DE3675690D1 - Prallkuehlung fuer einen turbineneinlasskanal. - Google Patents
Prallkuehlung fuer einen turbineneinlasskanal.Info
- Publication number
- DE3675690D1 DE3675690D1 DE8686106295T DE3675690T DE3675690D1 DE 3675690 D1 DE3675690 D1 DE 3675690D1 DE 8686106295 T DE8686106295 T DE 8686106295T DE 3675690 T DE3675690 T DE 3675690T DE 3675690 D1 DE3675690 D1 DE 3675690D1
- Authority
- DE
- Germany
- Prior art keywords
- inlet channel
- turbine inlet
- impact cooling
- impact
- cooling
- 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
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/08—Cooling; Heating; Heat-insulation
- F01D25/12—Cooling
-
- 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
- F23R3/002—Wall structures
-
- 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
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/201—Heat transfer, e.g. cooling by impingement of a fluid
-
- 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
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/202—Heat transfer, e.g. cooling by film cooling
-
- 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
- F23R2900/03044—Impingement cooled combustion chamber walls or subassemblies
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Devices That Are Associated With Refrigeration Equipment (AREA)
- Heat Treatments In General, Especially Conveying And Cooling (AREA)
- Transition And Organic Metals Composition Catalysts For Addition Polymerization (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US73401885A | 1985-05-14 | 1985-05-14 |
Publications (1)
Publication Number | Publication Date |
---|---|
DE3675690D1 true DE3675690D1 (de) | 1991-01-03 |
Family
ID=24950020
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE8686106295T Expired - Lifetime DE3675690D1 (de) | 1985-05-14 | 1986-05-07 | Prallkuehlung fuer einen turbineneinlasskanal. |
Country Status (6)
Country | Link |
---|---|
EP (1) | EP0203431B2 (de) |
JP (1) | JPS629157A (de) |
AU (1) | AU593551B2 (de) |
CA (1) | CA1263243A (de) |
DE (1) | DE3675690D1 (de) |
NO (1) | NO162887C (de) |
Families Citing this family (28)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5157188A (en) * | 1985-03-19 | 1992-10-20 | Phillips Petroleum Company | Methane conversion |
JPH0752014B2 (ja) * | 1986-03-20 | 1995-06-05 | 株式会社日立製作所 | ガスタ−ビン燃焼器 |
US4984429A (en) * | 1986-11-25 | 1991-01-15 | General Electric Company | Impingement cooled liner for dry low NOx venturi combustor |
CA1309873C (en) * | 1987-04-01 | 1992-11-10 | Graham P. Butt | Gas turbine combustor transition duct forced convection cooling |
GB2221979B (en) * | 1988-08-17 | 1992-03-25 | Rolls Royce Plc | A combustion chamber for a gas turbine engine |
DE4239856A1 (de) * | 1992-11-27 | 1994-06-01 | Asea Brown Boveri | Gasturbinenbrennkammer |
FR2714154B1 (fr) * | 1993-12-22 | 1996-01-19 | Snecma | Chambre de combustion comportant une paroi munie d'une multiperforation. |
DE19720786A1 (de) * | 1997-05-17 | 1998-11-19 | Abb Research Ltd | Brennkammer |
GB2328011A (en) * | 1997-08-05 | 1999-02-10 | Europ Gas Turbines Ltd | Combustor for gas or liquid fuelled turbine |
US6494044B1 (en) * | 1999-11-19 | 2002-12-17 | General Electric Company | Aerodynamic devices for enhancing sidepanel cooling on an impingement cooled transition duct and related method |
EP1146289B1 (de) * | 2000-04-13 | 2008-12-24 | Mitsubishi Heavy Industries, Ltd. | Kühlstruktur für das Endstück einer Gasturbinenbrennkammer |
DE10064264B4 (de) * | 2000-12-22 | 2017-03-23 | General Electric Technology Gmbh | Anordnung zur Kühlung eines Bauteils |
US7010921B2 (en) * | 2004-06-01 | 2006-03-14 | General Electric Company | Method and apparatus for cooling combustor liner and transition piece of a gas turbine |
EP1650503A1 (de) * | 2004-10-25 | 2006-04-26 | Siemens Aktiengesellschaft | Verfahren zur Kühlung eines Hitzeschildelements und Hitzeschildelement |
US7571611B2 (en) * | 2006-04-24 | 2009-08-11 | General Electric Company | Methods and system for reducing pressure losses in gas turbine engines |
