KR100871196B1 - 터빈 노즐 및 이를 포함하는 터빈 - Google Patents

터빈 노즐 및 이를 포함하는 터빈 Download PDF

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Publication number
KR100871196B1
KR100871196B1 KR1020047000462A KR20047000462A KR100871196B1 KR 100871196 B1 KR100871196 B1 KR 100871196B1 KR 1020047000462 A KR1020047000462 A KR 1020047000462A KR 20047000462 A KR20047000462 A KR 20047000462A KR 100871196 B1 KR100871196 B1 KR 100871196B1
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South Korea
Prior art keywords
airfoil
turbine
nozzle
values
section
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Expired - Lifetime
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KR1020047000462A
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Korean (ko)
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KR20040018453A (ko
Inventor
비엘레크크레이그알렌
보우단
브루너프레더릭제임스
Original Assignee
제너럴 일렉트릭 캄파니
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Priority claimed from PCT/US2002/021887 external-priority patent/WO2003006797A1/en
Publication of KR20040018453A publication Critical patent/KR20040018453A/ko
Application granted granted Critical
Publication of KR100871196B1 publication Critical patent/KR100871196B1/ko
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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
    • 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
    • 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

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Non-Silver Salt Photosensitive Materials And Non-Silver Salt Photography (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Materials For Photolithography (AREA)
KR1020047000462A 2001-07-13 2002-07-09 터빈 노즐 및 이를 포함하는 터빈 Expired - Lifetime KR100871196B1 (ko)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US09/903,853 US6503054B1 (en) 2001-07-13 2001-07-13 Second-stage turbine nozzle airfoil
US09/903,853 2001-07-13
PCT/US2002/021887 WO2003006797A1 (en) 2001-07-13 2002-07-09 Second-stage turbine nozzle airfoil

Publications (2)

Publication Number Publication Date
KR20040018453A KR20040018453A (ko) 2004-03-03
KR100871196B1 true KR100871196B1 (ko) 2008-12-01

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ID=25418163

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Application Number Title Priority Date Filing Date
KR1020047000462A Expired - Lifetime KR100871196B1 (ko) 2001-07-13 2002-07-09 터빈 노즐 및 이를 포함하는 터빈

Country Status (5)

Country Link
US (1) US6503054B1 (enExample)
EP (1) EP1409846A1 (enExample)
JP (1) JP2004534921A (enExample)
KR (1) KR100871196B1 (enExample)
CN (1) CN1329631C (enExample)

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US7568891B2 (en) * 2006-11-22 2009-08-04 Pratt & Whitney Canada Corp. HP turbine vane airfoil profile
US7568889B2 (en) * 2006-11-22 2009-08-04 Pratt & Whitney Canada Corp. HP turbine blade airfoil profile
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US8393870B2 (en) 2010-09-08 2013-03-12 United Technologies Corporation Turbine blade airfoil
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US8807950B2 (en) 2011-11-28 2014-08-19 General Electric Company Turbine nozzle airfoil profile
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US9322279B2 (en) 2012-07-02 2016-04-26 United Technologies Corporation Airfoil cooling arrangement
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US10822976B2 (en) 2013-06-03 2020-11-03 General Electric Company Nozzle insert rib cap
US10480323B2 (en) 2016-01-12 2019-11-19 United Technologies Corporation Gas turbine engine turbine blade airfoil profile
US10196908B2 (en) 2016-02-09 2019-02-05 General Electric Company Turbine bucket having part-span connector and profile
US10156149B2 (en) 2016-02-09 2018-12-18 General Electric Company Turbine nozzle having fillet, pinbank, throat region and profile
US10190421B2 (en) 2016-02-09 2019-01-29 General Electric Company Turbine bucket having tip shroud fillet, tip shroud cross-drilled apertures and profile
US10190417B2 (en) 2016-02-09 2019-01-29 General Electric Company Turbine bucket having non-axisymmetric endwall contour and profile
US10161255B2 (en) 2016-02-09 2018-12-25 General Electric Company Turbine nozzle having non-axisymmetric endwall contour (EWC)
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US10221710B2 (en) 2016-02-09 2019-03-05 General Electric Company Turbine nozzle having non-axisymmetric endwall contour (EWC) and profile
US10443393B2 (en) * 2016-07-13 2019-10-15 Safran Aircraft Engines Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the seventh stage of a turbine
US10443392B2 (en) * 2016-07-13 2019-10-15 Safran Aircraft Engines Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the second stage of a turbine
US10087952B2 (en) * 2016-09-23 2018-10-02 General Electric Company Airfoil shape for first stage compressor stator vane
US10352170B2 (en) 2017-05-02 2019-07-16 General Electric Company Airfoil shape for a turbine rotor blade
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Also Published As

Publication number Publication date
CN1568396A (zh) 2005-01-19
US20030021680A1 (en) 2003-01-30
CN1329631C (zh) 2007-08-01
EP1409846A1 (en) 2004-04-21
JP2004534921A (ja) 2004-11-18
US6503054B1 (en) 2003-01-07
KR20040018453A (ko) 2004-03-03

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