CN114867930B - 通过增材制造的带有翼部密封件且在相邻轮空间部分之间具有冷却剂传送通道的涡轮转子叶片 - Google Patents
通过增材制造的带有翼部密封件且在相邻轮空间部分之间具有冷却剂传送通道的涡轮转子叶片Info
- Publication number
- CN114867930B CN114867930B CN202180007604.7A CN202180007604A CN114867930B CN 114867930 B CN114867930 B CN 114867930B CN 202180007604 A CN202180007604 A CN 202180007604A CN 114867930 B CN114867930 B CN 114867930B
- Authority
- CN
- China
- Prior art keywords
- turbine rotor
- shank
- rotor blade
- angel
- extending laterally
- 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.)
- Active
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
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/02—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
-
- 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
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/08—Heating, heat-insulating or cooling means
- F01D5/081—Cooling fluid being directed on the side of the rotor disc or at the roots of the 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
- F01D5/147—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
- F01D5/14—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
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
- F01D5/3007—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B33—ADDITIVE MANUFACTURING TECHNOLOGY
- B33Y—ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
- B33Y80/00—Products made by additive manufacturing
-
- 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
- F05D2230/22—Manufacture essentially without removing material by sintering
-
- 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
- F05D2230/30—Manufacture with deposition of material
- F05D2230/31—Layer deposition
-
- 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
-
- 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
- F05D2240/80—Platforms for stationary or moving blades
- F05D2240/81—Cooled platforms
-
- 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
- F05D2260/60—Fluid 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Architecture (AREA)
- Chemical & Material Sciences (AREA)
- Manufacturing & Machinery (AREA)
- Materials Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US16/749,167 US11248471B2 (en) | 2020-01-22 | 2020-01-22 | Turbine rotor blade with angel wing with coolant transfer passage between adjacent wheel space portions by additive manufacture |
| US16/749,167 | 2020-01-22 | ||
| PCT/US2021/013387 WO2021150418A1 (en) | 2020-01-22 | 2021-01-14 | Turbine rotor blade with angel wing seals with coolant transfer passage between adjacent wheel space portions by additive manufacture |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN114867930A CN114867930A (zh) | 2022-08-05 |
| CN114867930B true CN114867930B (zh) | 2026-01-06 |
Family
ID=74562067
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202180007604.7A Active CN114867930B (zh) | 2020-01-22 | 2021-01-14 | 通过增材制造的带有翼部密封件且在相邻轮空间部分之间具有冷却剂传送通道的涡轮转子叶片 |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US11248471B2 (https=) |
| EP (1) | EP4093944B1 (https=) |
| JP (1) | JP7646670B2 (https=) |
| KR (1) | KR102889298B1 (https=) |
| CN (1) | CN114867930B (https=) |
| WO (1) | WO2021150418A1 (https=) |
Families Citing this family (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US11242760B2 (en) * | 2020-01-22 | 2022-02-08 | General Electric Company | Turbine rotor blade with integral impingement sleeve by additive manufacture |
| US11492908B2 (en) | 2020-01-22 | 2022-11-08 | General Electric Company | Turbine rotor blade root with hollow mount with lattice support structure by additive manufacture |
| US11248471B2 (en) | 2020-01-22 | 2022-02-15 | General Electric Company | Turbine rotor blade with angel wing with coolant transfer passage between adjacent wheel space portions by additive manufacture |
