ATE327415T1 - Luftfilmgekühlte mikrokreislauf und bauteil und herstellungsverfahren für ein solches bauteil - Google Patents
Luftfilmgekühlte mikrokreislauf und bauteil und herstellungsverfahren für ein solches bauteilInfo
- Publication number
- ATE327415T1 ATE327415T1 AT03253895T AT03253895T ATE327415T1 AT E327415 T1 ATE327415 T1 AT E327415T1 AT 03253895 T AT03253895 T AT 03253895T AT 03253895 T AT03253895 T AT 03253895T AT E327415 T1 ATE327415 T1 AT E327415T1
- Authority
- AT
- Austria
- Prior art keywords
- component
- production method
- air film
- film cooled
- micro circuit
- Prior art date
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
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F13/00—Arrangements for modifying heat-transfer, e.g. increasing, decreasing
- F28F13/02—Arrangements for modifying heat-transfer, e.g. increasing, decreasing by influencing fluid boundary
-
- 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
- F23R3/005—Combined with pressure or heat exchangers
-
- 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
- F23R2900/00018—Manufacturing combustion chamber liners or subparts
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D21/00—Heat-exchange apparatus not covered by any of the groups F28D1/00 - F28D20/00
- F28D2021/0019—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for
- F28D2021/0077—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for for tempering, e.g. with cooling or heating circuits for temperature control of elements
- F28D2021/0078—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for for tempering, e.g. with cooling or heating circuits for temperature control of elements in the form of cooling walls
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F2260/00—Heat exchangers or heat exchange elements having special size, e.g. microstructures
- F28F2260/02—Heat exchangers or heat exchange elements having special size, e.g. microstructures having microchannels
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
- Thermal Sciences (AREA)
- Chemical & Material Sciences (AREA)
- Physics & Mathematics (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Encapsulation Of And Coatings For Semiconductor Or Solid State Devices (AREA)
- Cooling Or The Like Of Semiconductors Or Solid State Devices (AREA)
- Micromachines (AREA)
- Extrusion Moulding Of Plastics Or The Like (AREA)
- Press Drives And Press Lines (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10/176,458 US7137776B2 (en) | 2002-06-19 | 2002-06-19 | Film cooling for microcircuits |
Publications (1)
Publication Number | Publication Date |
---|---|
ATE327415T1 true ATE327415T1 (de) | 2006-06-15 |
Family
ID=29717840
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT03253895T ATE327415T1 (de) | 2002-06-19 | 2003-06-19 | Luftfilmgekühlte mikrokreislauf und bauteil und herstellungsverfahren für ein solches bauteil |
Country Status (11)
Country | Link |
---|---|
US (1) | US7137776B2 (de) |
EP (1) | EP1377140B1 (de) |
JP (1) | JP2004044588A (de) |
KR (1) | KR100705116B1 (de) |
AT (1) | ATE327415T1 (de) |
AU (1) | AU2003204541B2 (de) |
CA (1) | CA2432490A1 (de) |
DE (1) | DE60305385T2 (de) |
DK (1) | DK1377140T3 (de) |
IL (1) | IL156301A0 (de) |
SG (1) | SG125088A1 (de) |
Families Citing this family (35)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7137776B2 (en) | 2002-06-19 | 2006-11-21 | United Technologies Corporation | Film cooling for microcircuits |
US7513744B2 (en) * | 2006-07-18 | 2009-04-07 | United Technologies Corporation | Microcircuit cooling and tip blowing |
US7581927B2 (en) * | 2006-07-28 | 2009-09-01 | United Technologies Corporation | Serpentine microcircuit cooling with pressure side features |
US7686582B2 (en) * | 2006-07-28 | 2010-03-30 | United Technologies Corporation | Radial split serpentine microcircuits |
