BE806783A - Raidisseur de dispositif de combustion - Google Patents
Raidisseur de dispositif de combustionInfo
- Publication number
- BE806783A BE806783A BE137290A BE137290A BE806783A BE 806783 A BE806783 A BE 806783A BE 137290 A BE137290 A BE 137290A BE 137290 A BE137290 A BE 137290A BE 806783 A BE806783 A BE 806783A
- Authority
- BE
- Belgium
- Prior art keywords
- combustion device
- straightener
- device straightener
- 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 |
---|---|---|---|
US30319772A | 1972-11-02 | 1972-11-02 |
Publications (1)
Publication Number | Publication Date |
---|---|
BE806783A true BE806783A (fr) | 1974-02-15 |
Family
ID=23170959
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BE137290A BE806783A (fr) | 1972-11-02 | 1973-10-31 | Raidisseur de dispositif de combustion |
Country Status (7)
Country | Link |
---|---|
US (1) | US3793827A (xx) |
JP (1) | JPS4995012A (xx) |
BE (1) | BE806783A (xx) |
CA (1) | CA986734A (xx) |
DE (1) | DE2354504C2 (xx) |
FR (1) | FR2205628A1 (xx) |
IT (1) | IT998848B (xx) |
Families Citing this family (30)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4232527A (en) * | 1979-04-13 | 1980-11-11 | General Motors Corporation | Combustor liner joints |
US4380906A (en) * | 1981-01-22 | 1983-04-26 | United Technologies Corporation | Combustion liner cooling scheme |
US4628694A (en) * | 1983-12-19 | 1986-12-16 | General Electric Company | Fabricated liner article and method |
US4688310A (en) * | 1983-12-19 | 1987-08-25 | General Electric Company | Fabricated liner article and method |
US4696431A (en) * | 1985-11-29 | 1987-09-29 | United Technologies Corporation | Augmentor liner support band having finger positioners |
US4928479A (en) * | 1987-12-28 | 1990-05-29 | Sundstrand Corporation | Annular combustor with tangential cooling air injection |
US4887663A (en) * | 1988-05-31 | 1989-12-19 | United Technologies Corporation | Hot gas duct liner |
US4944152A (en) * | 1988-10-11 | 1990-07-31 | Sundstrand Corporation | Augmented turbine combustor cooling |
JP2928607B2 (ja) * | 1989-12-22 | 1999-08-03 | 株式会社日立製作所 | 燃焼装置及びその燃焼方法 |
US5259182A (en) * | 1989-12-22 | 1993-11-09 | Hitachi, Ltd. | Combustion apparatus and combustion method therein |
US5388765A (en) * | 1990-04-18 | 1995-02-14 | United Technologies Corporation | Gas turbine nozzle construction |
JP2597800B2 (ja) * | 1992-06-12 | 1997-04-09 | ゼネラル・エレクトリック・カンパニイ | ガスタービンエンジン用燃焼器 |
US5771680A (en) * | 1995-12-21 | 1998-06-30 | General Electric Company | Stiffened composite structures and method of making thereof |
US7080514B2 (en) * | 2003-08-15 | 2006-07-25 | Siemens Power Generation,Inc. | High frequency dynamics resonator assembly |
US7278256B2 (en) * | 2004-11-08 | 2007-10-09 | United Technologies Corporation | Pulsed combustion engine |
US7500364B2 (en) | 2005-11-22 | 2009-03-10 | Honeywell International Inc. | System for coupling flow from a centrifugal compressor to an axial combustor for gas turbines |
US7571611B2 (en) * | 2006-04-24 | 2009-08-11 | General Electric Company | Methods and system for reducing pressure losses in gas turbine engines |
JP4969384B2 (ja) * | 2007-09-25 | 2012-07-04 | 三菱重工業株式会社 | ガスタービン燃焼器の冷却構造 |
US8033119B2 (en) * | 2008-09-25 | 2011-10-11 | Siemens Energy, Inc. | Gas turbine transition duct |
US8667801B2 (en) | 2010-09-08 | 2014-03-11 | Siemens Energy, Inc. | Combustor liner assembly with enhanced cooling system |
US9126374B2 (en) | 2010-09-28 | 2015-09-08 | Russell B. Hanson | Iso-grid composite component |
ES2427440T3 (es) * | 2011-03-15 | 2013-10-30 | Siemens Aktiengesellschaft | Cámara de combustión de turbina de gas |
US9410484B2 (en) | 2013-07-19 | 2016-08-09 | Siemens Aktiengesellschaft | Cooling chamber for upstream weld of damping resonator on turbine component |
WO2015095759A1 (en) * | 2013-12-19 | 2015-06-25 | United Technologies Corporation | Thermal mechanical dimple array for a combustor wall assembly |
KR101556532B1 (ko) * | 2014-01-16 | 2015-10-01 | 두산중공업 주식회사 | 냉각슬리브를 포함하는 라이너, 플로우슬리브 및 가스터빈연소기 |
US10012385B2 (en) | 2014-08-08 | 2018-07-03 | Pratt & Whitney Canada Corp. | Combustor heat shield sealing |
CN117091162A (zh) | 2022-05-13 | 2023-11-21 | 通用电气公司 | 具有稀释孔结构的燃烧器 |
CN117091158A (zh) | 2022-05-13 | 2023-11-21 | 通用电气公司 | 燃烧器室网状结构 |
CN117091159A (zh) | 2022-05-13 | 2023-11-21 | 通用电气公司 | 燃烧器衬里 |
CN117091161A (zh) | 2022-05-13 | 2023-11-21 | 通用电气公司 | 燃烧器衬里的中空板设计和结构 |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2549858A (en) * | 1946-07-30 | 1951-04-24 | Westinghouse Electric Corp | Annular combustion chamber having telescoping walls with corrugated ends for spacing |
DE1077002B (de) * | 1957-11-29 | 1960-03-03 | Gen Motors Corp | Brennkammer fuer Gasturbinentriebwerke |
US3038309A (en) * | 1959-07-21 | 1962-06-12 | Gen Electric | Cooling liner for jet engine afterburner |
US3064425A (en) * | 1959-10-05 | 1962-11-20 | Gen Motors Corp | Combustion liner |
US3138930A (en) * | 1961-09-26 | 1964-06-30 | Gen Electric | Combustion chamber liner construction |
US3359724A (en) * | 1965-08-03 | 1967-12-26 | Bristol Siddeley Engines Ltd | Cooling means in combustors for gas turbine engines |
US3307354A (en) * | 1965-10-01 | 1967-03-07 | Gen Electric | Cooling structure for overlapped panels |
-
1972
- 1972-11-02 US US00303197A patent/US3793827A/en not_active Expired - Lifetime
-
1973
- 1973-10-05 CA CA182,711A patent/CA986734A/en not_active Expired
- 1973-10-23 IT IT30417/73A patent/IT998848B/it active
- 1973-10-31 FR FR7338774A patent/FR2205628A1/fr not_active Withdrawn
- 1973-10-31 DE DE2354504A patent/DE2354504C2/de not_active Expired
- 1973-10-31 BE BE137290A patent/BE806783A/xx unknown
- 1973-11-02 JP JP48122981A patent/JPS4995012A/ja active Pending
Also Published As
Publication number | Publication date |
---|---|
CA986734A (en) | 1976-04-06 |
DE2354504A1 (de) | 1974-05-16 |
FR2205628A1 (xx) | 1974-05-31 |
US3793827A (en) | 1974-02-26 |
DE2354504C2 (de) | 1984-01-19 |
JPS4995012A (xx) | 1974-09-10 |
IT998848B (it) | 1976-02-20 |
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