CH534847A - Brennkammer, insbesondere für ein Gasturbinentriebwerk - Google Patents
Brennkammer, insbesondere für ein GasturbinentriebwerkInfo
- Publication number
- CH534847A CH534847A CH1381471A CH1381471A CH534847A CH 534847 A CH534847 A CH 534847A CH 1381471 A CH1381471 A CH 1381471A CH 1381471 A CH1381471 A CH 1381471A CH 534847 A CH534847 A CH 534847A
- Authority
- CH
- Switzerland
- Prior art keywords
- combustion chamber
- gas turbine
- turbine engine
- engine
- combustion
- 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)
- Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US8562970A | 1970-10-30 | 1970-10-30 |
Publications (1)
Publication Number | Publication Date |
---|---|
CH534847A true CH534847A (de) | 1973-03-15 |
Family
ID=22192885
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CH1381471A CH534847A (de) | 1970-10-30 | 1971-09-20 | Brennkammer, insbesondere für ein Gasturbinentriebwerk |
Country Status (10)
Country | Link |
---|---|
US (1) | US3706203A (de) |
AU (1) | AU3490971A (de) |
BE (1) | BE774560A (de) |
CA (1) | CA938797A (de) |
CH (1) | CH534847A (de) |
DE (1) | DE2147135A1 (de) |
FR (1) | FR2111931B1 (de) |
GB (1) | GB1314666A (de) |
IL (1) | IL37773A (de) |
NL (1) | NL7113326A (de) |
Families Citing this family (45)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3955361A (en) * | 1971-12-15 | 1976-05-11 | Phillips Petroleum Company | Gas turbine combustor with controlled fuel mixing |
US3938323A (en) * | 1971-12-15 | 1976-02-17 | Phillips Petroleum Company | Gas turbine combustor with controlled fuel mixing |
US4012902A (en) * | 1974-03-29 | 1977-03-22 | Phillips Petroleum Company | Method of operating a gas turbine combustor having an independent airstream to remove heat from the primary combustion zone |
US4184326A (en) * | 1975-12-05 | 1980-01-22 | United Technologies Corporation | Louver construction for liner of gas turbine engine combustor |
US4302941A (en) * | 1980-04-02 | 1981-12-01 | United Technologies Corporation | Combuster liner construction for gas turbine engine |
US4414816A (en) * | 1980-04-02 | 1983-11-15 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Combustor liner construction |
US4361010A (en) * | 1980-04-02 | 1982-11-30 | United Technologies Corporation | Combustor liner construction |
US4333216A (en) * | 1981-03-23 | 1982-06-08 | United Technologies Corporation | Method for manufacturing a sandwich panel structure |
US4407205A (en) * | 1982-04-30 | 1983-10-04 | Beaufrere Albert H | Regeneratively cooled coal combustor/gasifier with integral dry ash removal |
US4619604A (en) * | 1983-06-30 | 1986-10-28 | Carrier Corporation | Flame radiator structure |
JPH0648095B2 (ja) * | 1985-04-18 | 1994-06-22 | 石川島播磨重工業株式会社 | ガスタ−ビン燃焼器等のライナ−冷却構造 |
US4642993A (en) * | 1985-04-29 | 1987-02-17 | Avco Corporation | Combustor liner wall |
US5329773A (en) * | 1989-08-31 | 1994-07-19 | Alliedsignal Inc. | Turbine combustor cooling system |
US5323601A (en) * | 1992-12-21 | 1994-06-28 | United Technologies Corporation | Individually removable combustor liner panel for a gas turbine engine |
US5327727A (en) * | 1993-04-05 | 1994-07-12 | General Electric Company | Micro-grooved heat transfer combustor wall |
GB9926257D0 (en) * | 1999-11-06 | 2000-01-12 | Rolls Royce Plc | Wall elements for gas turbine engine combustors |
US6868675B1 (en) * | 2004-01-09 | 2005-03-22 | Honeywell International Inc. | Apparatus and method for controlling combustor liner carbon formation |
US20060010874A1 (en) * | 2004-07-15 | 2006-01-19 | Intile John C | Cooling aft end of a combustion liner |
US7278256B2 (en) * | 2004-11-08 | 2007-10-09 | United Technologies Corporation | Pulsed combustion engine |
US7509809B2 (en) * | 2005-06-10 | 2009-03-31 | Pratt & Whitney Canada Corp. | Gas turbine engine combustor with improved cooling |
DE102005059502A1 (de) * | 2005-12-06 | 2007-06-14 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Heißkammer |
EP2116770B1 (de) * | 2008-05-07 | 2013-12-04 | Siemens Aktiengesellschaft | Anordnung zur dynamischen Dämpfung und Kühlung von Verbrennern |
US8549861B2 (en) * | 2009-01-07 | 2013-10-08 | General Electric Company | Method and apparatus to enhance transition duct cooling in a gas turbine engine |
EP2430292A1 (de) | 2009-05-12 | 2012-03-21 | Icr Turbine Engine Corporation | Energiespeicherungs- und umwandlungssystem für gasturbinen |
US8307654B1 (en) * | 2009-09-21 | 2012-11-13 | Florida Turbine Technologies, Inc. | Transition duct with spiral finned cooling passage |
