a wall of a turbomachine combustion chamber |
FR2899315A1 (en) * | 2006-03-30 | 2007-10-05 | Snecma Sa | CONFIGURING DILUTION OPENINGS IN A TURBOMACHINE COMBUSTION CHAMBER WALL |
US7891194B2 (en) | 2006-03-30 | 2011-02-22 | Snecma | Configuration of dilution openings in a turbomachine combustion chamber wall |
RU2626876C2 (en) * | 2012-05-25 | 2017-08-02 | Снекма | Turbomachine combustion chamber shell |
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