| US11552523B2 (en) * | 2020-05-28 | 2023-01-10 | Honeywell International Inc. | Conformal cooling devices for rotating generator elements and additive manufacturing processes for fabricating the same |
| KR102621756B1 (ko) * | 2020-11-27 | 2024-01-09 | 연세대학교 산학협력단 | 격자구조의 냉각방식을 갖는 가스터빈 베인 및 블레이드 |
| US20250188843A1 (en) * | 2022-08-24 | 2025-06-12 | General Electric Company | Turbine engine airfoil |
| US12571351B2 (en) | 2023-06-14 | 2026-03-10 | General Electric Company | Gas turbine engine defining a rotor cavity |
| US20250369359A1 (en) * | 2024-05-29 | 2025-12-04 | Rtx Corporation | Cooling features for a component of a gas turbine engine |
| US12497897B1 (en) * | 2024-09-03 | 2025-12-16 | Ge Infrastructure Technology Llc | Airfoil component for turbomachine component with platform cooling using airfoil coolant |
Family Cites Families (39)
| Publication number | Priority date | Publication date | Assignee | Title |
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| US3628885A (en) * | 1969-10-01 | 1971-12-21 | Gen Electric | Fluid-cooled airfoil |
| US3867068A (en) | 1973-03-30 | 1975-02-18 | Gen Electric | Turbomachinery blade cooling insert retainers |
| US4203706A (en) | 1977-12-28 | 1980-05-20 | United Technologies Corporation | Radial wafer airfoil construction |
| US5816777A (en) | 1991-11-29 | 1998-10-06 | United Technologies Corporation | Turbine blade cooling |
| JPH0953406A (ja) | 1995-08-14 | 1997-02-25 | Mitsubishi Heavy Ind Ltd | インピンジメント冷却装置及びガスタービン翼 |
| US5800124A (en) | 1996-04-12 | 1998-09-01 | United Technologies Corporation | Cooled rotor assembly for a turbine engine |
| DE19634237A1 (de) | 1996-08-23 | 1998-02-26 | Asea Brown Boveri | Kühlbare Schaufel |
| EP0905353B1 (de) | 1997-09-30 | 2003-01-15 | ALSTOM (Switzerland) Ltd | Prallanordnung für ein konvektives Kühl- oder Heizverfahren |
| US6435813B1 (en) | 2000-05-10 | 2002-08-20 | General Electric Company | Impigement cooled airfoil |
| US6402471B1 (en) | 2000-11-03 | 2002-06-11 | General Electric Company | Turbine blade for gas turbine engine and method of cooling same |
| GB0515868D0 (en) | 2005-08-02 | 2005-09-07 | Rolls Royce Plc | Cooling arrangement |
| US7563072B1 (en) | 2006-09-25 | 2009-07-21 | Florida Turbine Technologies, Inc. | Turbine airfoil with near-wall spiral flow cooling circuit |
| US7837441B2 (en) | 2007-02-16 | 2010-11-23 | United Technologies Corporation | Impingement skin core cooling for gas turbine engine blade |
| US7785071B1 (en) | 2007-05-31 | 2010-08-31 | Florida Turbine Technologies, Inc. | Turbine airfoil with spiral trailing edge cooling passages |
| US8057183B1 (en) | 2008-12-16 | 2011-11-15 | Florida Turbine Technologies, Inc. | Light weight and highly cooled turbine blade |
| EP2256297B8 (en) | 2009-05-19 | 2012-10-03 | Alstom Technology Ltd | Gas turbine vane with improved cooling |
| US8523527B2 (en) | 2010-03-10 | 2013-09-03 | General Electric Company | Apparatus for cooling a platform of a turbine component |
| US8366394B1 (en) * | 2010-10-21 | 2013-02-05 | Florida Turbine Technologies, Inc. | Turbine blade with tip rail cooling channel |
| US20130104567A1 (en) | 2011-10-31 | 2013-05-02 | Douglas Gerard Konitzer | Method and apparatus for cooling gas turbine rotor blades |
| US8905714B2 (en) | 2011-12-30 | 2014-12-09 | General Electric Company | Turbine rotor blade platform cooling |
| US9249673B2 (en) | 2011-12-30 | 2016-02-02 | General Electric Company | Turbine rotor blade platform cooling |
| US20130170983A1 (en) * | 2012-01-04 | 2013-07-04 | General Electric Company | Turbine assembly and method for reducing fluid flow between turbine components |
| US9810070B2 (en) | 2013-05-15 | 2017-11-07 | General Electric Company | Turbine rotor blade for a turbine section of a gas turbine |