US7717675B1 (en) | 2007-05-24 | 2010-05-18 | Florida Turbine Technologies, Inc. | Turbine airfoil with a near wall mini serpentine cooling circuit |
US8061979B1 (en) * | 2007-10-19 | 2011-11-22 | Florida Turbine Technologies, Inc. | Turbine BOAS with edge cooling |
US8157527B2 (en) * | 2008-07-03 | 2012-04-17 | United Technologies Corporation | Airfoil with tapered radial cooling passage |
US8572844B2 (en) * | 2008-08-29 | 2013-11-05 | United Technologies Corporation | Airfoil with leading edge cooling passage |
US8303252B2 (en) * | 2008-10-16 | 2012-11-06 | United Technologies Corporation | Airfoil with cooling passage providing variable heat transfer rate |
US8109725B2 (en) * | 2008-12-15 | 2012-02-07 | United Technologies Corporation | Airfoil with wrapped leading edge cooling passage |
US8167558B2 (en) * | 2009-01-19 | 2012-05-01 | Siemens Energy, Inc. | Modular serpentine cooling systems for turbine engine components |
US8556575B2 (en) * | 2010-03-26 | 2013-10-15 | United Technologies Corporation | Blade outer seal for a gas turbine engine |
US8449254B2 (en) * | 2010-03-29 | 2013-05-28 | United Technologies Corporation | Branched airfoil core cooling arrangement |
US8777570B1 (en) * | 2010-04-09 | 2014-07-15 | Florida Turbine Technologies, Inc. | Turbine vane with film cooling slots |
US8894363B2 (en) * | 2011-02-09 | 2014-11-25 | Siemens Energy, Inc. | Cooling module design and method for cooling components of a gas turbine system |
CA2800209A1 (en) * | 2010-05-23 | 2011-12-01 | Forced Physics Llc | Heat and energy exchange |
GB201016335D0 (en) * | 2010-09-29 | 2010-11-10 | Rolls Royce Plc | Endwall component for a turbine stage of a gas turbine engine |
CN102320549B (zh) * | 2011-07-28 | 2014-05-28 | 北京大学 | 一种提高薄膜应变线性度的方法 |
US9057523B2 (en) * | 2011-07-29 | 2015-06-16 | United Technologies Corporation | Microcircuit cooling for gas turbine engine combustor |
US8978385B2 (en) | 2011-07-29 | 2015-03-17 | United Technologies Corporation | Distributed cooling for gas turbine engine combustor |
US9243502B2 (en) | 2012-04-24 | 2016-01-26 | United Technologies Corporation | Airfoil cooling enhancement and method of making the same |
US9296039B2 (en) | 2012-04-24 | 2016-03-29 | United Technologies Corporation | Gas turbine engine airfoil impingement cooling |
WO2015042262A1 (en) * | 2013-09-18 | 2015-03-26 | United Technologies Corporation | Tortuous cooling passageway for engine component |
JP6239938B2 (ja) * | 2013-11-05 | 2017-11-29 | 三菱日立パワーシステムズ株式会社 | ガスタービン燃焼器 |
US20150198063A1 (en) | 2014-01-14 | 2015-07-16 | Alstom Technology Ltd | Cooled stator heat shield |
WO2015175042A2 (en) | 2014-02-14 | 2015-11-19 | United Technologies Corporation | Blade outer air seal fin cooling assembly and method |
US10280761B2 (en) * | 2014-10-29 | 2019-05-07 | United Technologies Corporation | Three dimensional airfoil micro-core cooling chamber |
CA2935398A1 (en) | 2015-07-31 | 2017-01-31 | Rolls-Royce Corporation | Turbine airfoils with micro cooling features |
US10871075B2 (en) | 2015-10-27 | 2020-12-22 | Pratt & Whitney Canada Corp. | Cooling passages in a turbine component |
US10533749B2 (en) | 2015-10-27 | 2020-01-14 | Pratt & Whitney Cananda Corp. | Effusion cooling holes |
US10415396B2 (en) | 2016-05-10 | 2019-09-17 | General Electric Company | Airfoil having cooling circuit |
US10731472B2 (en) | 2016-05-10 | 2020-08-04 | General Electric Company | Airfoil with cooling circuit |
US10358928B2 (en) | 2016-05-10 | 2019-07-23 | General Electric Company | Airfoil with cooling circuit |
US10544941B2 (en) * | 2016-12-07 | 2020-01-28 | General Electric Company | Fuel nozzle assembly with micro-channel cooling |
GB202000870D0 (en) * | 2020-01-21 | 2020-03-04 | Rolls Royce Plc | A combustion chamber, a combustion chamber tile and a combustion chamber segment |
