SG10201603741QA - Core assembly for gas turbine engine - Google Patents
Core assembly for gas turbine engineInfo
- Publication number
- SG10201603741QA SG10201603741QA SG10201603741QA SG10201603741QA SG10201603741QA SG 10201603741Q A SG10201603741Q A SG 10201603741QA SG 10201603741Q A SG10201603741Q A SG 10201603741QA SG 10201603741Q A SG10201603741Q A SG 10201603741QA SG 10201603741Q A SG10201603741Q A SG 10201603741QA
- Authority
- SG
- Singapore
- Prior art keywords
- gas turbine
- turbine engine
- core assembly
- core
- assembly
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C9/00—Moulds or cores; Moulding processes
- B22C9/10—Cores; Manufacture or installation of cores
- B22C9/103—Multipart cores
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/12—Cooling of plants
-
- 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
-
- 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
- F01D5/147—Construction, i.e. structural features, e.g. of weight-saving hollow blades
-
- 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
- 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
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
- F01D5/284—Selection of ceramic materials
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
-
- 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
- F05D2230/00—Manufacture
- F05D2230/20—Manufacture essentially without removing material
- F05D2230/21—Manufacture essentially without removing material by casting
-
- 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 |
---|---|---|---|
US14/749,000 US10801407B2 (en) | 2015-06-24 | 2015-06-24 | Core assembly for gas turbine engine |
Publications (1)
Publication Number | Publication Date |
---|---|
SG10201603741QA true SG10201603741QA (en) | 2017-01-27 |
Family
ID=56203269
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SG10201603741QA SG10201603741QA (en) | 2015-06-24 | 2016-05-11 | Core assembly for gas turbine engine |
Country Status (3)
Country | Link |
---|---|
US (1) | US10801407B2 (en) |
EP (1) | EP3108981B1 (en) |
SG (1) | SG10201603741QA (en) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US11098595B2 (en) | 2017-05-02 | 2021-08-24 | Raytheon Technologies Corporation | Airfoil for gas turbine engine |
US10422232B2 (en) | 2017-05-22 | 2019-09-24 | United Technologies Corporation | Component for a gas turbine engine |
US10443406B2 (en) * | 2018-01-31 | 2019-10-15 | United Technologies Corporation | Airfoil having non-leading edge stagnation line cooling scheme |
US11440146B1 (en) * | 2021-04-22 | 2022-09-13 | Raytheon Technologies Corporation | Mini-core surface bonding |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6186217B1 (en) | 1998-12-01 | 2001-02-13 | Howmet Research Corporation | Multipiece core assembly |
US6929054B2 (en) | 2003-12-19 | 2005-08-16 | United Technologies Corporation | Investment casting cores |
US7744347B2 (en) | 2005-11-08 | 2010-06-29 | United Technologies Corporation | Peripheral microcircuit serpentine cooling for turbine airfoils |
US7364405B2 (en) | 2005-11-23 | 2008-04-29 | United Technologies Corporation | Microcircuit cooling for vanes |
US7731481B2 (en) | 2006-12-18 | 2010-06-08 | United Technologies Corporation | Airfoil cooling with staggered refractory metal core microcircuits |
US8157527B2 (en) | 2008-07-03 | 2012-04-17 | United Technologies Corporation | Airfoil with tapered radial 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 |
US8813812B2 (en) | 2010-02-25 | 2014-08-26 | Siemens Energy, Inc. | Turbine component casting core with high resolution region |
US8915289B2 (en) | 2011-05-10 | 2014-12-23 | Howmet Corporation | Ceramic core with composite insert for casting airfoils |
US8291963B1 (en) | 2011-08-03 | 2012-10-23 | United Technologies Corporation | Hybrid core assembly |
US9486854B2 (en) | 2012-09-10 | 2016-11-08 | United Technologies Corporation | Ceramic and refractory metal core assembly |
US20140102656A1 (en) | 2012-10-12 | 2014-04-17 | United Technologies Corporation | Casting Cores and Manufacture Methods |
US10166599B2 (en) | 2013-11-18 | 2019-01-01 | United Technologies Corporation | Coated casting cores and manufacture methods |
-
2015
- 2015-06-24 US US14/749,000 patent/US10801407B2/en active Active
-
2016
- 2016-05-11 SG SG10201603741QA patent/SG10201603741QA/en unknown
- 2016-06-24 EP EP16176117.6A patent/EP3108981B1/en active Active
Also Published As
Publication number | Publication date |
---|---|
US20160376989A1 (en) | 2016-12-29 |
EP3108981B1 (en) | 2019-05-15 |
US10801407B2 (en) | 2020-10-13 |
EP3108981A1 (en) | 2016-12-28 |
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