HK1196331A1 - 尤其用於渦輪機翼的鑲鑄冷卻特徵 - Google Patents
尤其用於渦輪機翼的鑲鑄冷卻特徵Info
- Publication number
- HK1196331A1 HK1196331A1 HK14109833.6A HK14109833A HK1196331A1 HK 1196331 A1 HK1196331 A1 HK 1196331A1 HK 14109833 A HK14109833 A HK 14109833A HK 1196331 A1 HK1196331 A1 HK 1196331A1
- Authority
- HK
- Hong Kong
- Prior art keywords
- cast
- cooling features
- turbine airfoils
- features especially
- airfoils
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C7/00—Patterns; Manufacture thereof so far as not provided for in other classes
- B22C7/02—Lost patterns
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C21/00—Flasks; Accessories therefor
- B22C21/12—Accessories
- B22C21/14—Accessories for reinforcing or securing moulding materials or cores, e.g. gaggers, chaplets, pins, bars
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C9/00—Moulds or cores; Moulding processes
- B22C9/02—Sand moulds or like moulds for shaped castings
- B22C9/04—Use of lost patterns
-
- 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
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Molds, Cores, And Manufacturing Methods Thereof (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13/815,595 US9835035B2 (en) | 2013-03-12 | 2013-03-12 | Cast-in cooling features especially for turbine airfoils |
Publications (1)
Publication Number | Publication Date |
---|---|
HK1196331A1 true HK1196331A1 (zh) | 2014-12-12 |
Family
ID=50241177
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
HK14109833.6A HK1196331A1 (zh) | 2013-03-12 | 2014-09-30 | 尤其用於渦輪機翼的鑲鑄冷卻特徵 |
Country Status (5)
Country | Link |
---|---|
US (1) | US9835035B2 (zh) |
EP (1) | EP2777842B1 (zh) |
JP (1) | JP6315553B2 (zh) |
ES (1) | ES2564407T3 (zh) |
HK (1) | HK1196331A1 (zh) |
Families Citing this family (34)
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EP2735387A1 (de) * | 2012-11-22 | 2014-05-28 | Siemens Aktiengesellschaft | Gussform mit angeschrägten Stirnseiten bei inneren Wänden |
EP3086893B1 (en) | 2013-12-23 | 2019-07-24 | United Technologies Corporation | Lost core structural frame |
US20150202702A1 (en) * | 2014-01-17 | 2015-07-23 | United Technologies Corporation | Gas turbine engine cast structure method for finishing |
CN106030039A (zh) * | 2014-02-25 | 2016-10-12 | 西门子公司 | 具有深度变化材料性质的涡轮机部件热障涂层 |
US9970319B2 (en) * | 2014-05-05 | 2018-05-15 | United Technologies Corporation | Reducing variation in cooling hole meter length |
EP3157694B1 (en) * | 2014-06-18 | 2020-07-29 | Mikro Systems Inc. | Turbine blade investment casting using film hole protrusions for integral wall thickness control |
EP2990605A1 (de) | 2014-08-26 | 2016-03-02 | Siemens Aktiengesellschaft | Turbinenschaufel |
US9963975B2 (en) | 2015-02-09 | 2018-05-08 | United Technologies Corporation | Trip strip restagger |
EP3259452A2 (en) | 2015-02-18 | 2017-12-27 | Siemens Aktiengesellschaft | Forming cooling passages in combustion turbine superalloy castings |
US10323524B2 (en) | 2015-05-08 | 2019-06-18 | United Technologies Corporation | Axial skin core cooling passage for a turbine engine component |
US10502066B2 (en) | 2015-05-08 | 2019-12-10 | United Technologies Corporation | Turbine engine component including an axially aligned skin core passage interrupted by a pedestal |
US10830052B2 (en) | 2016-09-15 | 2020-11-10 | Honeywell International Inc. | Gas turbine component with cooling aperture having shaped inlet and method of forming the same |
US20180161854A1 (en) | 2016-12-13 | 2018-06-14 | General Electric Company | Integrated casting core-shell structure |
US11813669B2 (en) | 2016-12-13 | 2023-11-14 | General Electric Company | Method for making an integrated core-shell structure |
