IL63012A - Wafer tip cap for rotor blades particularly of a gas turbine - Google Patents

Wafer tip cap for rotor blades particularly of a gas turbine

Info

Publication number
IL63012A
IL63012A IL63012A IL6301281A IL63012A IL 63012 A IL63012 A IL 63012A IL 63012 A IL63012 A IL 63012A IL 6301281 A IL6301281 A IL 6301281A IL 63012 A IL63012 A IL 63012A
Authority
IL
Israel
Prior art keywords
gas turbine
rotor blades
tip cap
wafer tip
blades particularly
Prior art date
Application number
IL63012A
Other versions
IL63012A0 (en
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 IL63012A0 publication Critical patent/IL63012A0/en
Publication of IL63012A publication Critical patent/IL63012A/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
    • 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)
  • Mechanical Treatment Of Semiconductor (AREA)
IL63012A 1980-06-05 1981-06-02 Wafer tip cap for rotor blades particularly of a gas turbine IL63012A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US15654980A 1980-06-05 1980-06-05

Publications (2)

Publication Number Publication Date
IL63012A0 IL63012A0 (en) 1981-09-13
IL63012A true IL63012A (en) 1984-10-31

Family

ID=22560030

Family Applications (1)

Application Number Title Priority Date Filing Date
IL63012A IL63012A (en) 1980-06-05 1981-06-02 Wafer tip cap for rotor blades particularly of a gas turbine

Country Status (8)

Country Link
JP (1) JPS5728803A (en)
BE (1) BE889078A (en)
DE (1) DE3122485A1 (en)
FR (1) FR2484015A1 (en)
GB (1) GB2077364B (en)
IL (1) IL63012A (en)
NO (1) NO811831L (en)
SE (1) SE8103503L (en)

Families Citing this family (4)

* 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
FR2689176B1 (en) * 1992-03-25 1995-07-13 Snecma DAWN REFRIGERATED FROM TURBO-MACHINE.
US5476364A (en) * 1992-10-27 1995-12-19 United Technologies Corporation Tip seal and anti-contamination for turbine blades
JP2955252B2 (en) * 1997-06-26 1999-10-04 三菱重工業株式会社 Gas turbine blade tip shroud

Also Published As

Publication number Publication date
GB2077364B (en) 1983-10-26
NO811831L (en) 1981-12-07
FR2484015A1 (en) 1981-12-11
DE3122485A1 (en) 1982-04-15
BE889078A (en) 1981-10-01
JPS5728803A (en) 1982-02-16
SE8103503L (en) 1981-12-06
IL63012A0 (en) 1981-09-13
GB2077364A (en) 1981-12-16

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