DE4223733C2 - Verbindung von Mischrohr und Flammrohr einer Gasturbine - Google Patents
Verbindung von Mischrohr und Flammrohr einer GasturbineInfo
- Publication number
- DE4223733C2 DE4223733C2 DE4223733A DE4223733A DE4223733C2 DE 4223733 C2 DE4223733 C2 DE 4223733C2 DE 4223733 A DE4223733 A DE 4223733A DE 4223733 A DE4223733 A DE 4223733A DE 4223733 C2 DE4223733 C2 DE 4223733C2
- Authority
- DE
- Germany
- Prior art keywords
- mixing tube
- intermediate ring
- tube
- cone
- spacer
- 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 - Lifetime
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
- F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
- F23R3/60—Support structures; Attaching or mounting means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/023—Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/20—Three-dimensional
- F05D2250/23—Three-dimensional prismatic
- F05D2250/232—Three-dimensional prismatic conical
-
- 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
- F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
- F23R2900/03342—Arrangement of silo-type combustion chambers
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE4223733A DE4223733C2 (de) | 1992-07-18 | 1992-07-18 | Verbindung von Mischrohr und Flammrohr einer Gasturbine |
US08/093,093 US5419114A (en) | 1992-07-18 | 1993-07-16 | Thermoelastic connection of the injector tube and the flame tube of a gas turbine |
IT93MI001585A IT1265170B1 (it) | 1992-07-18 | 1993-07-19 | Collegamento termoelastico di un tubo miscelatore e di un tubo di fiamma di una turbina a gas |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE4223733A DE4223733C2 (de) | 1992-07-18 | 1992-07-18 | Verbindung von Mischrohr und Flammrohr einer Gasturbine |
Publications (2)
Publication Number | Publication Date |
---|---|
DE4223733A1 DE4223733A1 (de) | 1994-01-20 |
DE4223733C2 true DE4223733C2 (de) | 1995-05-18 |
Family
ID=6463566
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE4223733A Expired - Lifetime DE4223733C2 (de) | 1992-07-18 | 1992-07-18 | Verbindung von Mischrohr und Flammrohr einer Gasturbine |
Country Status (3)
Country | Link |
---|---|
US (1) | US5419114A (en22) |
DE (1) | DE4223733C2 (en22) |
IT (1) | IT1265170B1 (en22) |
Families Citing this family (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2293232B (en) * | 1994-09-15 | 1998-05-20 | Rolls Royce Plc | A combustion chamber assembly |
US5669812A (en) * | 1996-02-21 | 1997-09-23 | Braden Manufacturing | Exhaust gas diffuser interface |
US6116013A (en) * | 1998-01-02 | 2000-09-12 | Siemens Westinghouse Power Corporation | Bolted gas turbine combustor transition coupling |
SE520576C2 (sv) * | 2000-09-29 | 2003-07-29 | Turbec Ab | Anslutningsanordning för en värmemotorenhet |
US7647779B2 (en) * | 2005-04-27 | 2010-01-19 | United Technologies Corporation | Compliant metal support for ceramic combustor liner in a gas turbine engine |
FR2896575B1 (fr) * | 2006-01-26 | 2013-01-18 | Snecma | Chambre de combustion annulaire d'une turbomachine |
FR2897144B1 (fr) * | 2006-02-08 | 2008-05-02 | Snecma Sa | Chambre de combustion de turbomachine a fentes tangentielles |
EP1994260B1 (de) * | 2006-03-15 | 2017-09-20 | Siemens Aktiengesellschaft | Brennkammer für eine gasturbine umfassend eine verstellvorrichtung |
EP1840471B1 (de) * | 2006-03-31 | 2011-07-27 | Alstom Technology Ltd | Vorrichtung zur Befestigung eines sequentiell betriebenen Brenners in einer Gasturbinenanordnung |
US7681403B2 (en) * | 2006-04-13 | 2010-03-23 | General Electric Company | Forward sleeve retainer plate and method |
FR2914707B1 (fr) * | 2007-04-05 | 2009-10-30 | Snecma Propulsion Solide Sa | Procede d'assemblage avec recouvrement de deux pieces ayant des coefficients de dilatation differents et assemblage ainsi obtenu |
DE102007050664A1 (de) * | 2007-10-24 | 2009-04-30 | Man Turbo Ag | Brenner für eine Strömungsmaschine, Leitblech für einen derartigen Brenner sowie eine Strömungsmaschine mit einem derartigen Brenner |
