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JPS4857003A - - Google Patents

Info

Publication number
JPS4857003A
JPS4857003A JP47111975A JP11197572A JPS4857003A JP S4857003 A JPS4857003 A JP S4857003A JP 47111975 A JP47111975 A JP 47111975A JP 11197572 A JP11197572 A JP 11197572A JP S4857003 A JPS4857003 A JP S4857003A
Authority
JP
Japan
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.)
Pending
Application number
JP47111975A
Other languages
Japanese (ja)
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 JPS4857003A publication Critical patent/JPS4857003A/ja
Pending 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
    • 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
    • F01D5/021Blade-carrying members, e.g. rotors for flow machines or engines with only one axial stage

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
JP47111975A 1971-11-08 1972-11-08 Pending JPS4857003A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2155344A DE2155344A1 (en) 1971-11-08 1971-11-08 INTEGRAL TURBINE WHEEL WITH OPEN AXIAL BREAKTHROUGHTS ON THE OUTER WREATH AND CONTROLLED WREATH Cracks

Publications (1)

Publication Number Publication Date
JPS4857003A true JPS4857003A (en) 1973-08-10

Family

ID=5824478

Family Applications (1)

Application Number Title Priority Date Filing Date
JP47111975A Pending JPS4857003A (en) 1971-11-08 1972-11-08

Country Status (6)

Country Link
US (1) US3817657A (en)
JP (1) JPS4857003A (en)
DE (1) DE2155344A1 (en)
FR (1) FR2160107A5 (en)
GB (1) GB1417132A (en)
IT (1) IT970290B (en)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
IT1025260B (en) * 1973-11-16 1978-08-10 Mtu Muenchen Gmbh TURBINE WITH INTERNAL COOLING OF THE CROWN AND WITH PRESCRIBED POSITIONS OF BREAKAGE
US3897171A (en) * 1974-06-25 1975-07-29 Westinghouse Electric Corp Ceramic turbine rotor disc and blade configuration
US4477222A (en) * 1982-09-30 1984-10-16 The United States Of America As Represented By The Secretary Of The Air Force Mounting construction for turbine vane assembly
US5593274A (en) * 1995-03-31 1997-01-14 General Electric Co. Closed or open circuit cooling of turbine rotor components
AT2429U3 (en) * 1998-07-10 1999-01-25 Jakadofsky Peter TURBINE WHEEL
FR2866057B1 (en) * 2004-02-06 2006-04-28 Snecma Moteurs DEVICE FOR BALANCING A ROTOR DISC, DISC EQUIPPED WITH SUCH A DEVICE, AND ROTOR HAVING SUCH A DISK
GB2468528B (en) * 2009-03-13 2011-03-30 Rolls Royce Plc Vibration damper
US8157514B2 (en) * 2009-03-19 2012-04-17 Honeywell International Inc. Components for gas turbine engines
DE102010042707A1 (en) * 2010-10-20 2012-04-26 Siemens Aktiengesellschaft Turbine component for, e.g. gas turbine used in gas-fired power plant, comprises end hole formed perpendicular to guide bore which is formed vertical to edge portion to form breaking point between inner wall of guide bore and flat side
DE102015111746A1 (en) * 2015-07-20 2017-01-26 Rolls-Royce Deutschland Ltd & Co Kg Cooled turbine wheel, in particular for an aircraft engine
FR3070965B1 (en) * 2017-09-13 2019-08-23 Safran Aircraft Engines NON-CARBONATED BLOWER PROPELLER HUB WITH BREAKING PRIMER AREA FOR DETECTION AND PREVENTION OF DAMAGE
DE102018200832A1 (en) * 2018-01-19 2019-07-25 MTU Aero Engines AG Rotor, in particular blisk of a gas turbine, with dissolved rim and method for producing the same
US11939877B1 (en) 2022-10-21 2024-03-26 Pratt & Whitney Canada Corp. Method and integrally bladed rotor for blade off testing
US12173614B1 (en) * 2023-08-25 2024-12-24 Pratt & Whitney Canada Corp. Test rotor blade for an aircraft engine blade-off test

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2965355A (en) * 1956-01-17 1960-12-20 United Aircraft Corp Turbine disc burst inhibitor
US3255994A (en) * 1963-09-03 1966-06-14 Chrysler Corp Turbine wheel
US3262676A (en) * 1964-05-27 1966-07-26 Chrysler Corp Turbine wheel
US3291446A (en) * 1965-04-13 1966-12-13 Chrysler Corp Turbine wheel
US3395891A (en) * 1967-09-21 1968-08-06 Gen Electric Lock for turbomachinery blades

Also Published As

Publication number Publication date
FR2160107A5 (en) 1973-06-22
IT970290B (en) 1974-04-10
GB1417132A (en) 1975-12-10
US3817657A (en) 1974-06-18
DE2155344A1 (en) 1973-05-17

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