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SE8103502L - ROTATING LEATHER FOR ROTOR SHEETS - Google Patents

ROTATING LEATHER FOR ROTOR SHEETS

Info

Publication number
SE8103502L
SE8103502L SE8103502A SE8103502A SE8103502L SE 8103502 L SE8103502 L SE 8103502L SE 8103502 A SE8103502 A SE 8103502A SE 8103502 A SE8103502 A SE 8103502A SE 8103502 L SE8103502 L SE 8103502L
Authority
SE
Sweden
Prior art keywords
rotor sheets
rotating leather
tip
leather
rotating
Prior art date
Application number
SE8103502A
Other languages
Unknown language ( )
Swedish (sv)
Inventor
G P Liang
Original Assignee
United Technologies 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 United Technologies Corp filed Critical United Technologies Corp
Publication of SE8103502L publication Critical patent/SE8103502L/en

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
    • F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/187—Convection cooling
    • 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
    • F01D5/182—Transpiration cooling
    • F01D5/184—Blade walls being made of perforated sheet laminae
    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Supercharger (AREA)
  • Polishing Bodies And Polishing Tools (AREA)

Abstract

The tip cap is fabricated from a plurality of chordwisely extending wafers 30, 32. The outermost wafer 30 being of an abrasive material such as silicon carbide embedded in a metal matrix. Convective cooling of the tip is established through the incorporation of laterally extending passages 34 between adjacent wafer elements. <IMAGE>
SE8103502A 1980-06-05 1981-06-03 ROTATING LEATHER FOR ROTOR SHEETS SE8103502L (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US15654880A 1980-06-05 1980-06-05

Publications (1)

Publication Number Publication Date
SE8103502L true SE8103502L (en) 1981-12-06

Family

ID=22560024

Family Applications (1)

Application Number Title Priority Date Filing Date
SE8103502A SE8103502L (en) 1980-06-05 1981-06-03 ROTATING LEATHER FOR ROTOR SHEETS

Country Status (8)

Country Link
JP (1) JPS5728802A (en)
BE (1) BE889077A (en)
DE (1) DE3122484A1 (en)
FR (1) FR2484014A1 (en)
GB (1) GB2077363A (en)
IL (1) IL63011A0 (en)
NO (1) NO811830L (en)
SE (1) SE8103502L (en)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4411597A (en) * 1981-03-20 1983-10-25 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Tip cap for a rotor blade
US4589823A (en) * 1984-04-27 1986-05-20 General Electric Company Rotor blade tip
DE3850681T2 (en) * 1987-02-06 1995-03-09 Wolfgang P Weinhold Rotor blade.
US5667359A (en) * 1988-08-24 1997-09-16 United Technologies Corp. Clearance control for the turbine of a gas turbine engine
US5125798A (en) * 1990-04-13 1992-06-30 General Electric Company Method and apparatus for cooling air flow at gas turbine bucket trailing edge tip
US5261789A (en) * 1992-08-25 1993-11-16 General Electric Company Tip cooled blade
US5486093A (en) * 1993-09-08 1996-01-23 United Technologies Corporation Leading edge cooling of turbine airfoils
GB2310896A (en) * 1996-03-05 1997-09-10 Rolls Royce Plc Air cooled wall
DE19939179B4 (en) * 1999-08-20 2007-08-02 Alstom Coolable blade for a gas turbine
US6932571B2 (en) * 2003-02-05 2005-08-23 United Technologies Corporation Microcircuit cooling for a turbine blade tip
US7481573B2 (en) * 2005-06-30 2009-01-27 Spx Corporation Mixing impeller with pre-shaped tip elements
FR2889243B1 (en) * 2005-07-26 2007-11-02 Snecma TURBINE DAWN
US10145245B2 (en) * 2013-09-24 2018-12-04 United Technologies Corporation Bonded multi-piece gas turbine engine component
GB2551527A (en) * 2016-06-21 2017-12-27 Rolls Royce Plc Method of producing a gas turbine engine component with an abrasive coating

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3301526A (en) * 1964-12-22 1967-01-31 United Aircraft Corp Stacked-wafer turbine vane or blade
US4118146A (en) * 1976-08-11 1978-10-03 United Technologies Corporation Coolable wall
US4221539A (en) * 1977-04-20 1980-09-09 The Garrett Corporation Laminated airfoil and method for turbomachinery
US4214355A (en) * 1977-12-21 1980-07-29 General Electric Company Method for repairing a turbomachinery blade tip
US4169020A (en) * 1977-12-21 1979-09-25 General Electric Company Method for making an improved gas seal

Also Published As

Publication number Publication date
FR2484014A1 (en) 1981-12-11
BE889077A (en) 1981-10-01
JPS5728802A (en) 1982-02-16
DE3122484A1 (en) 1982-03-25
GB2077363A (en) 1981-12-16
IL63011A0 (en) 1981-09-13
NO811830L (en) 1981-12-07

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