SG10201505408WA - Gas turbine engine blade with variable density and wide chord tip - Google Patents

Gas turbine engine blade with variable density and wide chord tip

Info

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
Application number
SG10201505408WA
Inventor
Vijay Chakka Pitchaiah
d hill James
R Pack David
Original Assignee
United Technologies Corp
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by United Technologies Corp filed Critical United Technologies Corp
Publication of SG10201505408WA publication Critical patent/SG10201505408WA/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/18Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/141Shape, i.e. outer, aerodynamic form
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/147Construction, i.e. structural features, e.g. of weight-saving hollow blades
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/28Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00Manufacture
    • F05D2230/20Manufacture essentially without removing material
    • F05D2230/21Manufacture essentially without removing material by casting
    • F05D2230/211Manufacture essentially without removing material by casting by precision casting, e.g. microfusing or investment casting
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00Materials; Properties thereof
    • F05D2300/10Metals, alloys or intermetallic compounds
    • F05D2300/17Alloys
    • F05D2300/172Copper alloys
    • F05D2300/1723Nickel-Copper alloy, e.g. Monel
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft
SG10201505408WA 2014-07-24 2015-07-09 Gas turbine engine blade with variable density and wide chord tip SG10201505408WA (en)

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)

* Cited by examiner, † Cited by third party
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

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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