US20180161852A1 (en) * | 2016-12-13 | 2018-06-14 | General Electric Company | Integrated casting core-shell structure with printed tubes for making cast component |
US10807154B2 (en) * | 2016-12-13 | 2020-10-20 | General Electric Company | Integrated casting core-shell structure for making cast component with cooling holes in inaccessible locations |
US20180161855A1 (en) * | 2016-12-13 | 2018-06-14 | General Electric Company | Multi-piece integrated core-shell structure with standoff and/or bumper for making cast component |
US20180161856A1 (en) * | 2016-12-13 | 2018-06-14 | General Electric Company | Integrated casting core-shell structure and filter for making cast component |
US20180161866A1 (en) | 2016-12-13 | 2018-06-14 | General Electric Company | Multi-piece integrated core-shell structure for making cast component |
US20180161859A1 (en) * | 2016-12-13 | 2018-06-14 | General Electric Company | Integrated casting core-shell structure for making cast component with non-linear holes |
US10934854B2 (en) | 2018-09-11 | 2021-03-02 | General Electric Company | CMC component cooling cavities |
US11040915B2 (en) | 2018-09-11 | 2021-06-22 | General Electric Company | Method of forming CMC component cooling cavities |
US10913106B2 (en) | 2018-09-14 | 2021-02-09 | Raytheon Technologies Corporation | Cast-in film cooling hole structures |
CN117858789A (zh) * | 2021-07-12 | 2024-04-09 | 想像航空有限公司 | 例如适用于机身和其他结构的制造方法和相关结构 |
US11603769B2 (en) | 2021-08-13 | 2023-03-14 | Raytheon Technologies Corporation | Forming lined cooling aperture(s) in a turbine engine component |
US11732590B2 (en) | 2021-08-13 | 2023-08-22 | Raytheon Technologies Corporation | Transition section for accommodating mismatch between other sections of a cooling aperture in a turbine engine component |
US12123839B2 (en) | 2021-08-13 | 2024-10-22 | Rtx Corporation | Forming and/or inspecting cooling aperture(s) in a turbine engine component |
US11542831B1 (en) | 2021-08-13 | 2023-01-03 | Raytheon Technologies Corporation | Energy beam positioning during formation of a cooling aperture |
US11673200B2 (en) | 2021-08-13 | 2023-06-13 | Raytheon Technologies Corporation | Forming cooling aperture(s) using electrical discharge machining |
US11913119B2 (en) | 2021-08-13 | 2024-02-27 | Rtx Corporation | Forming cooling aperture(s) in a turbine engine component |
US11898465B2 (en) | 2021-08-13 | 2024-02-13 | Rtx Corporation | Forming lined cooling aperture(s) in a turbine engine component |
US11813706B2 (en) | 2021-08-13 | 2023-11-14 | Rtx Corporation | Methods for forming cooling apertures in a turbine engine component |
US11998974B2 (en) * | 2022-08-30 | 2024-06-04 | General Electric Company | Casting core for a cast engine component |
US20240218828A1 (en) | 2022-11-01 | 2024-07-04 | General Electric Company | Gas Turbine Engine |
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-
2013
- 2013-03-12 US US13/815,595 patent/US9835035B2/en active Active
-
2014
- 2014-01-29 JP JP2014013974A patent/JP6315553B2/ja active Active
- 2014-03-10 EP EP14158655.2A patent/EP2777842B1/en active Active
- 2014-03-10 ES ES14158655.2T patent/ES2564407T3/es active Active
- 2014-09-30 HK HK14109833.6A patent/HK1196331A1/zh unknown
Also Published As
Publication number | Publication date |
---|---|
EP2777842B1 (en) | 2016-01-20 |
ES2564407T3 (es) | 2016-03-22 |
US9835035B2 (en) | 2017-12-05 |
JP6315553B2 (ja) | 2018-04-25 |
JP2014208373A (ja) | 2014-11-06 |
US20140271129A1 (en) | 2014-09-18 |
EP2777842A1 (en) | 2014-09-17 |
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