EP0207799A3 - Kühlkanäle für die Schaufeln einer Gasturbine - Google Patents
Kühlkanäle für die Schaufeln einer Gasturbine Download PDFInfo
- Publication number
- EP0207799A3 EP0207799A3 EP86305182A EP86305182A EP0207799A3 EP 0207799 A3 EP0207799 A3 EP 0207799A3 EP 86305182 A EP86305182 A EP 86305182A EP 86305182 A EP86305182 A EP 86305182A EP 0207799 A3 EP0207799 A3 EP 0207799A3
- Authority
- EP
- European Patent Office
- Prior art keywords
- combustion turbine
- rotor blades
- coolant passage
- passage structure
- improved coolant
- 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.)
- Withdrawn
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
- 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
- F05D2250/20—Three-dimensional
- F05D2250/23—Three-dimensional prismatic
- F05D2250/231—Three-dimensional prismatic cylindrical
-
- 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
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 |
---|---|---|---|
US75165785A | 1985-07-03 | 1985-07-03 | |
US751657 | 1985-07-03 |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0207799A2 EP0207799A2 (de) | 1987-01-07 |
EP0207799A3 true EP0207799A3 (de) | 1988-09-14 |
Family
ID=25022941
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP86305182A Withdrawn EP0207799A3 (de) | 1985-07-03 | 1986-07-03 | Kühlkanäle für die Schaufeln einer Gasturbine |
Country Status (5)
Country | Link |
---|---|
EP (1) | EP0207799A3 (de) |
JP (1) | JPS6210402A (de) |
CN (1) | CN86104500A (de) |
CA (1) | CA1262868A (de) |
IE (1) | IE861475L (de) |
Families Citing this family (33)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4893987A (en) * | 1987-12-08 | 1990-01-16 | General Electric Company | Diffusion-cooled blade tip cap |
US5413463A (en) * | 1991-12-30 | 1995-05-09 | General Electric Company | Turbulated cooling passages in gas turbine buckets |
DE4430302A1 (de) * | 1994-08-26 | 1996-02-29 | Abb Management Ag | Prallgekühltes Wandteil |
US6539627B2 (en) | 2000-01-19 | 2003-04-01 | General Electric Company | Method of making turbulated cooling holes |
US6994514B2 (en) * | 2002-11-20 | 2006-02-07 | Mitsubishi Heavy Industries, Ltd. | Turbine blade and gas turbine |
GB0229908D0 (en) * | 2002-12-21 | 2003-01-29 | Macdonald John | Turbine blade |
US6997679B2 (en) * | 2003-12-12 | 2006-02-14 | General Electric Company | Airfoil cooling holes |
CN1318735C (zh) * | 2005-12-26 | 2007-05-30 | 北京航空航天大学 | 一种适用于燃气涡轮发动机的脉动冲击冷却叶片 |
US7413406B2 (en) | 2006-02-15 | 2008-08-19 | United Technologies Corporation | Turbine blade with radial cooling channels |
US8511992B2 (en) * | 2008-01-22 | 2013-08-20 | United Technologies Corporation | Minimization of fouling and fluid losses in turbine airfoils |
US8157527B2 (en) * | 2008-07-03 | 2012-04-17 | United Technologies Corporation | Airfoil with tapered radial cooling passage |
JP2010053749A (ja) * | 2008-08-27 | 2010-03-11 | Mitsubishi Heavy Ind Ltd | タービン用翼 |
US8201621B2 (en) * | 2008-12-08 | 2012-06-19 | General Electric Company | Heat exchanging hollow passages with helicoidal grooves |
US8511990B2 (en) * | 2009-06-24 | 2013-08-20 | General Electric Company | Cooling hole exits for a turbine bucket tip shroud |
EP2354453B1 (de) * | 2010-02-02 | 2018-03-28 | Siemens Aktiengesellschaft | Turbinenmotorkomponente zur adaptiven Kühlung |
WO2011108164A1 (ja) * | 2010-03-03 | 2011-09-09 | 三菱重工業株式会社 | ガスタービンの動翼およびその製造方法ならびに動翼を用いたガスタービン |
US8506251B2 (en) | 2010-03-03 | 2013-08-13 | Mitsubishi Heavy Industries, Ltd. | Gas turbine blade, manufacturing method therefor, and gas turbine using turbine blade |
US8727724B2 (en) * | 2010-04-12 | 2014-05-20 | General Electric Company | Turbine bucket having a radial cooling hole |
US9181819B2 (en) * | 2010-06-11 | 2015-11-10 | Siemens Energy, Inc. | Component wall having diffusion sections for cooling in a turbine engine |
JP2012145098A (ja) * | 2010-12-21 | 2012-08-02 | Toshiba Corp | トランジションピースおよびガスタービン |
US20130052035A1 (en) * | 2011-08-24 | 2013-02-28 | General Electric Company | Axially cooled airfoil |
WO2014026287A1 (en) | 2012-08-14 | 2014-02-20 | Powerdisc Development Corporation Ltd. | Fuel cell components, stacks and modular fuel cell systems |
US9644277B2 (en) | 2012-08-14 | 2017-05-09 | Loop Energy Inc. | Reactant flow channels for electrolyzer applications |
