IT949676B - IMPROVEMENT IN GAS TURBINES - Google Patents
IMPROVEMENT IN GAS TURBINESInfo
- Publication number
- IT949676B IT949676B IT47877/72A IT4787772A IT949676B IT 949676 B IT949676 B IT 949676B IT 47877/72 A IT47877/72 A IT 47877/72A IT 4787772 A IT4787772 A IT 4787772A IT 949676 B IT949676 B IT 949676B
- Authority
- IT
- Italy
- Prior art keywords
- improvement
- gas turbines
- turbines
- gas
- Prior art date
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
- F23R3/06—Arrangement of apertures along the flame tube
- F23R3/08—Arrangement of apertures along the flame tube between annular flame tube sections, e.g. flame tubes with telescopic sections
-
- 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)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB305371 | 1971-01-25 |
Publications (1)
Publication Number | Publication Date |
---|---|
IT949676B true IT949676B (en) | 1973-06-11 |
Family
ID=9751092
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT47877/72A IT949676B (en) | 1971-01-25 | 1972-01-22 | IMPROVEMENT IN GAS TURBINES |
Country Status (4)
Country | Link |
---|---|
US (1) | US3737152A (en) |
FR (1) | FR2123386B1 (en) |
GB (1) | GB1320482A (en) |
IT (1) | IT949676B (en) |
Families Citing this family (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1429677A (en) * | 1973-03-20 | 1976-03-24 | Rolls Royce | Gas turbine engine combustion equipment |
FR2406075A1 (en) * | 1977-10-11 | 1979-05-11 | Snecma | COMBUSTION APPARATUS AND ITS EMBODIMENT PROCESS |
US4233123A (en) * | 1978-12-18 | 1980-11-11 | General Motors Corporation | Method for making an air cooled combustor |
FR2450349A1 (en) * | 1979-03-01 | 1980-09-26 | Snecma | IMPROVEMENT IN COOLING OF COMBUSTION CHAMBER WALLS BY AIR FILM |
GB2044912B (en) * | 1979-03-22 | 1983-02-23 | Rolls Royce | Gas turbine combustion chamber |
US4232527A (en) * | 1979-04-13 | 1980-11-11 | General Motors Corporation | Combustor liner joints |
US4242871A (en) * | 1979-09-18 | 1981-01-06 | United Technologies Corporation | Louver burner liner |
US4923371A (en) * | 1988-04-01 | 1990-05-08 | General Electric Company | Wall having cooling passage |
GB2221979B (en) * | 1988-08-17 | 1992-03-25 | Rolls Royce Plc | A combustion chamber for a gas turbine engine |
WO1995025932A1 (en) * | 1989-08-31 | 1995-09-28 | Alliedsignal Inc. | Turbine combustor cooling system |
US5329773A (en) * | 1989-08-31 | 1994-07-19 | Alliedsignal Inc. | Turbine combustor cooling system |
US5181379A (en) * | 1990-11-15 | 1993-01-26 | General Electric Company | Gas turbine engine multi-hole film cooled combustor liner and method of manufacture |
US5307637A (en) * | 1992-07-09 | 1994-05-03 | General Electric Company | Angled multi-hole film cooled single wall combustor dome plate |
US5261223A (en) * | 1992-10-07 | 1993-11-16 | General Electric Company | Multi-hole film cooled combustor liner with rectangular film restarting holes |
US6021570A (en) * | 1997-11-20 | 2000-02-08 | Caterpillar Inc. | Annular one piece combustor liner |
FR2914986B1 (en) * | 2007-04-12 | 2015-04-10 | Saint Gobain Isover | INTERNAL COMBUSTION BURNER |
US9494081B2 (en) | 2013-05-09 | 2016-11-15 | Siemens Aktiengesellschaft | Turbine engine shutdown temperature control system with an elongated ejector |
US11867402B2 (en) * | 2021-03-19 | 2024-01-09 | Rtx Corporation | CMC stepped combustor liner |
CN117091159A (en) | 2022-05-13 | 2023-11-21 | 通用电气公司 | Combustor liner |
CN117091157A (en) | 2022-05-13 | 2023-11-21 | 通用电气公司 | Plate hanger structure for durable combustor liner |
CN117091158A (en) | 2022-05-13 | 2023-11-21 | 通用电气公司 | Combustor chamber mesh structure |
CN117091162A (en) | 2022-05-13 | 2023-11-21 | 通用电气公司 | Burner with dilution hole structure |
CN117091161A (en) | 2022-05-13 | 2023-11-21 | 通用电气公司 | Combustor liner hollow plate design and construction |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
NL69245C (en) * | 1946-01-09 | |||
US3623711A (en) * | 1970-07-13 | 1971-11-30 | Avco Corp | Combustor liner cooling arrangement |
-
1971
- 1971-01-25 GB GB305371A patent/GB1320482A/en not_active Expired
-
1972
- 1972-01-17 US US00218286A patent/US3737152A/en not_active Expired - Lifetime
- 1972-01-22 IT IT47877/72A patent/IT949676B/en active
- 1972-01-25 FR FR7202345A patent/FR2123386B1/fr not_active Expired
Also Published As
Publication number | Publication date |
---|---|
GB1320482A (en) | 1973-06-13 |
FR2123386A1 (en) | 1972-09-08 |
US3737152A (en) | 1973-06-05 |
DE2202356B2 (en) | 1976-02-19 |
DE2202356A1 (en) | 1972-08-10 |
FR2123386B1 (en) | 1976-07-23 |
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