GB1379368A - Gas turbine engine having apparatus for the admission and condi tioning of fuel/air constituents - Google Patents
Gas turbine engine having apparatus for the admission and condi tioning of fuel/air constituentsInfo
- Publication number
- GB1379368A GB1379368A GB1009873A GB1009873A GB1379368A GB 1379368 A GB1379368 A GB 1379368A GB 1009873 A GB1009873 A GB 1009873A GB 1009873 A GB1009873 A GB 1009873A GB 1379368 A GB1379368 A GB 1379368A
- Authority
- GB
- United Kingdom
- Prior art keywords
- air
- fuel
- combustion chamber
- inlets
- compressor
- 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
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/14—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
-
- 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
- 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
- F23R3/38—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising rotary fuel injection means
-
- 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
- F23R3/52—Toroidal combustion chambers
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Processes For Solid Components From Exhaust (AREA)
- Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE2209727A DE2209727C3 (de) | 1972-03-01 | 1972-03-01 | Umkehr-Ringbrennkammer für Gasturbinentriebwerke |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1379368A true GB1379368A (en) | 1975-01-02 |
Family
ID=5837532
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1009873A Expired GB1379368A (en) | 1972-03-01 | 1973-03-01 | Gas turbine engine having apparatus for the admission and condi tioning of fuel/air constituents |
Country Status (3)
| Country | Link |
|---|---|
| DE (1) | DE2209727C3 (enExample) |
| FR (1) | FR2174260B1 (enExample) |
| GB (1) | GB1379368A (enExample) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2636093B1 (fr) * | 1988-09-02 | 1993-10-29 | Serrier Michel | Reacteur de petites dimensions fonctionnant au gaz propane |
| US10976052B2 (en) * | 2017-10-25 | 2021-04-13 | General Electric Company | Volute trapped vortex combustor assembly |
-
1972
- 1972-03-01 DE DE2209727A patent/DE2209727C3/de not_active Expired
-
1973
- 1973-03-01 GB GB1009873A patent/GB1379368A/en not_active Expired
- 1973-03-01 FR FR7307386A patent/FR2174260B1/fr not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| FR2174260A1 (enExample) | 1973-10-12 |
| DE2209727A1 (de) | 1973-09-13 |
| DE2209727C3 (de) | 1975-06-12 |
| FR2174260B1 (enExample) | 1977-12-30 |
| DE2209727B2 (de) | 1974-11-07 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PS | Patent sealed | ||
| PLNP | Patent lapsed through nonpayment of renewal fees |