CA2919875C (en) | 2012-08-14 | 2021-08-17 | Powerdisc Development Corporation Ltd. | Fuel cell flow channels and flow fields |
US20140161625A1 (en) * | 2012-12-11 | 2014-06-12 | General Electric Company | Turbine component having cooling passages with varying diameter |
WO2016133982A1 (en) | 2015-02-18 | 2016-08-25 | Siemens Aktiengesellschaft | Forming cooling passages in thermal barrier coated, combustion turbine superalloy components |
WO2017121689A1 (en) | 2016-01-15 | 2017-07-20 | Siemens Aktiengesellschaft | Gas turbine aerofoil |
EP3433894B1 (de) | 2016-03-22 | 2024-05-08 | Loop Energy Inc. | Brennstoffzellenströmungsfelddesign für thermomanagement |
US10577943B2 (en) * | 2017-05-11 | 2020-03-03 | General Electric Company | Turbine engine airfoil insert |
JP7234006B2 (ja) | 2019-03-29 | 2023-03-07 | 三菱重工業株式会社 | 高温部品及び高温部品の製造方法 |
CN110159357B (zh) * | 2019-06-04 | 2021-01-29 | 北京航空航天大学 | 一种提升被动安全的航空发动机涡轮叶片缩扩型供气通道 |
US11905848B2 (en) * | 2019-06-05 | 2024-02-20 | Mitsubishi Heavy Industries, Ltd. | Turbine blade, manufacturing method for turbine blade, and gas turbine |
JP6637630B1 (ja) * | 2019-06-05 | 2020-01-29 | 三菱日立パワーシステムズ株式会社 | タービン翼およびタービン翼の製造方法並びにガスタービン |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3301528A (en) * | 1964-11-13 | 1967-01-31 | Rolls Royce | Aerofoil shaped blade for fluid flow machines |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS4825103B1 (de) * | 1967-06-05 | 1973-07-26 | ||
JPS5520041A (en) * | 1978-07-29 | 1980-02-13 | Noto Denshi Kogyo Kk | Piezoelectric device |
JPS5669423A (en) * | 1979-11-09 | 1981-06-10 | Hitachi Ltd | Air-cooled blade of gas turbine |
-
1986
- 1986-06-04 IE IE147586A patent/IE861475L/xx unknown
- 1986-06-25 CA CA000512386A patent/CA1262868A/en not_active Expired
- 1986-06-30 JP JP15185286A patent/JPS6210402A/ja active Pending
- 1986-07-01 CN CN 86104500 patent/CN86104500A/zh active Pending
- 1986-07-03 EP EP86305182A patent/EP0207799A3/de not_active Withdrawn
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3301528A (en) * | 1964-11-13 | 1967-01-31 | Rolls Royce | Aerofoil shaped blade for fluid flow machines |
Also Published As
Publication number | Publication date |
---|---|
CN86104500A (zh) | 1987-02-04 |
CA1262868A (en) | 1989-11-14 |
EP0207799A2 (de) | 1987-01-07 |
JPS6210402A (ja) | 1987-01-19 |
IE861475L (en) | 1987-01-03 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP0207799A3 (de) | Kühlkanäle für die Schaufeln einer Gasturbine | |
JP4800689B2 (ja) | スカート付きタービンブレード | |
US6976826B2 (en) | Turbine blade dimple | |
US20050232769A1 (en) | Thermal shield turbine airfoil | |
FR2181407A5 (de) | ||
SE8305993L (sv) | Motroterande kraftturbin | |
EP0353498A3 (de) | Diaphragmaaufbau eines Verdichters | |
IE842485L (en) | Stator vane cooling | |
CA2254230A1 (en) | Gas turbine rotor blade | |
GB1514613A (en) | Blade or vane for a gas turbine engine | |
CA2130628A1 (en) | Steam turbine blade | |
GB1284538A (en) | Blade for a fluid flow machine | |
SE8601928L (sv) | Gasturbinmotorer | |
KR840007130A (ko) | 터어빈 회전날개 및 그의 조립방법 | |
KR880014231A (ko) | 터어빈 블레이드의 장착방법 | |
US6336791B1 (en) | Device and method employing a turbine for contributing thrust to a propeller on a spinner | |
JP2004028097A (ja) | タービンブレード壁の冷却装置及び製造方法 | |
GB666536A (en) | Stator blades for a gas turbine | |
GB1513338A (en) | Rotor blade for a gas turbine engine | |
EP0971096A3 (de) | Befestigung eines Schaufelblattes an einem Rotor | |
EP0080258A3 (de) | Radialturbinenläufer | |
GB1294593A (en) | Improvements in radial flow turbines | |
EP0194883A2 (de) | Gasturbinenschaufel mit in Richtung der Schaufellänge angeordneten Kühlkanälen | |
GB2095764A (en) | Turbine arrangement | |
RU94045348A (ru) | Охлаждаемая сопловая лопатка с вихревой матрицей |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
AK | Designated contracting states |
Kind code of ref document: A2 Designated state(s): DE FR GB IT NL |
|
PUAL | Search report despatched |
Free format text: ORIGINAL CODE: 0009013 |
|
AK | Designated contracting states |
Kind code of ref document: A3 Designated state(s): DE FR GB IT NL |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN |
|
18D | Application deemed to be withdrawn |
Effective date: 19890315 |
|
RIN1 | Information on inventor provided before grant (corrected) |
Inventor name: HOLDEN, PAUL CLARENCE |