JP6824623B2 - フレア状先端を有するロータブレード - Google Patents
フレア状先端を有するロータブレード Download PDFInfo
- Publication number
- JP6824623B2 JP6824623B2 JP2016084882A JP2016084882A JP6824623B2 JP 6824623 B2 JP6824623 B2 JP 6824623B2 JP 2016084882 A JP2016084882 A JP 2016084882A JP 2016084882 A JP2016084882 A JP 2016084882A JP 6824623 B2 JP6824623 B2 JP 6824623B2
- Authority
- JP
- Japan
- Prior art keywords
- pressure side
- side wall
- tip
- rotor blade
- airfoil
- 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
- 239000002826 coolant Substances 0.000 claims description 12
- 239000012530 fluid Substances 0.000 claims description 11
- 238000004891 communication Methods 0.000 claims description 4
- 238000011144 upstream manufacturing Methods 0.000 claims description 4
- 238000002485 combustion reaction Methods 0.000 claims description 3
- 239000007789 gas Substances 0.000 description 24
- 238000001816 cooling Methods 0.000 description 11
- 239000000567 combustion gas Substances 0.000 description 9
- 238000013461 design Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- 238000010586 diagram Methods 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000010348 incorporation Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
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
- F01D5/141—Shape, i.e. outer, aerodynamic form
-
- 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
- F01D5/20—Specially-shaped blade tips to seal space between tips and stator
-
- 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
- F01D5/188—Convection cooling with an insert in the blade cavity to guide the cooling fluid, e.g. forming a separation wall
- F01D5/189—Convection cooling with an insert in the blade cavity to guide the cooling fluid, e.g. forming a separation wall the insert having a tubular cross-section, e.g. airfoil shape
-
- 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
- F05D2250/30—Arrangement of components
- F05D2250/31—Arrangement of components according to the direction of their main axis or their axis of rotation
- F05D2250/314—Arrangement of components according to the direction of their main axis or their axis of rotation the axes being inclined in relation to each other
-
- 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
- F05D2250/30—Arrangement of components
- F05D2250/32—Arrangement of components according to their shape
- F05D2250/324—Arrangement of components according to their shape divergent
-
- 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
- F05D2250/713—Shape curved inflexed
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US14/699,308 US20160319672A1 (en) | 2015-04-29 | 2015-04-29 | Rotor blade having a flared tip |
US14/699,308 | 2015-04-29 |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2016211545A JP2016211545A (ja) | 2016-12-15 |
JP6824623B2 true JP6824623B2 (ja) | 2021-02-03 |
Family
ID=55808495
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2016084882A Active JP6824623B2 (ja) | 2015-04-29 | 2016-04-21 | フレア状先端を有するロータブレード |
Country Status (4)
Country | Link |
---|---|
US (1) | US20160319672A1 (de) |
EP (1) | EP3088674B1 (de) |
JP (1) | JP6824623B2 (de) |
CN (1) | CN106089313B (de) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20170058680A1 (en) * | 2015-09-02 | 2017-03-02 | General Electric Company | Configurations for turbine rotor blade tips |
US20170145827A1 (en) * | 2015-11-23 | 2017-05-25 | United Technologies Corporation | Turbine blade with airfoil tip vortex control |
US10677066B2 (en) | 2015-11-23 | 2020-06-09 | United Technologies Corporation | Turbine blade with airfoil tip vortex control |
EP3954882B1 (de) * | 2016-03-30 | 2023-05-03 | Mitsubishi Heavy Industries Engine & Turbocharger, Ltd. | Turbolader mit variabler geometrie |
US10443405B2 (en) * | 2017-05-10 | 2019-10-15 | General Electric Company | Rotor blade tip |
CN107559048B (zh) * | 2017-09-22 | 2024-01-30 | 哈尔滨汽轮机厂有限责任公司 | 一种用于中低热值重型燃气轮机发动机的转子叶片 |
KR102021139B1 (ko) * | 2018-04-04 | 2019-10-18 | 두산중공업 주식회사 | 스퀼러 팁을 구비한 터빈 블레이드 |
US10787932B2 (en) * | 2018-07-13 | 2020-09-29 | Honeywell International Inc. | Turbine blade with dust tolerant cooling system |
CN110863862B (zh) * | 2019-12-05 | 2022-12-06 | 中国航发四川燃气涡轮研究院 | 叶尖结构和涡轮 |
US11225874B2 (en) * | 2019-12-20 | 2022-01-18 | Raytheon Technologies Corporation | Turbine engine rotor blade with castellated tip surface |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4761116A (en) * | 1987-05-11 | 1988-08-02 | General Electric Company | Turbine blade with tip vent |
US6179556B1 (en) * | 1999-06-01 | 2001-01-30 | General Electric Company | Turbine blade tip with offset squealer |
US6494678B1 (en) * | 2001-05-31 | 2002-12-17 | General Electric Company | Film cooled blade tip |
US6971851B2 (en) * | 2003-03-12 | 2005-12-06 | Florida Turbine Technologies, Inc. | Multi-metered film cooled blade tip |
GB0813556D0 (en) * | 2008-07-24 | 2008-09-03 | Rolls Royce Plc | A blade for a rotor |
GB201006449D0 (en) * | 2010-04-19 | 2010-06-02 | Rolls Royce Plc | Blades |
GB201100957D0 (en) * | 2011-01-20 | 2011-03-02 | Rolls Royce Plc | Rotor blade |
US20120237358A1 (en) * | 2011-03-17 | 2012-09-20 | Campbell Christian X | Turbine blade tip |
US8801377B1 (en) * | 2011-08-25 | 2014-08-12 | Florida Turbine Technologies, Inc. | Turbine blade with tip cooling and sealing |
US9273561B2 (en) * | 2012-08-03 | 2016-03-01 | General Electric Company | Cooling structures for turbine rotor blade tips |
US10408066B2 (en) * | 2012-08-15 | 2019-09-10 | United Technologies Corporation | Suction side turbine blade tip cooling |
US9334742B2 (en) * | 2012-10-05 | 2016-05-10 | General Electric Company | Rotor blade and method for cooling the rotor blade |
JP6347892B2 (ja) * | 2014-07-07 | 2018-06-27 | シーメンス アクチエンゲゼルシヤフトSiemens Aktiengesellschaft | ガスタービンエンジンブレードスキーラ先端、対応する製造および冷却方法、ならびにガスタービンエンジン |
-
2015
- 2015-04-29 US US14/699,308 patent/US20160319672A1/en not_active Abandoned
-
2016
- 2016-04-21 JP JP2016084882A patent/JP6824623B2/ja active Active
- 2016-04-25 EP EP16166812.4A patent/EP3088674B1/de active Active
- 2016-04-29 CN CN201610276145.3A patent/CN106089313B/zh active Active
Also Published As
Publication number | Publication date |
---|---|
JP2016211545A (ja) | 2016-12-15 |
US20160319672A1 (en) | 2016-11-03 |
CN106089313A (zh) | 2016-11-09 |
EP3088674B1 (de) | 2024-05-29 |
EP3088674A1 (de) | 2016-11-02 |
CN106089313B (zh) | 2020-12-01 |
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