SG10201505408WA - Gas turbine engine blade with variable density and wide chord tip - Google Patents
Gas turbine engine blade with variable density and wide chord tipInfo
- Publication number
- SG10201505408WA SG10201505408WA SG10201505408WA SG10201505408WA SG10201505408WA SG 10201505408W A SG10201505408W A SG 10201505408WA SG 10201505408W A SG10201505408W A SG 10201505408WA SG 10201505408W A SG10201505408W A SG 10201505408WA SG 10201505408W A SG10201505408W A SG 10201505408WA
- Authority
- SG
- Singapore
- Prior art keywords
- gas turbine
- turbine engine
- variable density
- engine blade
- wide chord
- 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
-
- 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
- F01D5/147—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
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
-
- 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
- F05D2230/21—Manufacture essentially without removing material by casting
- F05D2230/211—Manufacture essentially without removing material by casting by precision casting, e.g. microfusing or investment casting
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/10—Metals, alloys or intermetallic compounds
- F05D2300/17—Alloys
- F05D2300/172—Copper alloys
- F05D2300/1723—Nickel-Copper alloy, e.g. Monel
-
- 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
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201462028476P | 2014-07-24 | 2014-07-24 |
Publications (1)
Publication Number | Publication Date |
---|---|
SG10201505408WA true SG10201505408WA (en) | 2016-02-26 |
Family
ID=53773255
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SG10201505408WA SG10201505408WA (en) | 2014-07-24 | 2015-07-09 | Gas turbine engine blade with variable density and wide chord tip |
Country Status (3)
Country | Link |
---|---|
US (2) | US10316671B2 (en) |
EP (1) | EP2977551B1 (en) |
SG (1) | SG10201505408WA (en) |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4431376A (en) | 1980-10-27 | 1984-02-14 | United Technologies Corporation | Airfoil shape for arrays of airfoils |
US5931641A (en) | 1997-04-25 | 1999-08-03 | General Electric Company | Steam turbine blade having areas of different densities |
JP2002213206A (en) * | 2001-01-12 | 2002-07-31 | Mitsubishi Heavy Ind Ltd | Blade structure of gas turbine |
DE102004054752A1 (en) | 2004-11-12 | 2006-05-18 | Rolls-Royce Deutschland Ltd & Co Kg | Blade of a flow machine with extended edge profile depth |
JP2009511811A (en) | 2005-10-11 | 2009-03-19 | アルストム テクノロジー リミテッド | Turbomachinery wing |
US7762783B2 (en) * | 2007-01-11 | 2010-07-27 | General Electric Company | Turbine blade apparatus |
US8734107B2 (en) * | 2011-05-31 | 2014-05-27 | General Electric Company | Ceramic-based tip cap for a turbine bucket |
US10655473B2 (en) | 2012-12-13 | 2020-05-19 | United Technologies Corporation | Gas turbine engine turbine blade leading edge tip trench cooling |
SG11201503276PA (en) | 2012-12-14 | 2015-06-29 | United Technologies Corp | Hybrid turbine blade for improved engine performance or architecture |
SG10201610144XA (en) | 2012-12-14 | 2017-01-27 | United Technologies Corp | Multi-shot casting |
WO2014098961A1 (en) | 2012-12-17 | 2014-06-26 | United Technologies Corporation | Two spool gas generator with improved pressure split |
-
2015
- 2015-07-09 SG SG10201505408WA patent/SG10201505408WA/en unknown
- 2015-07-17 US US14/802,512 patent/US10316671B2/en active Active
- 2015-07-20 EP EP15177509.5A patent/EP2977551B1/en active Active
-
2019
- 2019-04-29 US US16/397,265 patent/US10954799B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
US10316671B2 (en) | 2019-06-11 |
US20200024962A1 (en) | 2020-01-23 |
US10954799B2 (en) | 2021-03-23 |
EP2977551A3 (en) | 2016-05-11 |
US20160024935A1 (en) | 2016-01-28 |
EP2977551A2 (en) | 2016-01-27 |
EP2977551B1 (en) | 2019-10-23 |
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