| EP3030751B8 (en) | 2013-08-05 | 2021-04-07 | Raytheon Technologies Corporation | Gas turbine engine component and corresponding method of forming a gas turbine engine component |
| US9528377B2 (en) | 2013-08-21 | 2016-12-27 | General Electric Company | Method and system for cooling rotor blade angelwings |
| WO2015057310A2 (en) * | 2013-09-17 | 2015-04-23 | United Technologies Corporation | Platform cooling core for a gas turbine engine rotor blade |
| US20150184538A1 (en) * | 2013-12-30 | 2015-07-02 | General Electric Company | Interior cooling circuits in turbine blades |
| FR3034129B1 (fr) | 2015-03-27 | 2019-05-17 | Safran Aircraft Engines | Aube mobile de turbine a conception amelioree pour turbomachine d'aeronef |
| EP3232000A1 (de) | 2016-04-15 | 2017-10-18 | Siemens Aktiengesellschaft | Plattform einer laufschaufel mit filmkühlungsöffnungen an der plattform und zugehörige strömugsmaschine |
| US10436037B2 (en) | 2016-07-22 | 2019-10-08 | General Electric Company | Blade with parallel corrugated surfaces on inner and outer surfaces |
| US10450868B2 (en) * | 2016-07-22 | 2019-10-22 | General Electric Company | Turbine rotor blade with coupon having corrugated surface(s) |
| JP6860383B2 (ja) * | 2017-03-10 | 2021-04-14 | 川崎重工業株式会社 | タービン翼の冷却構造 |
| US10941671B2 (en) * | 2017-03-23 | 2021-03-09 | General Electric Company | Gas turbine engine component incorporating a seal slot |
| WO2018208370A2 (en) * | 2017-03-29 | 2018-11-15 | Siemens Aktiengesellschaft | Turbine rotor blade with airfoil cooling integrated with impingement platform cooling |
| US10323520B2 (en) | 2017-06-13 | 2019-06-18 | General Electric Company | Platform cooling arrangement in a turbine rotor blade |
| EP3447245A1 (en) | 2017-08-22 | 2019-02-27 | Siemens Aktiengesellschaft | Turbine blade foot |
| US20190264569A1 (en) * | 2018-02-23 | 2019-08-29 | General Electric Company | Turbine rotor blade with exiting hole to deliver fluid to boundary layer film |
| US11220916B2 (en) | 2020-01-22 | 2022-01-11 | General Electric Company | Turbine rotor blade with platform with non-linear cooling passages by additive manufacture |
| US11248471B2 (en) | 2020-01-22 | 2022-02-15 | General Electric Company | Turbine rotor blade with angel wing with coolant transfer passage between adjacent wheel space portions by additive manufacture |
-
2020
- 2020-01-22 US US16/749,167 patent/US11248471B2/en active Active
-
2021
- 2021-01-14 WO PCT/US2021/013387 patent/WO2021150418A1/en not_active Ceased
- 2021-01-14 KR KR1020227024486A patent/KR102889298B1/ko active Active
- 2021-01-14 JP JP2022538315A patent/JP7646670B2/ja active Active
- 2021-01-14 EP EP21704126.8A patent/EP4093944B1/en active Active
- 2021-01-14 CN CN202180007604.7A patent/CN114867930B/zh active Active
Also Published As
| Publication number | Publication date |
|---|---|
| WO2021150418A1 (en) | 2021-07-29 |
| US11248471B2 (en) | 2022-02-15 |
| US20210222566A1 (en) | 2021-07-22 |
| KR20220125257A (ko) | 2022-09-14 |
| EP4093944A1 (en) | 2022-11-30 |
| CN114867930A (zh) | 2022-08-05 |
| EP4093944B1 (en) | 2025-07-09 |
| KR102889298B1 (ko) | 2025-11-25 |
| JP7646670B2 (ja) | 2025-03-17 |
| JP2023513663A (ja) | 2023-04-03 |
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Legal Events
| Date | Code | Title | Description |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| TA01 | Transfer of patent application right |
Effective date of registration: 20240111 Address after: Swiss Baden Applicant after: GENERAL ELECTRIC CO. LTD. Address before: New York, United States Applicant before: General Electric Co. |
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| TA01 | Transfer of patent application right | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |