DE60027679T2 - Gekühlte Turbinenschaufel mit schrägen und sparrenförmige Wirbelerzeugern - Google Patents
Gekühlte Turbinenschaufel mit schrägen und sparrenförmige Wirbelerzeugern Download PDFInfo
- Publication number
- DE60027679T2 DE60027679T2 DE60027679T DE60027679T DE60027679T2 DE 60027679 T2 DE60027679 T2 DE 60027679T2 DE 60027679 T DE60027679 T DE 60027679T DE 60027679 T DE60027679 T DE 60027679T DE 60027679 T2 DE60027679 T2 DE 60027679T2
- Authority
- DE
- Germany
- Prior art keywords
- channel
- blade
- flow
- oblique
- swirlers
- 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.)
- Revoked
Links
- 239000002826 coolant Substances 0.000 claims description 55
- 238000005192 partition Methods 0.000 claims description 14
- 238000000034 method Methods 0.000 claims description 10
- 238000001816 cooling Methods 0.000 description 33
- 210000002414 leg Anatomy 0.000 description 8
- 239000000567 combustion gas Substances 0.000 description 4
- 230000000295 complement effect Effects 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 239000007789 gas Substances 0.000 description 3
- 230000008901 benefit Effects 0.000 description 2
- 238000002485 combustion reaction Methods 0.000 description 2
- 239000003507 refrigerant Substances 0.000 description 2
- 101001094044 Mus musculus Solute carrier family 26 member 6 Proteins 0.000 description 1
- 230000001154 acute effect Effects 0.000 description 1
- WYTGDNHDOZPMIW-RCBQFDQVSA-N alstonine Natural products C1=CC2=C3C=CC=CC3=NC2=C2N1C[C@H]1[C@H](C)OC=C(C(=O)OC)[C@H]1C2 WYTGDNHDOZPMIW-RCBQFDQVSA-N 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 239000000835 fiber Substances 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 229920000136 polysorbate Polymers 0.000 description 1
- 238000005057 refrigeration Methods 0.000 description 1
- 210000000689 upper leg Anatomy 0.000 description 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
- F01D5/187—Convection cooling
-
- 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
- F05D2250/30—Arrangement of components
- F05D2250/31—Arrangement of components according to the direction of their main axis or their axis of rotation
- F05D2250/314—Arrangement of components according to the direction of their main axis or their axis of rotation the axes being inclined in relation to each other
-
- 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
-
- 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)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US09/466,155 US6331098B1 (en) | 1999-12-18 | 1999-12-18 | Coriolis turbulator blade |
| US466155 | 1999-12-18 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| DE60027679D1 DE60027679D1 (de) | 2006-06-08 |
| DE60027679T2 true DE60027679T2 (de) | 2007-05-03 |
Family
ID=23850721
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DE60027679T Revoked DE60027679T2 (de) | 1999-12-18 | 2000-12-15 | Gekühlte Turbinenschaufel mit schrägen und sparrenförmige Wirbelerzeugern |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US6331098B1 (enExample) |
| EP (1) | EP1111190B1 (enExample) |
| JP (1) | JP4739509B2 (enExample) |
| DE (1) | DE60027679T2 (enExample) |
Families Citing this family (68)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6474947B1 (en) * | 1998-03-13 | 2002-11-05 | Mitsubishi Heavy Industries, Ltd. | Film cooling hole construction in gas turbine moving-vanes |
| US6511762B1 (en) * | 2000-11-06 | 2003-01-28 | General Electric Company | Multi-layer thermal barrier coating with transpiration cooling |
| US6910620B2 (en) * | 2002-10-15 | 2005-06-28 | General Electric Company | Method for providing turbulation on the inner surface of holes in an article, and related articles |
| US6932573B2 (en) | 2003-04-30 | 2005-08-23 | Siemens Westinghouse Power Corporation | Turbine blade having a vortex forming cooling system for a trailing edge |