US8402764B1 (en) * | 2009-09-21 | 2013-03-26 | Florida Turbine Technologies, Inc. | Transition duct with spiral cooling channels |
US20120003595A1 (en) * | 2009-09-29 | 2012-01-05 | Honeywell International Inc. | High turn down low nox burner |
WO2011109514A1 (en) | 2010-03-02 | 2011-09-09 | Icr Turbine Engine Corporatin | Dispatchable power from a renewable energy facility |
RU2530685C2 (ru) * | 2010-03-25 | 2014-10-10 | Дженерал Электрик Компани | Структуры ударного воздействия для систем охлаждения |
US8984895B2 (en) | 2010-07-09 | 2015-03-24 | Icr Turbine Engine Corporation | Metallic ceramic spool for a gas turbine engine |
EP2612009B1 (de) | 2010-09-03 | 2020-04-22 | ICR Turbine Engine Corporatin | Gasturbinenmotor |
WO2012112514A1 (en) * | 2011-02-14 | 2012-08-23 | Icr Turbine Engine Corporation | Radiation shield for a gas turbine combustor |
US8955330B2 (en) * | 2011-03-29 | 2015-02-17 | Siemens Energy, Inc. | Turbine combustion system liner |
US9051873B2 (en) | 2011-05-20 | 2015-06-09 | Icr Turbine Engine Corporation | Ceramic-to-metal turbine shaft attachment |
CN103717971B (zh) * | 2011-08-11 | 2015-09-02 | 通用电气公司 | 用于在燃气涡轮发动机中喷射燃料的*** |
US10094288B2 (en) | 2012-07-24 | 2018-10-09 | Icr Turbine Engine Corporation | Ceramic-to-metal turbine volute attachment for a gas turbine engine |
CN105318356A (zh) * | 2014-07-21 | 2016-02-10 | 北京航天动力研究所 | 一种大深宽比变截面换热通道 |
US10478920B2 (en) | 2014-09-29 | 2019-11-19 | Rolls-Royce Corporation | Dual wall components for gas turbine engines |
US10450871B2 (en) | 2015-02-26 | 2019-10-22 | Rolls-Royce Corporation | Repair of dual walled metallic components using directed energy deposition material addition |
EP3061556B1 (de) | 2015-02-26 | 2018-08-15 | Rolls-Royce Corporation | Verfahren zur reparatur von zwei dünnwandigen metallischen komponenten mithilfe von lötmaterial und hergestelltes komponent davon |
GB2545459B (en) * | 2015-12-17 | 2020-05-06 | Rolls Royce Plc | A combustion chamber |
US20180073390A1 (en) * | 2016-09-13 | 2018-03-15 | Rolls-Royce Corporation | Additively deposited gas turbine engine cooling component |
US11338396B2 (en) | 2018-03-08 | 2022-05-24 | Rolls-Royce Corporation | Techniques and assemblies for joining components |
US11480337B2 (en) | 2019-11-26 | 2022-10-25 | Collins Engine Nozzles, Inc. | Fuel injection for integral combustor and turbine vane |
RU201848U1 (ru) * | 2020-08-12 | 2021-01-15 | федеральное государственное бюджетное образовательное учреждение высшего образования "Ульяновский государственный технический университет" | Камера сгорания газотурбинного двигателя с активной зоной охлаждения |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2458066A (en) * | 1944-07-20 | 1949-01-04 | American Locomotive Co | Combustion chamber |
CH255541A (de) * | 1947-05-12 | 1948-06-30 | Bbc Brown Boveri & Cie | Gekühlte metallische Brennkammer zur Erzeugung von Heiz- und Treibgasen. |
US2775094A (en) * | 1953-12-03 | 1956-12-25 | Gen Electric | End cap for fluid fuel combustor |
US3154914A (en) * | 1959-12-12 | 1964-11-03 | Bolkow Entwicklungen Kg | Rocket engine construction |
US3545202A (en) * | 1969-04-02 | 1970-12-08 | United Aircraft Corp | Wall structure and combustion holes for a gas turbine engine |
US3572031A (en) * | 1969-07-11 | 1971-03-23 | United Aircraft Corp | Variable area cooling passages for gas turbine burners |
-
1970
- 1970-10-30 US US85629A patent/US3706203A/en not_active Expired - Lifetime
-
1971
- 1971-08-03 CA CA119723A patent/CA938797A/en not_active Expired
- 1971-09-02 GB GB4092871A patent/GB1314666A/en not_active Expired
- 1971-09-20 CH CH1381471A patent/CH534847A/de not_active IP Right Cessation
- 1971-09-21 DE DE19712147135 patent/DE2147135A1/de not_active Ceased
- 1971-09-23 IL IL37773A patent/IL37773A/xx unknown
- 1971-09-29 NL NL7113326A patent/NL7113326A/xx unknown
- 1971-10-06 FR FR7136545A patent/FR2111931B1/fr not_active Expired
- 1971-10-22 AU AU34909/71A patent/AU3490971A/en not_active Expired
- 1971-10-27 BE BE774560A patent/BE774560A/xx unknown
Also Published As
Publication number | Publication date |
---|---|
GB1314666A (en) | 1973-04-26 |
IL37773A (en) | 1974-01-14 |
AU3490971A (en) | 1973-05-03 |
BE774560A (fr) | 1972-02-14 |
IL37773A0 (en) | 1971-12-29 |
NL7113326A (de) | 1972-05-03 |
US3706203A (en) | 1972-12-19 |
FR2111931B1 (de) | 1976-02-13 |
DE2147135A1 (de) | 1972-05-04 |
FR2111931A1 (de) | 1972-06-09 |
CA938797A (en) | 1973-12-25 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PL | Patent ceased |