JPS61113902U - - Google Patents

Info

Publication number
JPS61113902U
JPS61113902U JP1985189183U JP18918385U JPS61113902U JP S61113902 U JPS61113902 U JP S61113902U JP 1985189183 U JP1985189183 U JP 1985189183U JP 18918385 U JP18918385 U JP 18918385U JP S61113902 U JPS61113902 U JP S61113902U
Authority
JP
Japan
Prior art keywords
tip
blade
cavity
trailing edge
opening
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.)
Granted
Application number
JP1985189183U
Other languages
English (en)
Japanese (ja)
Other versions
JPS6349521Y2 (US20080293856A1-20081127-C00150.png
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 filed Critical
Publication of JPS61113902U publication Critical patent/JPS61113902U/ja
Application granted granted Critical
Publication of JPS6349521Y2 publication Critical patent/JPS6349521Y2/ja
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/20Specially-shaped blade tips to seal space between tips and stator
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/18Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/187Convection cooling
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/20Three-dimensional
    • F05D2250/23Three-dimensional prismatic
    • F05D2250/231Three-dimensional prismatic cylindrical
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/20Three-dimensional
    • F05D2250/23Three-dimensional prismatic
    • F05D2250/232Three-dimensional prismatic conical
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/20Three-dimensional
    • F05D2250/24Three-dimensional ellipsoidal
    • F05D2250/241Three-dimensional ellipsoidal spherical

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
JP1985189183U 1981-09-02 1985-12-10 Expired JPS6349521Y2 (US20080293856A1-20081127-C00150.png)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US29881981A 1981-09-02 1981-09-02

Publications (2)

Publication Number Publication Date
JPS61113902U true JPS61113902U (US20080293856A1-20081127-C00150.png) 1986-07-18
JPS6349521Y2 JPS6349521Y2 (US20080293856A1-20081127-C00150.png) 1988-12-20

Family

ID=23152126

Family Applications (2)

Application Number Title Priority Date Filing Date
JP57149370A Pending JPS5844201A (ja) 1981-09-02 1982-08-30 タ−ビンロ−タ羽根
JP1985189183U Expired JPS6349521Y2 (US20080293856A1-20081127-C00150.png) 1981-09-02 1985-12-10

Family Applications Before (1)

Application Number Title Priority Date Filing Date
JP57149370A Pending JPS5844201A (ja) 1981-09-02 1982-08-30 タ−ビンロ−タ羽根

Country Status (8)

Country Link
JP (2) JPS5844201A (US20080293856A1-20081127-C00150.png)
AR (1) AR228676A1 (US20080293856A1-20081127-C00150.png)
BE (1) BE894260A (US20080293856A1-20081127-C00150.png)
BR (1) BR8205083A (US20080293856A1-20081127-C00150.png)
CA (1) CA1191456A (US20080293856A1-20081127-C00150.png)
GB (1) GB2105415B (US20080293856A1-20081127-C00150.png)
IT (1) IT1153721B (US20080293856A1-20081127-C00150.png)
MX (1) MX155481A (US20080293856A1-20081127-C00150.png)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2155558A (en) * 1984-03-10 1985-09-25 Rolls Royce Turbomachinery rotor blades
US4589823A (en) * 1984-04-27 1986-05-20 General Electric Company Rotor blade tip
US4682933A (en) * 1984-10-17 1987-07-28 Rockwell International Corporation Labyrinthine turbine-rotor-blade tip seal
US4761116A (en) * 1987-05-11 1988-08-02 General Electric Company Turbine blade with tip vent
US4893987A (en) * 1987-12-08 1990-01-16 General Electric Company Diffusion-cooled blade tip cap
US5667359A (en) * 1988-08-24 1997-09-16 United Technologies Corp. Clearance control for the turbine of a gas turbine engine
JPH04260047A (ja) * 1991-02-15 1992-09-16 Konica Corp シームレスベルト感光体の製造方法
JPH04109401U (ja) * 1991-03-12 1992-09-22 アドバンス・コージエネレーシヨンシステム技術研究組合 空冷動翼
US5476364A (en) * 1992-10-27 1995-12-19 United Technologies Corporation Tip seal and anti-contamination for turbine blades
US6652235B1 (en) * 2002-05-31 2003-11-25 General Electric Company Method and apparatus for reducing turbine blade tip region temperatures
US7270514B2 (en) * 2004-10-21 2007-09-18 General Electric Company Turbine blade tip squealer and rebuild method
US8157504B2 (en) * 2009-04-17 2012-04-17 General Electric Company Rotor blades for turbine engines
GB201112803D0 (en) 2011-07-26 2011-09-07 Rolls Royce Plc Master component for flow calibration
JP6159151B2 (ja) * 2013-05-24 2017-07-05 三菱日立パワーシステムズ株式会社 タービン動翼
US10041358B2 (en) 2014-05-08 2018-08-07 United Technologies Corporation Gas turbine engine blade squealer pockets
US20160258302A1 (en) * 2015-03-05 2016-09-08 General Electric Company Airfoil and method for managing pressure at tip of airfoil
US10107108B2 (en) 2015-04-29 2018-10-23 General Electric Company Rotor blade having a flared tip

Also Published As

Publication number Publication date
AR228676A1 (es) 1983-03-30
IT8223026A0 (it) 1982-08-30
GB2105415A (en) 1983-03-23
MX155481A (es) 1988-03-17
BR8205083A (pt) 1983-08-09
BE894260A (fr) 1983-02-28
JPS6349521Y2 (US20080293856A1-20081127-C00150.png) 1988-12-20
JPS5844201A (ja) 1983-03-15
GB2105415B (en) 1985-08-07
CA1191456A (en) 1985-08-06
IT1153721B (it) 1987-01-14

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