Family Cites Families (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3672787A (en) | 1969-10-31 | 1972-06-27 | Avco Corp | Turbine blade having a cooled laminated skin |
US3957104A (en) * | 1974-02-27 | 1976-05-18 | The United States Of America As Represented By The Administrator Of The United States National Aeronautics And Space Administration | Method of making an apertured casting |
GB1530594A (en) | 1974-12-13 | 1978-11-01 | Rolls Royce | Perforate laminated material |
US4664597A (en) * | 1985-12-23 | 1987-05-12 | United Technologies Corporation | Coolant passages with full coverage film cooling slot |
US5383766A (en) | 1990-07-09 | 1995-01-24 | United Technologies Corporation | Cooled vane |
US5152667A (en) | 1991-07-16 | 1992-10-06 | General Motors Corporation | Cooled wall structure especially for gas turbine engines |
US5216886A (en) * | 1991-08-14 | 1993-06-08 | The United States Of America As Represented By The Secretary Of The Air Force | Segmented cell wall liner for a combustion chamber |
US5649806A (en) | 1993-11-22 | 1997-07-22 | United Technologies Corporation | Enhanced film cooling slot for turbine blade outer air seals |
GB9900102D0 (en) * | 1999-01-06 | 1999-02-24 | Rolls Royce Plc | A seal arrangement |
US6247896B1 (en) * | 1999-06-23 | 2001-06-19 | United Technologies Corporation | Method and apparatus for cooling an airfoil |
US6213714B1 (en) | 1999-06-29 | 2001-04-10 | Allison Advanced Development Company | Cooled airfoil |
US6402470B1 (en) * | 1999-10-05 | 2002-06-11 | United Technologies Corporation | Method and apparatus for cooling a wall within a gas turbine engine |
US6254334B1 (en) * | 1999-10-05 | 2001-07-03 | United Technologies Corporation | Method and apparatus for cooling a wall within a gas turbine engine |
US6280140B1 (en) * | 1999-11-18 | 2001-08-28 | United Technologies Corporation | Method and apparatus for cooling an airfoil |
DE10001109B4 (de) | 2000-01-13 | 2012-01-19 | Alstom Technology Ltd. | Gekühlte Schaufel für eine Gasturbine |
US7137776B2 (en) | 2002-06-19 | 2006-11-21 | United Technologies Corporation | Film cooling for microcircuits |
-
2002
- 2002-06-19 US US10/176,458 patent/US7137776B2/en not_active Expired - Lifetime
-
2003
- 2003-06-04 IL IL15630103A patent/IL156301A0/xx unknown
- 2003-06-05 AU AU2003204541A patent/AU2003204541B2/en not_active Ceased
- 2003-06-09 SG SG200303390A patent/SG125088A1/en unknown
- 2003-06-16 CA CA002432490A patent/CA2432490A1/en not_active Abandoned
- 2003-06-19 JP JP2003175179A patent/JP2004044588A/ja active Pending
- 2003-06-19 AT AT03253895T patent/ATE327415T1/de not_active IP Right Cessation
- 2003-06-19 KR KR1020030039952A patent/KR100705116B1/ko not_active IP Right Cessation
- 2003-06-19 EP EP03253895A patent/EP1377140B1/de not_active Expired - Lifetime
- 2003-06-19 DK DK03253895T patent/DK1377140T3/da active
- 2003-06-19 DE DE60305385T patent/DE60305385T2/de not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
KR100705116B1 (ko) | 2007-04-06 |
AU2003204541B2 (en) | 2005-07-07 |
DE60305385T2 (de) | 2007-03-29 |
AU2003204541A1 (en) | 2004-01-22 |
DE60305385D1 (de) | 2006-06-29 |
IL156301A0 (en) | 2004-01-04 |
US7137776B2 (en) | 2006-11-21 |
EP1377140A2 (de) | 2004-01-02 |
KR20030097708A (ko) | 2003-12-31 |
EP1377140A3 (de) | 2004-09-08 |
DK1377140T3 (da) | 2006-08-21 |
SG125088A1 (en) | 2006-09-29 |
EP1377140B1 (de) | 2006-05-24 |
CA2432490A1 (en) | 2003-12-19 |
US20060210390A1 (en) | 2006-09-21 |
JP2004044588A (ja) | 2004-02-12 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
UEP | Publication of translation of european patent specification |
Ref document number: 1377140 Country of ref document: EP |
|
REN | Ceased due to non-payment of the annual fee |