| US6955525B2 (en) * | 2003-08-08 | 2005-10-18 | Siemens Westinghouse Power Corporation | Cooling system for an outer wall of a turbine blade |
| US6984102B2 (en) | 2003-11-19 | 2006-01-10 | General Electric Company | Hot gas path component with mesh and turbulated cooling |
| US7186084B2 (en) | 2003-11-19 | 2007-03-06 | General Electric Company | Hot gas path component with mesh and dimpled cooling |
| US7114923B2 (en) * | 2004-06-17 | 2006-10-03 | Siemens Power Generation, Inc. | Cooling system for a showerhead of a turbine blade |
| DE502004003477D1 (de) * | 2004-07-05 | 2007-05-24 | Siemens Ag | Filmgekühlte Turbinenschaufel |
| US7094031B2 (en) * | 2004-09-09 | 2006-08-22 | General Electric Company | Offset Coriolis turbulator blade |
| US7128533B2 (en) * | 2004-09-10 | 2006-10-31 | Siemens Power Generation, Inc. | Vortex cooling system for a turbine blade |
| US7156620B2 (en) * | 2004-12-21 | 2007-01-02 | Pratt & Whitney Canada Corp. | Internally cooled gas turbine airfoil and method |
| US7156619B2 (en) * | 2004-12-21 | 2007-01-02 | Pratt & Whitney Canada Corp. | Internally cooled gas turbine airfoil and method |
| US7189060B2 (en) * | 2005-01-07 | 2007-03-13 | Siemens Power Generation, Inc. | Cooling system including mini channels within a turbine blade of a turbine engine |
| US7435053B2 (en) * | 2005-03-29 | 2008-10-14 | Siemens Power Generation, Inc. | Turbine blade cooling system having multiple serpentine trailing edge cooling channels |
| US7534089B2 (en) | 2006-07-18 | 2009-05-19 | Siemens Energy, Inc. | Turbine airfoil with near wall multi-serpentine cooling channels |
| US7549844B2 (en) * | 2006-08-24 | 2009-06-23 | Siemens Energy, Inc. | Turbine airfoil cooling system with bifurcated and recessed trailing edge exhaust channels |
| US7637720B1 (en) | 2006-11-16 | 2009-12-29 | Florida Turbine Technologies, Inc. | Turbulator for a turbine airfoil cooling passage |
| US7914257B1 (en) | 2007-01-17 | 2011-03-29 | Florida Turbine Technologies, Inc. | Turbine rotor blade with spiral and serpentine flow cooling circuit |
| US8083485B2 (en) * | 2007-08-15 | 2011-12-27 | United Technologies Corporation | Angled tripped airfoil peanut cavity |
| US8366383B2 (en) * | 2007-11-13 | 2013-02-05 | United Technologies Corporation | Air sealing element |
| US7988410B1 (en) * | 2007-11-19 | 2011-08-02 | Florida Turbine Technologies, Inc. | Blade tip shroud with circular grooves |
| US8210814B2 (en) * | 2008-06-18 | 2012-07-03 | General Electric Company | Crossflow turbine airfoil |
| US8303252B2 (en) * | 2008-10-16 | 2012-11-06 | United Technologies Corporation | Airfoil with cooling passage providing variable heat transfer rate |
| US8079813B2 (en) * | 2009-01-19 | 2011-12-20 | Siemens Energy, Inc. | Turbine blade with multiple trailing edge cooling slots |
| US8167558B2 (en) * | 2009-01-19 | 2012-05-01 | Siemens Energy, Inc. | Modular serpentine cooling systems for turbine engine components |
| US8894367B2 (en) * | 2009-08-06 | 2014-11-25 | Siemens Energy, Inc. | Compound cooling flow turbulator for turbine component |
| US8920122B2 (en) | 2012-03-12 | 2014-12-30 | Siemens Energy, Inc. | Turbine airfoil with an internal cooling system having vortex forming turbulators |
| US9388700B2 (en) * | 2012-03-16 | 2016-07-12 | United Technologies Corporation | Gas turbine engine airfoil cooling circuit |
| US8876475B1 (en) * | 2012-04-27 | 2014-11-04 | Florida Turbine Technologies, Inc. | Turbine blade with radial cooling passage having continuous discrete turbulence air mixers |
| US9157329B2 (en) * | 2012-08-22 | 2015-10-13 | United Technologies Corporation | Gas turbine engine airfoil internal cooling features |
| US9995148B2 (en) | 2012-10-04 | 2018-06-12 | General Electric Company | Method and apparatus for cooling gas turbine and rotor blades |
