FR1238089A - Flame tube improvements for gas turbines - Google Patents
Flame tube improvements for gas turbinesInfo
- Publication number
- FR1238089A FR1238089A FR807874A FR807874A FR1238089A FR 1238089 A FR1238089 A FR 1238089A FR 807874 A FR807874 A FR 807874A FR 807874 A FR807874 A FR 807874A FR 1238089 A FR1238089 A FR 1238089A
- Authority
- FR
- France
- Prior art keywords
- gas turbines
- flame tube
- tube improvements
- flame
- 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
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/34—Feeding into different combustion zones
-
- 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
- F23R3/12—Air inlet arrangements for primary air inducing a vortex
- F23R3/14—Air inlet arrangements for primary air inducing a vortex by using swirl vanes
-
- 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)
- Pre-Mixing And Non-Premixing Gas Burner (AREA)
- Spray-Type Burners (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US803175A US2951339A (en) | 1959-03-31 | 1959-03-31 | Combustion chamber swirler |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1238089A true FR1238089A (en) | 1960-08-05 |
Family
ID=25185787
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR807874A Expired FR1238089A (en) | 1959-03-31 | 1959-10-19 | Flame tube improvements for gas turbines |
Country Status (4)
Country | Link |
---|---|
US (1) | US2951339A (en) |
DE (1) | DE1118535B (en) |
FR (1) | FR1238089A (en) |
GB (1) | GB887829A (en) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3099134A (en) * | 1959-12-24 | 1963-07-30 | Havilland Engine Co Ltd | Combustion chambers |
DE2538134C2 (en) * | 1974-08-27 | 1984-11-08 | Mitsubishi Jukogyo K.K., Tokio/Tokyo | Oil burner |
US4173118A (en) * | 1974-08-27 | 1979-11-06 | Mitsubishi Jukogyo Kabushiki Kaisha | Fuel combustion apparatus employing staged combustion |
US3991562A (en) * | 1975-07-21 | 1976-11-16 | United Technologies Corporation | Combustion chamber assembly having removable center liner |
US5197278A (en) * | 1990-12-17 | 1993-03-30 | General Electric Company | Double dome combustor and method of operation |
US5253478A (en) * | 1991-12-30 | 1993-10-19 | General Electric Company | Flame holding diverging centerbody cup construction for a dry low NOx combustor |
US6430919B1 (en) * | 2000-03-02 | 2002-08-13 | Direct Propulsion Devices, Inc. | Shaped charged engine |
US7574865B2 (en) * | 2004-11-18 | 2009-08-18 | Siemens Energy, Inc. | Combustor flow sleeve with optimized cooling and airflow distribution |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2175866A (en) * | 1934-04-16 | 1939-10-10 | Philip S Arnold | Fuel burner |
GB670092A (en) * | 1949-01-03 | 1952-04-16 | Rolls Royce | Improvements relating to combustion equipment for gas-turbine engines |
US2676460A (en) * | 1950-03-23 | 1954-04-27 | United Aircraft Corp | Burner construction of the can-an-nular type having means for distributing airflow to each can |
GB800512A (en) * | 1955-01-03 | 1958-08-27 | Lucas Industries Ltd | Liquid fuel combustion chambers |
US2813397A (en) * | 1957-01-02 | 1957-11-19 | United Aircraft Corp | Thermal expansion means for combustion chambers |
-
1959
- 1959-03-31 US US803175A patent/US2951339A/en not_active Expired - Lifetime
- 1959-10-19 DE DEU6592A patent/DE1118535B/en active Pending
- 1959-10-19 FR FR807874A patent/FR1238089A/en not_active Expired
- 1959-11-04 GB GB37442/59A patent/GB887829A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
US2951339A (en) | 1960-09-06 |
DE1118535B (en) | 1961-11-30 |
GB887829A (en) | 1962-01-24 |
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