JP4307814B2 - 衝撃波が減少された遷音速翼形部 - Google Patents

衝撃波が減少された遷音速翼形部 Download PDF

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Publication number
JP4307814B2
JP4307814B2 JP2002291753A JP2002291753A JP4307814B2 JP 4307814 B2 JP4307814 B2 JP 4307814B2 JP 2002291753 A JP2002291753 A JP 2002291753A JP 2002291753 A JP2002291753 A JP 2002291753A JP 4307814 B2 JP4307814 B2 JP 4307814B2
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Japan
Prior art keywords
turbine
airfoil
blade
trailing edge
turbine blade
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JP2002291753A
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Japanese (ja)
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JP2003138902A (ja
JP2003138902A5 (enExample
Inventor
クレイグ・ミラー・キューネ
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General Electric Co
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General Electric Co
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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
    • F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
    • F01D1/02—Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor, e.g. multi-bladed impulse steam turbines
    • F01D1/04—Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor, e.g. multi-bladed impulse steam turbines traversed by the working-fluid substantially axially
    • 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

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
JP2002291753A 2001-10-05 2002-10-04 衝撃波が減少された遷音速翼形部 Expired - Fee Related JP4307814B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/972443 2001-10-05
US09/972,443 US6682301B2 (en) 2001-10-05 2001-10-05 Reduced shock transonic airfoil

Publications (3)

Publication Number Publication Date
JP2003138902A JP2003138902A (ja) 2003-05-14
JP2003138902A5 JP2003138902A5 (enExample) 2005-11-04
JP4307814B2 true JP4307814B2 (ja) 2009-08-05

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Family Applications (1)

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JP2002291753A Expired - Fee Related JP4307814B2 (ja) 2001-10-05 2002-10-04 衝撃波が減少された遷音速翼形部

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US (2) US6682301B2 (enExample)
EP (1) EP1300547B1 (enExample)
JP (1) JP4307814B2 (enExample)

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US11454120B2 (en) * 2018-12-07 2022-09-27 General Electric Company Turbine airfoil profile
CN111425259A (zh) * 2020-02-27 2020-07-17 合肥通用机械研究院有限公司 一种磁悬浮超音速透平膨胀机
WO2024096946A2 (en) 2022-08-11 2024-05-10 Next Gen Compression Llc Variable geometry supersonic compressor
US12460651B2 (en) 2022-08-11 2025-11-04 Next Gen Compression Llc Method for efficient part load compressor operation
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Also Published As

Publication number Publication date
EP1300547A3 (en) 2009-07-29
EP1300547A2 (en) 2003-04-09
JP2003138902A (ja) 2003-05-14
EP1300547B1 (en) 2013-04-10
USRE42370E1 (en) 2011-05-17
US20030072649A1 (en) 2003-04-17
US6682301B2 (en) 2004-01-27

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