US7878002B2 (en) * | 2007-04-17 | 2011-02-01 | General Electric Company | Methods and systems to facilitate reducing combustor pressure drops |
EP2245374B1 (de) | 2008-02-20 | 2017-11-15 | General Electric Technology GmbH | Thermische maschine |
US8474266B2 (en) * | 2009-07-24 | 2013-07-02 | General Electric Company | System and method for a gas turbine combustor having a bleed duct from a diffuser to a fuel nozzle |
US8516822B2 (en) * | 2010-03-02 | 2013-08-27 | General Electric Company | Angled vanes in combustor flow sleeve |
US8252251B2 (en) * | 2010-03-30 | 2012-08-28 | General Electric Company | Fluid cooled reformer and method for cooling a reformer |
US8359867B2 (en) * | 2010-04-08 | 2013-01-29 | General Electric Company | Combustor having a flow sleeve |
US8276391B2 (en) * | 2010-04-19 | 2012-10-02 | General Electric Company | Combustor liner cooling at transition duct interface and related method |
US9506359B2 (en) * | 2012-04-03 | 2016-11-29 | General Electric Company | Transition nozzle combustion system |
US9447971B2 (en) * | 2012-05-02 | 2016-09-20 | General Electric Company | Acoustic resonator located at flow sleeve of gas turbine combustor |
EP2738469B1 (de) * | 2012-11-30 | 2019-04-17 | Ansaldo Energia IP UK Limited | Verbrennungskammerteil einer Gasturbine mit wandnaher Kühlanordnung |
US10100738B2 (en) * | 2015-01-20 | 2018-10-16 | United Technologies Corporation | Overcooled air cooling system with annular mixing passage |
US10415478B2 (en) | 2015-01-20 | 2019-09-17 | United Technologies Corporation | Air mixing systems having mixing chambers for gas turbine engines |
WO2020092896A1 (en) * | 2018-11-02 | 2020-05-07 | Chromalloy Gas Turbine Llc | System and method for providing compressed air to a gas turbine combustor |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2873944A (en) * | 1952-09-10 | 1959-02-17 | Gen Motors Corp | Turbine blade cooling |
GB849255A (en) * | 1956-11-01 | 1960-09-21 | Josef Cermak | Method of and arrangements for cooling the walls of combustion spaces and other spaces subject to high thermal stresses |
GB1070480A (en) * | 1966-02-01 | 1967-06-01 | Rolls Royce | Aerofoil shaped blade for a fluid flow machine such as a gas turbine engine |
US3652181A (en) * | 1970-11-23 | 1972-03-28 | Carl F Wilhelm Jr | Cooling sleeve for gas turbine combustor transition member |
US3806276A (en) * | 1972-08-30 | 1974-04-23 | Gen Motors Corp | Cooled turbine blade |
FR2221020A5 (de) * | 1973-03-09 | 1974-10-04 | Gen Electric | |
JPS5098105U (de) * | 1974-01-12 | 1975-08-15 | ||
CH584833A5 (de) * | 1975-05-16 | 1977-02-15 | Bbc Brown Boveri & Cie | |
JPS5443123A (en) * | 1977-09-12 | 1979-04-05 | Furukawa Electric Co Ltd:The | High tensile electric condictive copper alloy |
CH633347A5 (de) * | 1978-08-03 | 1982-11-30 | Bbc Brown Boveri & Cie | Gasturbine. |
US4526226A (en) * | 1981-08-31 | 1985-07-02 | General Electric Company | Multiple-impingement cooled structure |
CA1193551A (en) * | 1981-12-31 | 1985-09-17 | Paul C. Holden | Shell-spar cooled airfoil having variable coolant passageway area |
JPS58197402A (ja) * | 1982-05-14 | 1983-11-17 | Hitachi Ltd | ガスタ−ビン翼 |
-
1986
- 1986-04-25 CA CA000507566A patent/CA1263243A/en not_active Expired
- 1986-05-07 DE DE8686106295T patent/DE3675690D1/de not_active Expired - Lifetime
- 1986-05-07 EP EP19860106295 patent/EP0203431B2/de not_active Expired - Lifetime
- 1986-05-12 JP JP10690486A patent/JPS629157A/ja active Granted
- 1986-05-12 AU AU57353/86A patent/AU593551B2/en not_active Ceased
- 1986-05-13 NO NO861900A patent/NO162887C/no not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
JPS629157A (ja) | 1987-01-17 |
NO162887B (no) | 1989-11-20 |
JPH0524337B2 (de) | 1993-04-07 |
NO861900L (no) | 1986-11-17 |
CA1263243A (en) | 1989-11-28 |
EP0203431B2 (de) | 1996-05-22 |
AU5735386A (en) | 1986-11-20 |
EP0203431A1 (de) | 1986-12-03 |
AU593551B2 (en) | 1990-02-15 |
EP0203431B1 (de) | 1990-11-22 |
NO162887C (no) | 1990-02-28 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8363 | Opposition against the patent | ||
8366 | Restricted maintained after opposition proceedings |