JP6356410B2 - タービンロータブレード先端シュラウドと共に使用するためのフィレット - Google Patents
タービンロータブレード先端シュラウドと共に使用するためのフィレット Download PDFInfo
- Publication number
- JP6356410B2 JP6356410B2 JP2013244507A JP2013244507A JP6356410B2 JP 6356410 B2 JP6356410 B2 JP 6356410B2 JP 2013244507 A JP2013244507 A JP 2013244507A JP 2013244507 A JP2013244507 A JP 2013244507A JP 6356410 B2 JP6356410 B2 JP 6356410B2
- Authority
- JP
- Japan
- Prior art keywords
- airfoil
- fillet
- tip shroud
- tip
- contour
- 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
- F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
- F01D5/225—Blade-to-blade connections, e.g. for damping vibrations by shrouding
-
- 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
- F01D5/142—Shape, i.e. outer, aerodynamic form of the blades of successive rotor or stator blade-rows
- F01D5/143—Contour of the outer or inner working fluid flow path wall, i.e. shroud or hub contour
-
- 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
- F05D2240/307—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 tip 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
- F05D2250/74—Shape given by a set or table of xyz-coordinates
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 |
|---|---|---|---|
| US13/690,361 | 2012-11-30 | ||
| US13/690,361 US9322282B2 (en) | 2012-11-30 | 2012-11-30 | Fillet for use with a turbine rotor blade tip shroud |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2014109273A JP2014109273A (ja) | 2014-06-12 |
| JP2014109273A5 JP2014109273A5 (enExample) | 2017-01-12 |
| JP6356410B2 true JP6356410B2 (ja) | 2018-07-11 |
Family
ID=49709532
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2013244507A Active JP6356410B2 (ja) | 2012-11-30 | 2013-11-27 | タービンロータブレード先端シュラウドと共に使用するためのフィレット |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US9322282B2 (enExample) |
| EP (1) | EP2738352A1 (enExample) |
| JP (1) | JP6356410B2 (enExample) |
| CN (1) | CN103850717B (enExample) |
Families Citing this family (30)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US10267158B2 (en) * | 2014-12-22 | 2019-04-23 | United Technologies Corporation | Airfoil fillet |
| US20170009587A1 (en) * | 2015-07-06 | 2017-01-12 | United Technologies Corporation | Method for generating an airfoil including an aerodynamically-shaped fillet and airfoils including the aerodynamically-shaped fillet |
| US10001014B2 (en) | 2016-02-09 | 2018-06-19 | General Electric Company | Turbine bucket profile |
| US10190417B2 (en) | 2016-02-09 | 2019-01-29 | General Electric Company | Turbine bucket having non-axisymmetric endwall contour and profile |
| US10161255B2 (en) | 2016-02-09 | 2018-12-25 | General Electric Company | Turbine nozzle having non-axisymmetric endwall contour (EWC) |
| US10190421B2 (en) * | 2016-02-09 | 2019-01-29 | General Electric Company | Turbine bucket having tip shroud fillet, tip shroud cross-drilled apertures and profile |
| US10221710B2 (en) | 2016-02-09 | 2019-03-05 | General Electric Company | Turbine nozzle having non-axisymmetric endwall contour (EWC) and profile |
| US10156149B2 (en) | 2016-02-09 | 2018-12-18 | General Electric Company | Turbine nozzle having fillet, pinbank, throat region and profile |
| US10125623B2 (en) | 2016-02-09 | 2018-11-13 | General Electric Company | Turbine nozzle profile |
| US10196908B2 (en) | 2016-02-09 | 2019-02-05 | General Electric Company | Turbine bucket having part-span connector and profile |
| DE102016211315A1 (de) * | 2016-06-23 | 2017-12-28 | MTU Aero Engines AG | Lauf- oder Leitschaufel mit erhabenen Bereichen |
| US10443392B2 (en) * | 2016-07-13 | 2019-10-15 | Safran Aircraft Engines | Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the second stage of a turbine |
| US10443393B2 (en) * | 2016-07-13 | 2019-10-15 | Safran Aircraft Engines | Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the seventh stage of a turbine |