| US8920123B2 (en) * | 2012-12-14 | 2014-12-30 | Siemens Aktiengesellschaft | Turbine blade with integrated serpentine and axial tip cooling circuits |
| US10316668B2 (en) | 2013-02-05 | 2019-06-11 | United Technologies Corporation | Gas turbine engine component having curved turbulator |
| US9850762B2 (en) | 2013-03-13 | 2017-12-26 | General Electric Company | Dust mitigation for turbine blade tip turns |
| EP2971543B1 (en) | 2013-03-15 | 2020-08-19 | United Technologies Corporation | Gas turbine engine component having shaped pedestals |
| US8985949B2 (en) * | 2013-04-29 | 2015-03-24 | Siemens Aktiengesellschaft | Cooling system including wavy cooling chamber in a trailing edge portion of an airfoil assembly |
| US9091495B2 (en) | 2013-05-14 | 2015-07-28 | Siemens Aktiengesellschaft | Cooling passage including turbulator system in a turbine engine component |
| US9500093B2 (en) * | 2013-09-26 | 2016-11-22 | Pratt & Whitney Canada Corp. | Internally cooled airfoil |
| FR3020402B1 (fr) * | 2014-04-24 | 2019-06-14 | Safran Aircraft Engines | Aube pour turbine de turbomachine comprenant un circuit de refroidissement a homogeneite amelioree |
| EP3149284A2 (en) | 2014-05-29 | 2017-04-05 | General Electric Company | Engine components with impingement cooling features |
| WO2015184294A1 (en) | 2014-05-29 | 2015-12-03 | General Electric Company | Fastback turbulator |
| US10364684B2 (en) | 2014-05-29 | 2019-07-30 | General Electric Company | Fastback vorticor pin |
| US10422235B2 (en) | 2014-05-29 | 2019-09-24 | General Electric Company | Angled impingement inserts with cooling features |
| US9957816B2 (en) | 2014-05-29 | 2018-05-01 | General Electric Company | Angled impingement insert |
| EP3194726B1 (en) | 2014-09-18 | 2020-04-15 | Siemens Aktiengesellschaft | Gas turbine airfoil including integrated leading edge and tip cooling fluid passage and core structure used for forming such an airfoil |
| US10233775B2 (en) | 2014-10-31 | 2019-03-19 | General Electric Company | Engine component for a gas turbine engine |
| US10280785B2 (en) | 2014-10-31 | 2019-05-07 | General Electric Company | Shroud assembly for a turbine engine |
| US10605094B2 (en) | 2015-01-21 | 2020-03-31 | United Technologies Corporation | Internal cooling cavity with trip strips |
| US10156157B2 (en) * | 2015-02-13 | 2018-12-18 | United Technologies Corporation | S-shaped trip strips in internally cooled components |
| CN107429569B (zh) | 2015-04-03 | 2019-09-24 | 西门子公司 | 具有低流动框架式通道的涡轮动叶后缘 |
| US9995146B2 (en) * | 2015-04-29 | 2018-06-12 | General Electric Company | Turbine airfoil turbulator arrangement |
| US10830051B2 (en) * | 2015-12-11 | 2020-11-10 | General Electric Company | Engine component with film cooling |
| US20170175532A1 (en) * | 2015-12-21 | 2017-06-22 | United Technologies Corporation | Angled heat transfer pedestal |
| CN108884717B (zh) * | 2016-03-31 | 2021-02-26 | 西门子股份公司 | 在冷壁上具有湍流特征的涡轮翼型件 |
| US10208604B2 (en) * | 2016-04-27 | 2019-02-19 | United Technologies Corporation | Cooling features with three dimensional chevron geometry |
| US10502068B2 (en) | 2016-12-02 | 2019-12-10 | General Electric Company | Engine with chevron pin bank |
| US10801724B2 (en) | 2017-06-14 | 2020-10-13 | General Electric Company | Method and apparatus for minimizing cross-flow across an engine cooling hole |
| US11149555B2 (en) | 2017-06-14 | 2021-10-19 | General Electric Company | Turbine engine component with deflector |
| US10590778B2 (en) | 2017-08-03 | 2020-03-17 | General Electric Company | Engine component with non-uniform chevron pins |
| US10577944B2 (en) | 2017-08-03 | 2020-03-03 | General Electric Company | Engine component with hollow turbulators |
| US11408302B2 (en) * | 2017-10-13 | 2022-08-09 | Raytheon Technologies Corporation | Film cooling hole arrangement for gas turbine engine component |
