FR2557206B1 - TWO-STAGE ROTOR ARRANGEMENT WITH IMPROVED CIRCULATION OF THE COOLING AGENT - Google Patents

TWO-STAGE ROTOR ARRANGEMENT WITH IMPROVED CIRCULATION OF THE COOLING AGENT

Info

Publication number
FR2557206B1
FR2557206B1 FR848419767A FR8419767A FR2557206B1 FR 2557206 B1 FR2557206 B1 FR 2557206B1 FR 848419767 A FR848419767 A FR 848419767A FR 8419767 A FR8419767 A FR 8419767A FR 2557206 B1 FR2557206 B1 FR 2557206B1
Authority
FR
France
Prior art keywords
cooling agent
stage rotor
rotor arrangement
improved circulation
circulation
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.)
Expired
Application number
FR848419767A
Other languages
French (fr)
Other versions
FR2557206A1 (en
Inventor
Douglas L Kisling
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Raytheon Technologies Corp
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 FR2557206A1 publication Critical patent/FR2557206A1/en
Application granted granted Critical
Publication of FR2557206B1 publication Critical patent/FR2557206B1/en
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
    • F01D5/02Blade-carrying members, e.g. rotors
    • F01D5/08Heating, heat-insulating or cooling means
    • F01D5/081Cooling fluid being directed on the side of the rotor disc or at the roots of the blades
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12Cooling of plants
    • 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
    • F01D5/30Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3007Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
    • F01D5/3015Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type with side plates
FR848419767A 1983-12-22 1984-12-24 TWO-STAGE ROTOR ARRANGEMENT WITH IMPROVED CIRCULATION OF THE COOLING AGENT Expired FR2557206B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US56445483A 1983-12-22 1983-12-22

Publications (2)

Publication Number Publication Date
FR2557206A1 FR2557206A1 (en) 1985-06-28
FR2557206B1 true FR2557206B1 (en) 1989-11-10

Family

ID=24254543

Family Applications (1)

Application Number Title Priority Date Filing Date
FR848419767A Expired FR2557206B1 (en) 1983-12-22 1984-12-24 TWO-STAGE ROTOR ARRANGEMENT WITH IMPROVED CIRCULATION OF THE COOLING AGENT

Country Status (14)

Country Link
JP (1) JPS60156903A (en)
KR (1) KR850004511A (en)
BE (1) BE901368A (en)
CA (1) CA1209482A (en)
CH (1) CH667896A5 (en)
DE (1) DE3444586A1 (en)
DK (1) DK599084A (en)
FR (1) FR2557206B1 (en)
GB (1) GB2151715B (en)
GR (1) GR82527B (en)
IL (1) IL73764A (en)
NL (1) NL8403845A (en)
TR (1) TR23227A (en)
YU (1) YU217584A (en)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2586061B1 (en) * 1985-08-08 1989-06-09 Snecma MULTIFUNCTIONAL LABYRINTH DISC FOR TURBOMACHINE ROTOR
DE3627306A1 (en) * 1986-02-28 1987-09-03 Mtu Muenchen Gmbh DEVICE FOR VENTILATING ROTOR COMPONENTS FOR COMPRESSORS OF GAS TURBINE ENGINE PLANTS
FR2600377B1 (en) * 1986-06-18 1988-09-02 Snecma DEVICE FOR MONITORING THE COOLING AIR FLOWS OF AN ENGINE TURBINE
DE19705442A1 (en) 1997-02-13 1998-08-20 Bmw Rolls Royce Gmbh Turbine impeller disk with cooling air channels
DE19705441A1 (en) 1997-02-13 1998-08-20 Bmw Rolls Royce Gmbh Turbine impeller disk
DE19828817C2 (en) * 1998-06-27 2000-07-13 Mtu Muenchen Gmbh Rotor for a turbo machine
DE19857554A1 (en) 1998-12-14 2000-06-15 Rolls Royce Deutschland Connection arrangement of two running disks of an axial flow machine
JP4649763B2 (en) * 2001-04-05 2011-03-16 株式会社Ihi Cooling air adjustment structure for turbine blades
FR2867223B1 (en) * 2004-03-03 2006-07-28 Snecma Moteurs TURBOMACHINE AS FOR EXAMPLE A TURBOJET AIRCRAFT
FR3026430B1 (en) * 2014-09-29 2020-07-10 Safran Aircraft Engines TURBINE WHEEL IN A TURBOMACHINE

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB612097A (en) * 1946-10-09 1948-11-08 English Electric Co Ltd Improvements in and relating to the cooling of gas turbine rotors
US2807434A (en) * 1952-04-22 1957-09-24 Gen Motors Corp Turbine rotor assembly
US2858103A (en) * 1956-03-26 1958-10-28 Westinghouse Electric Corp Gas turbine apparatus
GB851306A (en) * 1958-02-04 1960-10-12 Napier & Son Ltd Improvements in or relating to turbine blades
US3056579A (en) * 1959-04-13 1962-10-02 Gen Electric Rotor construction
US3343806A (en) * 1965-05-27 1967-09-26 Gen Electric Rotor assembly for gas turbine engines
CH495496A (en) * 1969-02-26 1970-08-31 Bbc Sulzer Turbomaschinen Turbomachine with a cooled rotor
CA939521A (en) * 1970-04-28 1974-01-08 Bruce R. Branstrom Turbine coolant flow system
US4021138A (en) * 1975-11-03 1977-05-03 Westinghouse Electric Corporation Rotor disk, blade, and seal plate assembly for cooled turbine rotor blades
GB2057573A (en) * 1979-08-30 1981-04-01 Rolls Royce Turbine rotor assembly
CA1187810A (en) * 1981-09-22 1985-05-28 Leroy D. Mclaurin Cooled combustion turbine blade with retrofit blade seal

Also Published As

Publication number Publication date
CA1209482A (en) 1986-08-12
CH667896A5 (en) 1988-11-15
BE901368A (en) 1985-04-16
TR23227A (en) 1989-06-23
GB8431269D0 (en) 1985-01-23
YU217584A (en) 1989-12-31
DK599084D0 (en) 1984-12-14
IL73764A0 (en) 1985-03-31
KR850004511A (en) 1985-07-15
DE3444586A1 (en) 1985-07-04
FR2557206A1 (en) 1985-06-28
GB2151715B (en) 1987-09-16
IL73764A (en) 1989-06-30
GR82527B (en) 1985-01-23
NL8403845A (en) 1985-07-16
GB2151715A (en) 1985-07-24
JPS60156903A (en) 1985-08-17
DK599084A (en) 1985-06-23

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Legal Events

Date Code Title Description
ST Notification of lapse