GB662764A - Improvements relating to combustion chambers for jet-engines or gas turbines - Google Patents
Improvements relating to combustion chambers for jet-engines or gas turbinesInfo
- Publication number
- GB662764A GB662764A GB82949A GB82949A GB662764A GB 662764 A GB662764 A GB 662764A GB 82949 A GB82949 A GB 82949A GB 82949 A GB82949 A GB 82949A GB 662764 A GB662764 A GB 662764A
- Authority
- GB
- United Kingdom
- Prior art keywords
- screens
- combustion
- gas turbines
- engines
- jet
- 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
- F23R3/02—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
-
- 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
- F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
662,764. Generating combustion products under pressure. LUCAS, Ltd., J. Jan. 2, 1950 [Jan. 12, 1949], No. 829/49. Class 51 (i). In an annular type combustion chamber for jet propulsion engines or gas turbines, screens e are arranged around the fuel injection nozzles h, the screens being shaped to provide a pair of segmental boundaries between a pair of adjacent combustion regions. The screens are shaped to a U-section, the sides of which have perforations f for admission of air to the combustion regions. The fuel nozzles are located in the annular plate g which has rings of perforations i for admission of primary combustion air and air swirling means j.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB82949A GB662764A (en) | 1949-01-12 | 1949-01-12 | Improvements relating to combustion chambers for jet-engines or gas turbines |
FR1008197D FR1008197A (en) | 1949-01-12 | 1950-01-10 | Engine combustion chamber |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB82949A GB662764A (en) | 1949-01-12 | 1949-01-12 | Improvements relating to combustion chambers for jet-engines or gas turbines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB662764A true GB662764A (en) | 1951-12-12 |
Family
ID=9711203
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB82949A Expired GB662764A (en) | 1949-01-12 | 1949-01-12 | Improvements relating to combustion chambers for jet-engines or gas turbines |
Country Status (2)
Country | Link |
---|---|
FR (1) | FR1008197A (en) |
GB (1) | GB662764A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5479774A (en) * | 1991-04-30 | 1996-01-02 | Rolls-Royce Plc | Combustion chamber assembly in a gas turbine engine |
GB2543435A (en) * | 2014-07-14 | 2017-04-19 | Caterpillar (Ni) Ltd | A fluid distribution apparatus for an engine system |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1046954B (en) * | 1953-03-26 | 1958-12-18 | Herbert Troeger | Combustion turbine with combustion chambers that also act as expansion nozzles |
FR2683891B1 (en) * | 1991-11-20 | 1995-03-24 | Snecma | TURBOMACHINE COMPRISING A DEVICE FOR REDUCING THE EMISSION OF NITROGEN OXIDES. |
FR2694624B1 (en) * | 1992-08-05 | 1994-09-23 | Snecma | Combustion chamber with several fuel injectors. |
FR2694799B1 (en) * | 1992-08-12 | 1994-09-23 | Snecma | Conventional annular combustion chamber with several injectors. |
-
1949
- 1949-01-12 GB GB82949A patent/GB662764A/en not_active Expired
-
1950
- 1950-01-10 FR FR1008197D patent/FR1008197A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5479774A (en) * | 1991-04-30 | 1996-01-02 | Rolls-Royce Plc | Combustion chamber assembly in a gas turbine engine |
GB2543435A (en) * | 2014-07-14 | 2017-04-19 | Caterpillar (Ni) Ltd | A fluid distribution apparatus for an engine system |
GB2543435B (en) * | 2014-07-14 | 2017-10-11 | Caterpillar (Ni) Ltd | A fluid distribution apparatus for an engine system |
Also Published As
Publication number | Publication date |
---|---|
FR1008197A (en) | 1952-05-14 |
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