| WO2020013863A1 (en) * | 2018-07-13 | 2020-01-16 | Siemens Aktiengesellschaft | Airfoil for a turbine engine incorporating pins |
| US10787932B2 (en) * | 2018-07-13 | 2020-09-29 | Honeywell International Inc. | Turbine blade with dust tolerant cooling system |
| KR102161765B1 (ko) * | 2019-02-22 | 2020-10-05 | 두산중공업 주식회사 | 터빈용 에어포일, 이를 포함하는 터빈 |
| CN111648830B (zh) * | 2020-05-14 | 2021-04-20 | 西安交通大学 | 一种用于涡轮动叶后部的内冷带肋通道 |
| CN114215609B (zh) * | 2021-12-30 | 2023-07-04 | 华中科技大学 | 一种可强化冷却的叶片内冷通道及其应用 |
| JP2023165485A (ja) * | 2022-05-06 | 2023-11-16 | 三菱重工業株式会社 | タービン翼及びガスタービン |
Family Cites Families (23)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1410014A (en) * | 1971-12-14 | 1975-10-15 | Rolls Royce | Gas turbine engine blade |
| US4416585A (en) | 1980-01-17 | 1983-11-22 | Pratt & Whitney Aircraft Of Canada Limited | Blade cooling for gas turbine engine |
| US4775296A (en) | 1981-12-28 | 1988-10-04 | United Technologies Corporation | Coolable airfoil for a rotary machine |
| US4474532A (en) | 1981-12-28 | 1984-10-02 | United Technologies Corporation | Coolable airfoil for a rotary machine |
| US4515626A (en) | 1982-10-06 | 1985-05-07 | Ciba Geigy Corporation | N-(Cyclopropyl-triazinyl-n'-(arylsulfonyl) ureas having herbicidal activity |
| JPS60101202A (ja) * | 1983-06-20 | 1985-06-05 | ゼネラル・エレクトリツク・カンパニイ | 角度をつけた乱流促進装置 |
| US4514144A (en) | 1983-06-20 | 1985-04-30 | General Electric Company | Angled turbulence promoter |
| US5052889A (en) | 1990-05-17 | 1991-10-01 | Pratt & Whintey Canada | Offset ribs for heat transfer surface |
| JP3006174B2 (ja) | 1991-07-04 | 2000-02-07 | 株式会社日立製作所 | 内部に冷却通路を有する部材 |
| US5700132A (en) * | 1991-12-17 | 1997-12-23 | General Electric Company | Turbine blade having opposing wall turbulators |
| US5681144A (en) | 1991-12-17 | 1997-10-28 | General Electric Company | Turbine blade having offset turbulators |
| US5203676A (en) * | 1992-03-05 | 1993-04-20 | Westinghouse Electric Corp. | Ruggedized tapered twisted integral shroud blade |
| US5403157A (en) | 1993-12-08 | 1995-04-04 | United Technologies Corporation | Heat exchange means for obtaining temperature gradient balance |
| US5536143A (en) * | 1995-03-31 | 1996-07-16 | General Electric Co. | Closed circuit steam cooled bucket |
| US5842829A (en) * | 1996-09-26 | 1998-12-01 | General Electric Co. | Cooling circuits for trailing edge cavities in airfoils |
| US5797726A (en) * | 1997-01-03 | 1998-08-25 | General Electric Company | Turbulator configuration for cooling passages or rotor blade in a gas turbine engine |
| JPH10266803A (ja) * | 1997-03-25 | 1998-10-06 | Mitsubishi Heavy Ind Ltd | ガスタービン冷却動翼 |
| JPH10280905A (ja) * | 1997-04-02 | 1998-10-20 | Mitsubishi Heavy Ind Ltd | ガスタービン冷却翼のタービュレータ |
| JPH10306701A (ja) * | 1997-05-08 | 1998-11-17 | Toshiba Corp | タービン動翼およびその製造方法 |
| JP3790328B2 (ja) * | 1997-05-28 | 2006-06-28 | 三菱重工業株式会社 | ガスタービンの冷却翼 |
| JPH11193701A (ja) * | 1997-10-31 | 1999-07-21 | General Electric Co <Ge> | タービン翼 |
| JPH11241602A (ja) * | 1998-02-26 | 1999-09-07 | Toshiba Corp | ガスタービン翼 |
| US6174134B1 (en) * | 1999-03-05 | 2001-01-16 | General Electric Company | Multiple impingement airfoil cooling |
-
1999
- 1999-12-18 US US09/466,155 patent/US6331098B1/en not_active Expired - Lifetime
-
2000
- 2000-12-15 DE DE60027679T patent/DE60027679T2/de not_active Revoked
- 2000-12-15 JP JP2000381145A patent/JP4739509B2/ja not_active Expired - Fee Related
- 2000-12-15 EP EP00311244A patent/EP1111190B1/en not_active Revoked
Also Published As
| Publication number | Publication date |
|---|---|
| EP1111190B1 (en) | 2006-05-03 |
| DE60027679D1 (de) | 2006-06-08 |
| US6331098B1 (en) | 2001-12-18 |
| JP2001234702A (ja) | 2001-08-31 |
| JP4739509B2 (ja) | 2011-08-03 |
| EP1111190A1 (en) | 2001-06-27 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| 8363 | Opposition against the patent | ||
| 8331 | Complete revocation |