ATE388303T1 - Heissgas führendes gassammelrohr mit luftkühlung - Google Patents
Heissgas führendes gassammelrohr mit luftkühlungInfo
- Publication number
- ATE388303T1 ATE388303T1 AT03015750T AT03015750T ATE388303T1 AT E388303 T1 ATE388303 T1 AT E388303T1 AT 03015750 T AT03015750 T AT 03015750T AT 03015750 T AT03015750 T AT 03015750T AT E388303 T1 ATE388303 T1 AT E388303T1
- Authority
- AT
- Austria
- Prior art keywords
- gas
- air cooling
- collection tube
- inlets
- hot gas
- Prior art date
Links
- 238000002485 combustion reaction Methods 0.000 abstract 1
- 238000001816 cooling Methods 0.000 abstract 1
- 230000008878 coupling Effects 0.000 abstract 1
- 238000010168 coupling process Methods 0.000 abstract 1
- 238000005859 coupling reaction Methods 0.000 abstract 1
- 239000000203 mixture Substances 0.000 abstract 1
- 230000002787 reinforcement Effects 0.000 abstract 1
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
- 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
- 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
- F05D2260/221—Improvement of heat transfer
- F05D2260/2214—Improvement of heat transfer by increasing the heat transfer surface
- F05D2260/22141—Improvement of heat transfer by increasing the heat transfer surface using fins or ribs
-
- 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
- F05D2260/94—Functionality given by mechanical stress related aspects such as low cycle fatigue [LCF] of high cycle fatigue [HCF]
-
- 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
- F05D2260/94—Functionality given by mechanical stress related aspects such as low cycle fatigue [LCF] of high cycle fatigue [HCF]
- F05D2260/941—Functionality given by mechanical stress related aspects such as low cycle fatigue [LCF] of high cycle fatigue [HCF] particularly aimed at mechanical or thermal stress reduction
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
- Sampling And Sample Adjustment (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE10239534A DE10239534A1 (de) | 2002-08-23 | 2002-08-23 | Heißgas führendes Gassammelrohr |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ATE388303T1 true ATE388303T1 (de) | 2008-03-15 |
Family
ID=30775573
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AT03015750T ATE388303T1 (de) | 2002-08-23 | 2003-07-10 | Heissgas führendes gassammelrohr mit luftkühlung |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US6996992B2 (de) |
| EP (1) | EP1391583B1 (de) |
| JP (1) | JP2007046456A (de) |
| CN (1) | CN1255623C (de) |
| AT (1) | ATE388303T1 (de) |
| CA (1) | CA2424166C (de) |
| DE (2) | DE10239534A1 (de) |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2157285A1 (de) * | 2008-08-21 | 2010-02-24 | Siemens Aktiengesellschaft | Gasturbineanordnung und Verfahren zur Turbinenanströmung |
| EP2157286A1 (de) * | 2008-08-21 | 2010-02-24 | Siemens Aktiengesellschaft | Gasturbine mit angewinkeltem Mischgehäuse und Verfahren zur Turbinenanströmung |
| USD818502S1 (en) * | 2015-12-17 | 2018-05-22 | General Electric Company | Turbocharger transition section |
| USD814522S1 (en) * | 2016-06-21 | 2018-04-03 | General Electric Company | Transition section for a turbocharged engine |
Family Cites Families (22)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB624285A (en) | 1946-07-01 | 1949-06-01 | Westinghouse Electric Int Co | Improvements in or relating to combustion apparatus |
| US2526281A (en) * | 1947-04-10 | 1950-10-17 | Wright Aeronautical Corp | Turbine and turbine nozzle construction |
