SG130114A1 - Turbine airfoil platform platypus for low buttress stress - Google Patents

Turbine airfoil platform platypus for low buttress stress

Info

Publication number
SG130114A1
SG130114A1 SG200605221-1A SG2006052211A SG130114A1 SG 130114 A1 SG130114 A1 SG 130114A1 SG 2006052211 A SG2006052211 A SG 2006052211A SG 130114 A1 SG130114 A1 SG 130114A1
Authority
SG
Singapore
Prior art keywords
platform
platypus
stress
buttress
turbine airfoil
Prior art date
Application number
SG200605221-1A
Inventor
Bryan P Dube
Randall J Butcher
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 SG130114A1 publication Critical patent/SG130114A1/en

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
    • F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3007—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
    • 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
    • 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
    • F05D2240/80—Platforms for stationary or moving blades
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

A blade is provided for use in a gas turbine engine. The blade has a platform, an airfoil portion extending radially from a first side of the platform, and an attachment portion extending from a second or underside side of the platform. The attachment portion includes a buttress which abuts the second side of the platform. The blade is provided with additional material on the second side of the platform for redistributing load away from the buttress.
SG200605221-1A 2005-08-03 2006-08-02 Turbine airfoil platform platypus for low buttress stress SG130114A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US11/197,162 US20070031260A1 (en) 2005-08-03 2005-08-03 Turbine airfoil platform platypus for low buttress stress

Publications (1)

Publication Number Publication Date
SG130114A1 true SG130114A1 (en) 2007-03-20

Family

ID=37387422

Family Applications (1)

Application Number Title Priority Date Filing Date
SG200605221-1A SG130114A1 (en) 2005-08-03 2006-08-02 Turbine airfoil platform platypus for low buttress stress

Country Status (6)

Country Link
US (1) US20070031260A1 (en)
EP (1) EP1749970B1 (en)
JP (1) JP2007040295A (en)
CN (1) CN1908379A (en)
SG (1) SG130114A1 (en)
TW (1) TW200710319A (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102010004854A1 (en) * 2010-01-16 2011-07-21 MTU Aero Engines GmbH, 80995 Blade for a turbomachine and turbomachine
US9976433B2 (en) * 2010-04-02 2018-05-22 United Technologies Corporation Gas turbine engine with non-axisymmetric surface contoured rotor blade platform
WO2019136672A1 (en) * 2018-01-11 2019-07-18 贵州智慧能源科技有限公司 Turbine blade flange plate based on spline curve design
FR3107301B1 (en) * 2020-02-19 2022-03-11 Safran Aircraft Engines blade for a moving bladed wheel of an aircraft turbomachine comprising a sealing spoiler with optimized scalable section

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2807436A (en) * 1952-03-25 1957-09-24 Gen Motors Corp Turbine wheel and bucket assembly
US4259037A (en) * 1976-12-13 1981-03-31 General Electric Company Liquid cooled gas turbine buckets
GB2228541B (en) * 1989-02-23 1993-04-14 Rolls Royce Plc Device for damping vibrations in turbomachinery blades
US5302085A (en) * 1992-02-03 1994-04-12 General Electric Company Turbine blade damper
FR2712631B1 (en) * 1993-11-19 1998-08-21 Gen Electric Rotor fin and rotor disc-fin assembly comprising such a fin.
FR2743845B1 (en) * 1996-01-23 1998-02-20 Snecma MOBILE BLOWER BLADE WITH SECURITY PROFILE
US6158962A (en) * 1999-04-30 2000-12-12 General Electric Company Turbine blade with ribbed platform
US6511294B1 (en) * 1999-09-23 2003-01-28 General Electric Company Reduced-stress compressor blisk flowpath
US6561761B1 (en) * 2000-02-18 2003-05-13 General Electric Company Fluted compressor flowpath
US6422820B1 (en) * 2000-06-30 2002-07-23 General Electric Company Corner tang fan blade
US6506016B1 (en) * 2001-11-15 2003-01-14 General Electric Company Angel wing seals for blades of a gas turbine and methods for determining angel wing seal profiles
FR2851285B1 (en) * 2003-02-13 2007-03-16 Snecma Moteurs REALIZATION OF TURBINES FOR TURBOMACHINES HAVING DIFFERENT ADJUSTED RESONANCE FREQUENCIES AND METHOD FOR ADJUSTING THE RESONANCE FREQUENCY OF A TURBINE BLADE

Also Published As

Publication number Publication date
EP1749970B1 (en) 2015-05-13
TW200710319A (en) 2007-03-16
US20070031260A1 (en) 2007-02-08
EP1749970A2 (en) 2007-02-07
JP2007040295A (en) 2007-02-15
CN1908379A (en) 2007-02-07
EP1749970A3 (en) 2010-05-26

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