| US10513934B2 (en) | 2017-01-19 | 2019-12-24 | General Electric Company | Z-notch shape for a turbine blade tip shroud |
| WO2018147162A1 (ja) | 2017-02-07 | 2018-08-16 | 株式会社Ihi | 軸流機械の翼 |
| US10526899B2 (en) * | 2017-02-14 | 2020-01-07 | General Electric Company | Turbine blade having a tip shroud |
| US10247007B2 (en) | 2017-05-02 | 2019-04-02 | General Electric Company | Airfoil shape for a turbine rotor blade |
| US10352170B2 (en) | 2017-05-02 | 2019-07-16 | General Electric Company | Airfoil shape for a turbine rotor blade |
| US10422227B2 (en) | 2017-05-02 | 2019-09-24 | General Electric Company | Airfoil shape for a turbine rotor blade |
| US10280774B2 (en) | 2017-05-03 | 2019-05-07 | General Electric Company | Turbine nozzle airfoil profile |
| US10415406B2 (en) | 2017-05-03 | 2019-09-17 | General Electric Company | Turbine nozzle airfoil profile |
| US10408072B2 (en) | 2017-05-08 | 2019-09-10 | General Electric Company | Turbine nozzle airfoil profile |
| US10724378B2 (en) * | 2017-05-11 | 2020-07-28 | Safran Aircraft Engines | Optimized aerodynamic profile for a turbine blade, in particular for a rotary wheel of a turbine |
| US10533440B2 (en) | 2017-05-15 | 2020-01-14 | General Electric Company | Turbine nozzle airfoil profile |
| US10436034B2 (en) | 2017-05-15 | 2019-10-08 | General Electric Company | Airfoil shape for a turbine rotor blade |
| US10704392B2 (en) | 2018-03-23 | 2020-07-07 | General Electric Company | Tip shroud fillets for turbine rotor blades |
| US11098591B1 (en) * | 2019-02-04 | 2021-08-24 | Raytheon Technologies Corporation | Turbine blade with contoured fillet |
| US11236620B1 (en) * | 2021-02-24 | 2022-02-01 | General Electric Company | Turbine blade tip shroud surface profiles |
| US11506064B2 (en) * | 2021-03-09 | 2022-11-22 | General Electric Company | Turbine blade tip shroud surface profiles |
| US11713685B2 (en) * | 2021-03-09 | 2023-08-01 | General Electric Company | Turbine blade tip shroud with protrusion under wing |
Family Cites Families (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH10317910A (ja) * | 1997-05-20 | 1998-12-02 | Mitsubishi Heavy Ind Ltd | ガスタービンの圧縮機静翼環 |
| US6893216B2 (en) | 2003-07-17 | 2005-05-17 | General Electric Company | Turbine bucket tip shroud edge profile |
| US6857853B1 (en) * | 2003-08-13 | 2005-02-22 | General Electric Company | Conical tip shroud fillet for a turbine bucket |
| US7063509B2 (en) | 2003-09-05 | 2006-06-20 | General Electric Company | Conical tip shroud fillet for a turbine bucket |
| US7066713B2 (en) | 2004-01-31 | 2006-06-27 | United Technologies Corporation | Rotor blade for a rotary machine |
| US7568882B2 (en) | 2007-01-12 | 2009-08-04 | General Electric Company | Impingement cooled bucket shroud, turbine rotor incorporating the same, and cooling method |
| FR2924958B1 (fr) * | 2007-12-14 | 2012-08-24 | Snecma | Aube de turbomachine realisee de fonderie avec un engraissement local de la section de la pale |
| US8057186B2 (en) | 2008-04-22 | 2011-11-15 | General Electric Company | Shape for a turbine bucket tip shroud |
| GB0901129D0 (en) * | 2009-01-26 | 2009-03-11 | Rolls Royce Plc | Rotor blade |
-
2012
- 2012-11-30 US US13/690,361 patent/US9322282B2/en active Active
-
2013
- 2013-11-27 JP JP2013244507A patent/JP6356410B2/ja active Active
- 2013-11-28 EP EP13194959.6A patent/EP2738352A1/en not_active Withdrawn
- 2013-11-29 CN CN201310629865.XA patent/CN103850717B/zh active Active
Also Published As
| Publication number | Publication date |
|---|---|
| EP2738352A1 (en) | 2014-06-04 |
| US9322282B2 (en) | 2016-04-26 |
| US20140154079A1 (en) | 2014-06-05 |
| CN103850717A (zh) | 2014-06-11 |
| CN103850717B (zh) | 2017-07-28 |
| JP2014109273A (ja) | 2014-06-12 |
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