IT1012310B - Turbina con disco forato di sup porto delle palette - Google Patents

Turbina con disco forato di sup porto delle palette

Info

Publication number
IT1012310B
IT1012310B IT2263974A IT2263974A IT1012310B IT 1012310 B IT1012310 B IT 1012310B IT 2263974 A IT2263974 A IT 2263974A IT 2263974 A IT2263974 A IT 2263974A IT 1012310 B IT1012310 B IT 1012310B
Authority
IT
Italy
Prior art keywords
sup
vanes
perforated
turbine
disc port
Prior art date
Application number
IT2263974A
Other languages
English (en)
Original Assignee
British Leyland Uk Ltd
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 British Leyland Uk Ltd filed Critical British Leyland Uk Ltd
Application granted granted Critical
Publication of IT1012310B publication Critical patent/IT1012310B/it

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
    • F01D5/10Anti- vibration means
    • 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
    • F01D5/34Rotor-blade aggregates of unitary construction, e.g. formed of sheet laminae

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
IT2263974A 1973-05-14 1974-05-13 Turbina con disco forato di sup porto delle palette IT1012310B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2293073A GB1458524A (en) 1973-05-14 1973-05-14 Turbine rotor discs

Publications (1)

Publication Number Publication Date
IT1012310B true IT1012310B (it) 1977-03-10

Family

ID=10187365

Family Applications (1)

Application Number Title Priority Date Filing Date
IT2263974A IT1012310B (it) 1973-05-14 1974-05-13 Turbina con disco forato di sup porto delle palette

Country Status (4)

Country Link
JP (1) JPS5031208A (it)
DE (1) DE2423036A1 (it)
GB (1) GB1458524A (it)
IT (1) IT1012310B (it)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4926535A (it) * 1972-07-06 1974-03-09
JPS5378218U (it) * 1976-11-24 1978-06-29
US4536932A (en) * 1982-11-22 1985-08-27 United Technologies Corporation Method for eliminating low cycle fatigue cracking in integrally bladed disks
DE3402084A1 (de) * 1984-01-21 1985-08-01 W. Schlafhorst & Co, 4050 Mönchengladbach Verfahren und vorrichtung zur spinnfasernformation
DE3448514C2 (de) * 1984-01-21 1995-08-31 Brockmanns Karl Josef Dr Ing Faservorlageverstreckvorrichtung
US9133720B2 (en) * 2007-12-28 2015-09-15 United Technologies Corporation Integrally bladed rotor with slotted outer rim
CH701914A1 (de) 2009-09-30 2011-03-31 Alstom Technology Ltd Dampfturbine mit Entlastungsnut am Rotor im Bereich des Schubausgleichskolbens.
DE102009052305A1 (de) * 2009-11-07 2011-05-12 Mtu Aero Engines Gmbh Blisk, Gasturbine und Verfahren zur Herstellung einer derartigen Blisk
US9714577B2 (en) 2013-10-24 2017-07-25 Honeywell International Inc. Gas turbine engine rotors including intra-hub stress relief features and methods for the manufacture thereof
US9683447B2 (en) * 2014-04-11 2017-06-20 Honeywell International Inc. Components resistant to traveling wave vibration and methods for manufacturing the same
US10040122B2 (en) 2014-09-22 2018-08-07 Honeywell International Inc. Methods for producing gas turbine engine rotors and other powdered metal articles having shaped internal cavities
CN104949823A (zh) * 2015-05-19 2015-09-30 北京华清燃气轮机与煤气化联合循环工程技术有限公司 一种改善转子动力学特性的方法
DE102018200832A1 (de) * 2018-01-19 2019-07-25 MTU Aero Engines AG Rotor, insbesondere Blisk einer Gasturbine, mit aufgelöstem Rim und Verfahren zum Herstellen desselben

Also Published As

Publication number Publication date
JPS5031208A (it) 1975-03-27
GB1458524A (en) 1976-12-15
DE2423036A1 (de) 1974-12-05

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