SG10201608480QA - Turbine blade - Google Patents
Turbine bladeInfo
- Publication number
- SG10201608480QA SG10201608480QA SG10201608480QA SG10201608480QA SG10201608480QA SG 10201608480Q A SG10201608480Q A SG 10201608480QA SG 10201608480Q A SG10201608480Q A SG 10201608480QA SG 10201608480Q A SG10201608480Q A SG 10201608480QA SG 10201608480Q A SG10201608480Q A SG 10201608480QA
- Authority
- SG
- Singapore
- Prior art keywords
- turbine blade
- turbine
- blade
- 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
- F01D5/187—Convection 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
- 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
- F01D5/186—Film 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
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/32—Application in turbines in gas turbines
- F05D2220/323—Application in turbines in gas turbines for aircraft propulsion, e.g. jet engines
-
- 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
- F05D2240/00—Components
- F05D2240/20—Rotors
- F05D2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
- F05D2240/303—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor related to the leading edge of a rotor blade
-
- 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
- F05D2250/70—Shape
- F05D2250/71—Shape curved
-
- 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
- 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
-
- 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
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US14/884,088 US20170107827A1 (en) | 2015-10-15 | 2015-10-15 | Turbine blade |
Publications (1)
Publication Number | Publication Date |
---|---|
SG10201608480QA true SG10201608480QA (en) | 2017-05-30 |
Family
ID=57130290
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SG10201608480QA SG10201608480QA (en) | 2015-10-15 | 2016-10-10 | Turbine blade |
Country Status (7)
Country | Link |
---|---|
US (1) | US20170107827A1 (en) |
EP (1) | EP3165715A1 (en) |
JP (1) | JP2017078414A (en) |
CN (1) | CN106801622A (en) |
BR (1) | BR102016022302A2 (en) |
CA (1) | CA2944464A1 (en) |
SG (1) | SG10201608480QA (en) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10174620B2 (en) | 2015-10-15 | 2019-01-08 | General Electric Company | Turbine blade |
US10208605B2 (en) | 2015-10-15 | 2019-02-19 | General Electric Company | Turbine blade |
US10364681B2 (en) | 2015-10-15 | 2019-07-30 | General Electric Company | Turbine blade |
US11047240B2 (en) * | 2017-05-11 | 2021-06-29 | General Electric Company | CMC components having microchannels and methods for forming microchannels in CMC components |
KR102028803B1 (en) * | 2017-09-29 | 2019-10-04 | 두산중공업 주식회사 | Gas Turbine |
US10975704B2 (en) * | 2018-02-19 | 2021-04-13 | General Electric Company | Engine component with cooling hole |
US10787932B2 (en) * | 2018-07-13 | 2020-09-29 | Honeywell International Inc. | Turbine blade with dust tolerant cooling system |
US10837293B2 (en) * | 2018-07-19 | 2020-11-17 | General Electric Company | Airfoil with tunable cooling configuration |
US11174736B2 (en) * | 2018-12-18 | 2021-11-16 | General Electric Company | Method of forming an additively manufactured component |
KR102161765B1 (en) | 2019-02-22 | 2020-10-05 | 두산중공업 주식회사 | Airfoil for turbine, turbine including the same |
GB202214883D0 (en) * | 2022-10-10 | 2022-11-23 | Rolls Royce Plc | Aerofoil for a gas turbine engine |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6099251A (en) * | 1998-07-06 | 2000-08-08 | United Technologies Corporation | Coolable airfoil for a gas turbine engine |
US6602047B1 (en) * | 2002-02-28 | 2003-08-05 | General Electric Company | Methods and apparatus for cooling gas turbine nozzles |
GB2395232B (en) * | 2002-11-12 | 2006-01-25 | Rolls Royce Plc | Turbine components |
US6932573B2 (en) * | 2003-04-30 | 2005-08-23 | Siemens Westinghouse Power Corporation | Turbine blade having a vortex forming cooling system for a trailing edge |
US6923623B2 (en) * | 2003-08-07 | 2005-08-02 | General Electric Company | Perimeter-cooled turbine bucket airfoil cooling hole location, style and configuration |
US7625179B2 (en) * | 2006-09-13 | 2009-12-01 | United Technologies Corporation | Airfoil thermal management with microcircuit cooling |
EP1921268A1 (en) * | 2006-11-08 | 2008-05-14 | Siemens Aktiengesellschaft | Turbine blade |
US8757974B2 (en) * | 2007-01-11 | 2014-06-24 | United Technologies Corporation | Cooling circuit flow path for a turbine section airfoil |
FR2918105B1 (en) * | 2007-06-27 | 2013-12-27 | Snecma | TURBOMACHINE COOLED AUBE COMPRISING VARIABLE IMPACT REMOTE COOLING HOLES. |
GB0811391D0 (en) * | 2008-06-23 | 2008-07-30 | Rolls Royce Plc | A rotor blade |
GB0909255D0 (en) * | 2009-06-01 | 2009-07-15 | Rolls Royce Plc | Cooling arrangements |
US8292582B1 (en) * | 2009-07-09 | 2012-10-23 | Florida Turbine Technologies, Inc. | Turbine blade with serpentine flow cooling |
EP2828484B1 (en) * | 2012-03-22 | 2019-05-08 | Ansaldo Energia IP UK Limited | Turbine blade |
US9296039B2 (en) * | 2012-04-24 | 2016-03-29 | United Technologies Corporation | Gas turbine engine airfoil impingement cooling |
-
2015
- 2015-10-15 US US14/884,088 patent/US20170107827A1/en not_active Abandoned
-
2016
- 2016-09-27 BR BR102016022302A patent/BR102016022302A2/en not_active Application Discontinuation
- 2016-10-05 JP JP2016196839A patent/JP2017078414A/en active Pending
- 2016-10-06 CA CA2944464A patent/CA2944464A1/en not_active Abandoned
- 2016-10-10 SG SG10201608480QA patent/SG10201608480QA/en unknown
- 2016-10-12 EP EP16193543.2A patent/EP3165715A1/en not_active Withdrawn
- 2016-10-14 CN CN201610896213.6A patent/CN106801622A/en active Pending
Also Published As
Publication number | Publication date |
---|---|
US20170107827A1 (en) | 2017-04-20 |
JP2017078414A (en) | 2017-04-27 |
EP3165715A1 (en) | 2017-05-10 |
BR102016022302A2 (en) | 2017-04-25 |
CA2944464A1 (en) | 2017-04-15 |
CN106801622A (en) | 2017-06-06 |
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