US9074005B2 (en) * | 2009-01-02 | 2015-07-07 | Washington State University | Compositions and methods for modulating plant disease resistance and immunity |
US8448444B2 (en) | 2011-02-18 | 2013-05-28 | General Electric Company | Method and apparatus for mounting transition piece in combustor |
US20130333389A1 (en) * | 2012-06-15 | 2013-12-19 | General Electric Company | Cross fire tube retention system for a gas turbine engine |
EP2964898B1 (en) * | 2013-03-06 | 2019-01-16 | Rolls-Royce North American Technologies, Inc. | Gas turbine engine with soft mounted pre-swirl nozzle |
EP3296638B1 (en) | 2016-09-20 | 2020-02-19 | General Electric Technology GmbH | Burner assembly and method for a burner of a gas turbine |
DE102017207392A1 (de) * | 2017-05-03 | 2018-11-08 | Siemens Aktiengesellschaft | Silobrennkammer und Verfahren zum Umrüsten einer solchen |
CN113775417B (zh) * | 2021-09-18 | 2022-11-08 | 贵州黎阳天翔科技有限公司 | 一种燃气轮机引射器 |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2337038A (en) * | 1942-06-11 | 1943-12-21 | Chicago Metal Hose Corp | Flexible connector |
GB584820A (en) * | 1944-12-22 | 1947-01-23 | Lucas Ltd Joseph | Improvements relating to internal combustion prime movers |
US2592060A (en) * | 1946-03-25 | 1952-04-08 | Rolls Royce | Mounting of combustion chambers in jet-propulsion and gas-turbine power-units |
GB612532A (en) * | 1946-04-08 | 1948-11-15 | Adrian Albert Lombard | Improvements in or relating to combustion chambers for internal combustion turbines |
DE825777C (de) * | 1949-08-19 | 1951-12-20 | Canadian Patents Dev | Flammrohr von Brennkammern, insbesondere fuer Gasturbinen |
US2693371A (en) * | 1952-06-16 | 1954-11-02 | Solar Aircraft Co | Short flexible coupling |
US2709338A (en) * | 1953-01-16 | 1955-05-31 | Rolls Royce | Double-walled ducting for conveying hot gas with means to interconnect the walls |
GB1010338A (en) * | 1962-09-11 | 1965-11-17 | Lucas Industries Ltd | Means for supporting the downstream end of a combustion chamber in a gas turbine engine |
US4614082A (en) * | 1972-12-19 | 1986-09-30 | General Electric Company | Combustion chamber construction |
US4016718A (en) * | 1975-07-21 | 1977-04-12 | United Technologies Corporation | Gas turbine engine having an improved transition duct support |
GB1592858A (en) * | 1977-01-21 | 1981-07-08 | Rolls Royce | Combustion equipment for gas turbine engines |
FR2465080A1 (fr) * | 1979-09-17 | 1981-03-20 | Snecma | Dispositif de suspension aval de chambre de combustion pour turbomachines |
US4302941A (en) * | 1980-04-02 | 1981-12-01 | United Technologies Corporation | Combuster liner construction for gas turbine engine |
-
1992
- 1992-07-18 DE DE4223733A patent/DE4223733C2/de not_active Expired - Lifetime
-
1993
- 1993-07-16 US US08/093,093 patent/US5419114A/en not_active Expired - Lifetime
- 1993-07-19 IT IT93MI001585A patent/IT1265170B1/it active IP Right Grant
Also Published As
Publication number | Publication date |
---|---|
IT1265170B1 (it) | 1996-10-31 |
ITMI931585A0 (it) | 1993-07-19 |
ITMI931585A1 (it) | 1995-01-19 |
US5419114A (en) | 1995-05-30 |
DE4223733A1 (de) | 1994-01-20 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
OM8 | Search report available as to paragraph 43 lit. 1 sentence 1 patent law | ||
8110 | Request for examination paragraph 44 | ||
D2 | Grant after examination | ||
8364 | No opposition during term of opposition | ||
8327 | Change in the person/name/address of the patent owner |
Owner name: GHH BORSIG TURBOMASCHINEN GMBH, 46145 OBERHAUSEN, |
|
8327 | Change in the person/name/address of the patent owner |
Owner name: MAN TURBOMASCHINEN AG GHH BORSIG, 46145 OBERHAUSEN |
|
8327 | Change in the person/name/address of the patent owner |
Owner name: MAN DIESEL & TURBO SE, 86153 AUGSBURG, DE |
|
R081 | Change of applicant/patentee |
Owner name: MAN DIESEL & TURBO SE, DE Free format text: FORMER OWNER: MAN TURBOMASCHINEN AG GHH BORSIG, 46145 OBERHAUSEN, DE Effective date: 20110325 |
|
R071 | Expiry of right | ||
R071 | Expiry of right |