CN106948866B - 涡轮机及其涡轮叶片 - Google Patents

涡轮机及其涡轮叶片 Download PDF

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Publication number
CN106948866B
CN106948866B CN201611166841.5A CN201611166841A CN106948866B CN 106948866 B CN106948866 B CN 106948866B CN 201611166841 A CN201611166841 A CN 201611166841A CN 106948866 B CN106948866 B CN 106948866B
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China
Prior art keywords
span
airfoil
throat
throat width
distribution
Prior art date
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CN201611166841.5A
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English (en)
Chinese (zh)
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CN106948866A (zh
Inventor
S.索尼
R.J.古斯塔夫松
R.舒罕
J.A.内维尔
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General Electric Company PLC
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General Electric Co
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Publication date
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Publication of CN106948866A publication Critical patent/CN106948866A/zh
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Publication of CN106948866B publication Critical patent/CN106948866B/zh
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    • 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
    • F01D5/141—Shape, i.e. outer, aerodynamic form
    • F01D5/142—Shape, i.e. outer, aerodynamic form of the blades of successive rotor or stator blade-rows
    • 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
    • F01D5/145—Means for influencing boundary layers or secondary circulations
    • 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
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/26—Rotors specially for elastic fluids
    • F04D29/32—Rotors specially for elastic fluids for axial flow pumps
    • F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
    • F04D29/324—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
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • 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
    • F05D2240/122—Fluid guiding means, e.g. vanes related to the trailing edge 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
    • F05D2240/301—Cross-sectional characteristics
    • 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
    • F05D2250/71—Shape curved
    • 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
    • F05D2250/74—Shape given by a set or table of xyz-coordinates

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
CN201611166841.5A 2015-12-18 2016-12-16 涡轮机及其涡轮叶片 Active CN106948866B (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US14/973894 2015-12-18
US14/973,894 US9957805B2 (en) 2015-12-18 2015-12-18 Turbomachine and turbine blade therefor

Publications (2)

Publication Number Publication Date
CN106948866A CN106948866A (zh) 2017-07-14
CN106948866B true CN106948866B (zh) 2021-10-12

Family

ID=58994626

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201611166841.5A Active CN106948866B (zh) 2015-12-18 2016-12-16 涡轮机及其涡轮叶片

Country Status (5)

Country Link
US (1) US9957805B2 (enExample)
JP (1) JP6929050B2 (enExample)
CN (1) CN106948866B (enExample)
DE (1) DE102016124151A1 (enExample)
IT (1) IT201600127373A1 (enExample)

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JP6396093B2 (ja) * 2014-06-26 2018-09-26 三菱重工業株式会社 タービン動翼列、タービン段落及び軸流タービン
US10655471B2 (en) * 2015-02-10 2020-05-19 Mitsubishi Hitachi Power Systems, Ltd. Turbine and gas turbine
WO2017105259A1 (en) 2015-12-18 2017-06-22 General Electric Company Vane and corresponding turbomachine
US10544681B2 (en) * 2015-12-18 2020-01-28 General Electric Company Turbomachine and turbine blade therefor
US9995144B2 (en) * 2016-02-18 2018-06-12 General Electric Company Turbine blade centroid shifting method and system
US10774650B2 (en) * 2017-10-12 2020-09-15 Raytheon Technologies Corporation Gas turbine engine airfoil
US11280199B2 (en) 2018-11-21 2022-03-22 Honeywell International Inc. Throat distribution for a rotor and rotor blade having camber and location of local maximum thickness distribution
US10859094B2 (en) 2018-11-21 2020-12-08 Honeywell International Inc. Throat distribution for a rotor and rotor blade having camber and location of local maximum thickness distribution
US20210381385A1 (en) * 2020-06-03 2021-12-09 Honeywell International Inc. Characteristic distribution for rotor blade of booster rotor
US11401816B1 (en) * 2021-04-30 2022-08-02 General Electric Company Compressor rotor blade airfoils
US11459892B1 (en) 2021-04-30 2022-10-04 General Electric Company Compressor stator vane airfoils
US11441427B1 (en) 2021-04-30 2022-09-13 General Electric Company Compressor rotor blade airfoils
US11326620B1 (en) 2021-04-30 2022-05-10 General Electric Company Compressor stator vane airfoils
US11293454B1 (en) 2021-04-30 2022-04-05 General Electric Company Compressor stator vane airfoils
CN115263804A (zh) 2021-04-30 2022-11-01 通用电气公司 压缩机转子叶片翼型件
US11480062B1 (en) 2021-04-30 2022-10-25 General Electric Company Compressor stator vane airfoils
US11519273B1 (en) * 2021-04-30 2022-12-06 General Electric Company Compressor rotor blade airfoils
US11519272B2 (en) * 2021-04-30 2022-12-06 General Electric Company Compressor rotor blade airfoils
US11414996B1 (en) 2021-04-30 2022-08-16 General Electric Company Compressor rotor blade airfoils
US11643932B2 (en) 2021-04-30 2023-05-09 General Electric Company Compressor rotor blade airfoils
GB202107128D0 (en) * 2021-05-19 2021-06-30 Rolls Royce Plc Nozzle guide vane
US11512595B1 (en) * 2022-02-04 2022-11-29 Pratt & Whitney Canada Corp. Turbine blade airfoil profile
US11867081B1 (en) * 2023-01-26 2024-01-09 Pratt & Whitney Canada Corp. Turbine blade airfoil profile
US12305529B1 (en) * 2024-05-21 2025-05-20 Ge Vernova Infrastructure Technology Llc Compressor stator vane airfoils

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CN1243910A (zh) * 1998-07-31 2000-02-09 东芝株式会社 汽轮机的高效叶片结构
CN1769647A (zh) * 2004-04-09 2006-05-10 诺沃皮尼奥内有限公司 用于燃气轮机的第二相的高效定子
CN1773079A (zh) * 2004-04-09 2006-05-17 诺沃皮尼奥内有限公司 用于燃气轮机的第一相的高效转子

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CN1243910A (zh) * 1998-07-31 2000-02-09 东芝株式会社 汽轮机的高效叶片结构
CN1769647A (zh) * 2004-04-09 2006-05-10 诺沃皮尼奥内有限公司 用于燃气轮机的第二相的高效定子
CN1773079A (zh) * 2004-04-09 2006-05-17 诺沃皮尼奥内有限公司 用于燃气轮机的第一相的高效转子

Also Published As

Publication number Publication date
DE102016124151A1 (de) 2017-06-22
JP2017122439A (ja) 2017-07-13
CN106948866A (zh) 2017-07-14
US20170175530A1 (en) 2017-06-22
JP6929050B2 (ja) 2021-09-01
IT201600127373A1 (it) 2018-06-16
US9957805B2 (en) 2018-05-01

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Effective date of registration: 20240103

Address after: Swiss Baden

Patentee after: GENERAL ELECTRIC CO. LTD.

Address before: New York State, USA

Patentee before: General Electric Co.