| CH599458A5 (en) | 1976-12-24 | 1978-05-31 | Sim Sa Ets | Air cooled internal combustion engine |
| CH633347A5 (de) * | 1978-08-03 | 1982-11-30 | Bbc Brown Boveri & Cie | Gasturbine. |
| DE3314720A1 (de) | 1983-04-22 | 1984-10-25 | KHD Canada Inc. Deutz R & D Devision, Montreal, Quebec | Zylinderkopf fuer eine luftgekuehlte hubkolbenbrennkraftmaschine |
| JPS62131927A (ja) * | 1985-12-04 | 1987-06-15 | Hitachi Ltd | ガスタ−ビン燃焼器尾筒の冷却構造 |
| GB2261281B (en) | 1991-11-08 | 1995-01-18 | Bmw Rolls Royce Gmbh | A combustion-chamber casting for a gas turbine |
| US5274991A (en) * | 1992-03-30 | 1994-01-04 | General Electric Company | Dry low NOx multi-nozzle combustion liner cap assembly |
| DE4242721A1 (de) * | 1992-12-17 | 1994-06-23 | Asea Brown Boveri | Gasturbinenbrennkammer |
| EP0718468B1 (de) * | 1994-12-20 | 2001-10-31 | General Electric Company | Verstärkungrahmen für Gasturbinenbrennkammerendstück |
| JPH1026022A (ja) | 1996-07-10 | 1998-01-27 | Yanmar Diesel Engine Co Ltd | 空冷式内燃機関の排気系構造 |
| US6018950A (en) * | 1997-06-13 | 2000-02-01 | Siemens Westinghouse Power Corporation | Combustion turbine modular cooling panel |
| GB2328011A (en) * | 1997-08-05 | 1999-02-10 | Europ Gas Turbines Ltd | Combustor for gas or liquid fuelled turbine |
| DE19815473A1 (de) * | 1998-04-07 | 1999-10-14 | Ghh Borsig Turbomaschinen Gmbh | Heißgasführendes Gassammelrohr einer Gasturbine |
| JP2895831B1 (ja) * | 1998-04-22 | 1999-05-24 | 川崎重工業株式会社 | スクロールの冷却を改善したガスタービン |
| GB9813972D0 (en) * | 1998-06-30 | 1998-08-26 | Rolls Royce Plc | A combustion chamber |
| US6196793B1 (en) * | 1999-01-11 | 2001-03-06 | General Electric Company | Nozzle box |
| GB2361302A (en) | 2000-04-13 | 2001-10-17 | Rolls Royce Plc | Discharge nozzle for a gas turbine engine combustion chamber |
| JP3478531B2 (ja) * | 2000-04-21 | 2003-12-15 | 川崎重工業株式会社 | ガスタービンのセラミック部品支持構造 |
| DE10032454A1 (de) * | 2000-07-04 | 2002-01-17 | Man Turbomasch Ag Ghh Borsig | Vorrichtung zum Kühlen eines ungleichmäßig stark temperaturbelasteten Bauteiles |
| DE10064264B4 (de) * | 2000-12-22 | 2017-03-23 | General Electric Technology Gmbh | Anordnung zur Kühlung eines Bauteils |
| US6675584B1 (en) * | 2002-08-15 | 2004-01-13 | Power Systems Mfg, Llc | Coated seal article used in turbine engines |
-
2002
- 2002-08-23 DE DE10239534A patent/DE10239534A1/de not_active Withdrawn
-
2003
- 2003-03-17 US US10/390,407 patent/US6996992B2/en not_active Expired - Fee Related
- 2003-04-01 CA CA002424166A patent/CA2424166C/en not_active Expired - Fee Related
- 2003-04-24 CN CNB031220525A patent/CN1255623C/zh not_active Expired - Fee Related
- 2003-07-08 JP JP2003193957A patent/JP2007046456A/ja active Pending
- 2003-07-10 DE DE50309297T patent/DE50309297D1/de not_active Expired - Lifetime
- 2003-07-10 EP EP03015750A patent/EP1391583B1/de not_active Expired - Lifetime
- 2003-07-10 AT AT03015750T patent/ATE388303T1/de not_active IP Right Cessation
Also Published As
| Publication number | Publication date |
|---|---|
| EP1391583A1 (de) | 2004-02-25 |
| CN1255623C (zh) | 2006-05-10 |
| EP1391583B1 (de) | 2008-03-05 |
| US20040035116A1 (en) | 2004-02-26 |
| JP2007046456A (ja) | 2007-02-22 |
| CA2424166A1 (en) | 2004-02-23 |
| DE10239534A1 (de) | 2004-04-22 |
| CA2424166C (en) | 2008-09-09 |
| CN1477298A (zh) | 2004-02-25 |
| DE50309297D1 (de) | 2008-04-17 |
| US6996992B2 (en) | 2006-02-14 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| REN | Ceased due to non-payment of the annual fee |