DE602004008950D1 - Versteifung einer hohlen turbinenschaufel - Google Patents

Versteifung einer hohlen turbinenschaufel

Info

Publication number
DE602004008950D1
DE602004008950D1 DE602004008950T DE602004008950T DE602004008950D1 DE 602004008950 D1 DE602004008950 D1 DE 602004008950D1 DE 602004008950 T DE602004008950 T DE 602004008950T DE 602004008950 T DE602004008950 T DE 602004008950T DE 602004008950 D1 DE602004008950 D1 DE 602004008950D1
Authority
DE
Germany
Prior art keywords
stiffing
turbine blade
hollow turbine
hollow
blade
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
Application number
DE602004008950T
Other languages
English (en)
Other versions
DE602004008950T2 (de
Inventor
Steven John Fett
Scott Walker Smith
Bich Nhu Le
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Pratt and Whitney Canada Corp
Original Assignee
Pratt and Whitney Canada 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 Pratt and Whitney Canada Corp filed Critical Pratt and Whitney Canada Corp
Publication of DE602004008950D1 publication Critical patent/DE602004008950D1/de
Application granted granted Critical
Publication of DE602004008950T2 publication Critical patent/DE602004008950T2/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F01D5/16—Form or construction for counteracting blade vibration
    • 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
    • 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
    • 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
    • F05D2260/00—Function
    • F05D2260/96—Preventing, counteracting or reducing vibration or noise
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S416/00—Fluid reaction surfaces, i.e. impellers
    • Y10S416/50—Vibration damping features
DE602004008950T 2003-10-16 2004-07-19 Versteifung einer hohlen turbinenschaufel Active DE602004008950T2 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US685707 1984-12-24
US10/685,707 US7001150B2 (en) 2003-10-16 2003-10-16 Hollow turbine blade stiffening
PCT/CA2004/001023 WO2005035947A1 (en) 2003-10-16 2004-07-19 Hollow turbine blade stiffening

Publications (2)

Publication Number Publication Date
DE602004008950D1 true DE602004008950D1 (de) 2007-10-25
DE602004008950T2 DE602004008950T2 (de) 2008-06-12

Family

ID=34435408

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602004008950T Active DE602004008950T2 (de) 2003-10-16 2004-07-19 Versteifung einer hohlen turbinenschaufel

Country Status (6)

Country Link
US (1) US7001150B2 (de)
EP (1) EP1673518B1 (de)
JP (1) JP2007508486A (de)
CA (1) CA2542285C (de)
DE (1) DE602004008950T2 (de)
WO (1) WO2005035947A1 (de)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7413409B2 (en) * 2006-02-14 2008-08-19 General Electric Company Turbine airfoil with weight reduction plenum
US7857588B2 (en) * 2007-07-06 2010-12-28 United Technologies Corporation Reinforced airfoils
US8221083B2 (en) 2008-04-15 2012-07-17 United Technologies Corporation Asymmetrical rotor blade fir-tree attachment
US8282354B2 (en) * 2008-04-16 2012-10-09 United Technologies Corporation Reduced weight blade for a gas turbine engine
US8926289B2 (en) * 2012-03-08 2015-01-06 Hamilton Sundstrand Corporation Blade pocket design
US9617860B2 (en) 2012-12-20 2017-04-11 United Technologies Corporation Fan blades for gas turbine engines with reduced stress concentration at leading edge
US20140255207A1 (en) * 2012-12-21 2014-09-11 General Electric Company Turbine rotor blades having mid-span shrouds
US20150322797A1 (en) * 2014-05-09 2015-11-12 United Technologies Corporation Blade element cross-ties
US10920594B2 (en) 2018-12-12 2021-02-16 Solar Turbines Incorporated Modal response tuned turbine blade
US11168569B1 (en) * 2020-04-17 2021-11-09 General Electric Company Blades having tip pockets

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2615520A (en) * 1947-11-26 1952-10-28 Curtiss Wright Corp Reinforced propeller blade
US2954208A (en) * 1953-01-09 1960-09-27 Gen Motors Corp Air foil section
US2925996A (en) * 1955-02-23 1960-02-23 Stalker Corp Blades for compressors and turbines
US3310116A (en) * 1966-02-16 1967-03-21 Mitsui Shipbuilding Eng Marine propeller
US3383093A (en) * 1966-06-23 1968-05-14 Gen Electric Hollow turbomachinery blades
US3626580A (en) * 1968-10-01 1971-12-14 Gen Motors Corp Method of manufacturing disc brake caliper housings
US3761201A (en) * 1969-04-23 1973-09-25 Avco Corp Hollow turbine blade having diffusion bonded therein
US3626568A (en) * 1969-04-23 1971-12-14 Avco Corp Method for bonding pins into holes in a hollow turbine blade
US3606580A (en) * 1969-09-10 1971-09-20 Cyclops Corp Hollow airfoil members
BE795073A (fr) * 1972-03-02 1973-05-29 Gen Electric Procede pour la fabrication d'aubes creuses
US4650399A (en) * 1982-06-14 1987-03-17 United Technologies Corporation Rotor blade for a rotary machine
JPS60228705A (ja) 1984-04-26 1985-11-14 Mitsubishi Heavy Ind Ltd 中空翼
FR2695163B1 (fr) * 1992-09-02 1994-10-28 Snecma Aube creuse pour turbomachine et son procédé de fabrication.
US5328331A (en) * 1993-06-28 1994-07-12 General Electric Company Turbine airfoil with double shell outer wall
US5692881A (en) * 1995-06-08 1997-12-02 United Technologies Corporation Hollow metallic structure and method of manufacture
JPH09280003A (ja) * 1996-04-16 1997-10-28 Toshiba Corp ガスタービン冷却動翼
US5988982A (en) * 1997-09-09 1999-11-23 Lsp Technologies, Inc. Altering vibration frequencies of workpieces, such as gas turbine engine blades
DE19905887C1 (de) * 1999-02-11 2000-08-24 Abb Alstom Power Ch Ag Hohlgegossenes Bauteil
US6033186A (en) * 1999-04-16 2000-03-07 General Electric Company Frequency tuned hybrid blade
US6481972B2 (en) 2000-12-22 2002-11-19 General Electric Company Turbine bucket natural frequency tuning rib
US6502303B2 (en) * 2001-05-07 2003-01-07 Chromalloy Gas Turbine Corporation Method of repairing a turbine blade tip

Also Published As

Publication number Publication date
US20050084380A1 (en) 2005-04-21
EP1673518A1 (de) 2006-06-28
EP1673518B1 (de) 2007-09-12
US7001150B2 (en) 2006-02-21
WO2005035947A1 (en) 2005-04-21
JP2007508486A (ja) 2007-04-05
CA2542285C (en) 2011-06-14
CA2542285A1 (en) 2005-04-21
DE602004008950T2 (de) 2008-06-12

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Legal Events

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8364 No opposition during term of opposition