SG11201501228YA - Compliant cantilevered airfoil - Google Patents
Compliant cantilevered airfoilInfo
- Publication number
- SG11201501228YA SG11201501228YA SG11201501228YA SG11201501228YA SG11201501228YA SG 11201501228Y A SG11201501228Y A SG 11201501228YA SG 11201501228Y A SG11201501228Y A SG 11201501228YA SG 11201501228Y A SG11201501228Y A SG 11201501228YA SG 11201501228Y A SG11201501228Y A SG 11201501228YA
- Authority
- SG
- Singapore
- Prior art keywords
- cantilevered airfoil
- compliant cantilevered
- compliant
- airfoil
- cantilevered
- 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
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
- F01D5/288—Protective coatings for 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
- F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
- F01D11/12—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
- F01D11/122—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part with erodable or abradable material
-
- 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
- F01D5/20—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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
-
- 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
- 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
- F05D2240/10—Stators
- F05D2240/12—Fluid guiding means, e.g. vanes
- F05D2240/125—Fluid guiding means, e.g. vanes related to the tip of a stator vane
-
- 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
-
- 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)
- Chemical & Material Sciences (AREA)
- Materials Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201261692006P | 2012-08-22 | 2012-08-22 | |
PCT/US2013/031276 WO2014031160A1 (en) | 2012-08-22 | 2013-03-14 | Compliant cantilevered airfoil |
Publications (1)
Publication Number | Publication Date |
---|---|
SG11201501228YA true SG11201501228YA (en) | 2015-04-29 |
Family
ID=50150281
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SG11201501228YA SG11201501228YA (en) | 2012-08-22 | 2013-03-14 | Compliant cantilevered airfoil |
Country Status (5)
Country | Link |
---|---|
US (1) | US10584598B2 (en) |
EP (1) | EP2888449B1 (en) |
MY (1) | MY176943A (en) |
SG (1) | SG11201501228YA (en) |
WO (1) | WO2014031160A1 (en) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9995166B2 (en) * | 2014-11-21 | 2018-06-12 | General Electric Company | Turbomachine including a vane and method of assembling such turbomachine |
CN109312658B (en) * | 2016-03-30 | 2022-02-22 | 三菱重工发动机和增压器株式会社 | Variable capacity turbocharger |
KR101901682B1 (en) * | 2017-06-20 | 2018-09-27 | 두산중공업 주식회사 | J Type Cantilevered Vane And Gas Turbine Having The Same |
CN110926745B (en) * | 2019-11-22 | 2020-11-17 | 华中科技大学 | Aero-engine low-pressure turbine rotor and stator blade rub-impact test bed |
US11713679B1 (en) * | 2022-01-27 | 2023-08-01 | Raytheon Technologies Corporation | Tangentially bowed airfoil |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4874031A (en) | 1985-04-01 | 1989-10-17 | Janney David F | Cantilevered integral airfoil method |
US4805351A (en) * | 1988-02-08 | 1989-02-21 | Avco Corporation | Blade airfoil holding system |
US5088892A (en) | 1990-02-07 | 1992-02-18 | United Technologies Corporation | Bowed airfoil for the compression section of a rotary machine |
US5167489A (en) | 1991-04-15 | 1992-12-01 | General Electric Company | Forward swept rotor blade |
US6290465B1 (en) | 1999-07-30 | 2001-09-18 | General Electric Company | Rotor blade |
JP4045993B2 (en) * | 2003-03-28 | 2008-02-13 | 株式会社Ihi | Fan vane, fan for aircraft engine, and aircraft engine |
US7396205B2 (en) * | 2004-01-31 | 2008-07-08 | United Technologies Corporation | Rotor blade for a rotary machine |
CH698109B1 (en) | 2005-07-01 | 2009-05-29 | Alstom Technology Ltd | Turbomachinery blade. |
US7497664B2 (en) | 2005-08-16 | 2009-03-03 | General Electric Company | Methods and apparatus for reducing vibrations induced to airfoils |
US7726937B2 (en) * | 2006-09-12 | 2010-06-01 | United Technologies Corporation | Turbine engine compressor vanes |
US7794201B2 (en) * | 2006-12-22 | 2010-09-14 | General Electric Company | Gas turbine engines including lean stator vanes and methods of assembling the same |
EP1953344B1 (en) | 2007-02-05 | 2012-04-11 | Siemens Aktiengesellschaft | Turbine blade |
US8333559B2 (en) * | 2007-04-03 | 2012-12-18 | Carrier Corporation | Outlet guide vanes for axial flow fans |
EP2133573B1 (en) | 2008-06-13 | 2011-08-17 | Siemens Aktiengesellschaft | Vane or blade for an axial flow compressor |
US8167567B2 (en) * | 2008-12-17 | 2012-05-01 | United Technologies Corporation | Gas turbine engine airfoil |
US8393870B2 (en) | 2010-09-08 | 2013-03-12 | United Technologies Corporation | Turbine blade airfoil |
US9181814B2 (en) | 2010-11-24 | 2015-11-10 | United Technology Corporation | Turbine engine compressor stator |
-
2013
- 2013-03-14 WO PCT/US2013/031276 patent/WO2014031160A1/en active Application Filing
- 2013-03-14 SG SG11201501228YA patent/SG11201501228YA/en unknown
- 2013-03-14 US US14/422,368 patent/US10584598B2/en active Active
- 2013-03-14 MY MYPI2015000199A patent/MY176943A/en unknown
- 2013-03-14 EP EP13830598.2A patent/EP2888449B1/en active Active
Also Published As
Publication number | Publication date |
---|---|
EP2888449A1 (en) | 2015-07-01 |
US20150218955A1 (en) | 2015-08-06 |
EP2888449B1 (en) | 2020-04-29 |
US10584598B2 (en) | 2020-03-10 |
WO2014031160A1 (en) | 2014-02-27 |
EP2888449A4 (en) | 2015-10-28 |
MY176943A (en) | 2020-08-27 |
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