IT1142247B - Rotore in ceramica per turbine a gas - Google Patents

Rotore in ceramica per turbine a gas

Info

Publication number
IT1142247B
IT1142247B IT47655/81A IT4765581A IT1142247B IT 1142247 B IT1142247 B IT 1142247B IT 47655/81 A IT47655/81 A IT 47655/81A IT 4765581 A IT4765581 A IT 4765581A IT 1142247 B IT1142247 B IT 1142247B
Authority
IT
Italy
Prior art keywords
gas turbines
ceramic rotor
rotor
ceramic
turbines
Prior art date
Application number
IT47655/81A
Other languages
English (en)
Other versions
IT8147655A0 (it
Inventor
Edwin F C Cain
Original Assignee
Rockwell International 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 Rockwell International Corp filed Critical Rockwell International Corp
Publication of IT8147655A0 publication Critical patent/IT8147655A0/it
Application granted granted Critical
Publication of IT1142247B publication Critical patent/IT1142247B/it

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
    • F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3084—Fixing blades to rotors; Blade roots ; Blade spacers the blades being made of ceramics
    • 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
    • F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F01D21/04—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position
    • F01D21/045—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position special arrangements in stators or in rotors dealing with breaking-off of part of rotor
    • 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
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/284—Selection of ceramic materials
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/06—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages
    • F02C3/073—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages the compressor and turbine stages being concentric

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Materials Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
IT47655/81A 1980-02-04 1981-01-28 Rotore in ceramica per turbine a gas IT1142247B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US11829580A 1980-02-04 1980-02-04

Publications (2)

Publication Number Publication Date
IT8147655A0 IT8147655A0 (it) 1981-01-28
IT1142247B true IT1142247B (it) 1986-10-08

Family

ID=22377719

Family Applications (1)

Application Number Title Priority Date Filing Date
IT47655/81A IT1142247B (it) 1980-02-04 1981-01-28 Rotore in ceramica per turbine a gas

Country Status (7)

Country Link
JP (1) JPS56124603A (it)
DE (1) DE3103821C2 (it)
ES (1) ES498630A0 (it)
FR (1) FR2475113A1 (it)
GB (1) GB2069065A (it)
IT (1) IT1142247B (it)
SE (1) SE8100355L (it)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4580943A (en) * 1980-12-29 1986-04-08 The United States Of America As Represented By The Secretary Of The Army Turbine wheel for hot gas turbine engine
GB2161110B (en) * 1984-07-07 1988-03-23 Rolls Royce An annular bladed member having an integral shroud and a method of manufacture thereof
GB2164098B (en) * 1984-09-07 1988-12-07 Rolls Royce Improvements in or relating to aerofoil section members for turbine engines
DE3508889C1 (de) * 1985-03-13 1992-02-20 Alpine Ag, 8900 Augsburg Windsichter mit verschleissfreiem Sichtrad
FR2613772B1 (fr) * 1987-04-13 1991-06-28 Gros Jean Marc Compresseur, roue de turbine monobloc. redresseur, distributeur monobloc. entree d'air, tuyere d'echappement monobloc
US8011877B2 (en) * 2008-11-24 2011-09-06 General Electric Company Fiber composite reinforced aircraft gas turbine engine drums with radially inwardly extending blades
DE102009012749B4 (de) * 2009-03-12 2012-08-30 Siemens Aktiengesellschaft Endstufe mit Faserverbund
FR2951226B1 (fr) * 2009-10-14 2013-01-04 Turbomeca Dispositif de filtrage d'air en entree de moteur a combustion interne avec moyen de ventilation
WO2013040679A1 (en) * 2011-09-23 2013-03-28 Socpra Sciences Et Génie S.E.C. Rotor assembly having a concentric arrangement of a turbine portion, a cooling channel and a reinforcement wall
FR3005690B1 (fr) * 2013-05-16 2018-07-06 Gerard Cerdan Turboreacteur a compresseur et turbine monoblocs (tr a ctm)
US11208893B2 (en) 2015-05-25 2021-12-28 Socpra Sciences Et Genie S.E.C. High temperature ceramic rotary turbomachinery
GB201616239D0 (en) * 2016-09-23 2016-11-09 Intelligent Power Generation Limited Axial Turbine
EP3545173A4 (en) * 2016-11-25 2020-07-29 Societé de Commercialisation des Produits de la Recherche Appliquée SOCPRA Sciences et Génie S.E.C HIGH TEMPERATURE CERAMIC ROTARY TURBOMACHINE

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3042366A (en) * 1958-05-05 1962-07-03 Holmquist Ernst Rudolf Magnus Axial flow gas turbine
US3635577A (en) * 1968-04-11 1972-01-18 Aerostatic Ltd Coaxial unit
DE2027861C3 (de) * 1970-06-06 1973-12-06 Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen Scheibenförmiges Laufrad fur hoch tourige Axialturbinen
IT975329B (it) * 1972-10-23 1974-07-20 Fiat Spa Struttura di parti metalliche e nom metalliche statiche o rotanti per ambienti ad alta temperatura particolarmente per rotori e stato ri di turbine a gas
SE375583B (it) * 1973-05-22 1975-04-21 United Turbine Ab & Co
US4017209A (en) * 1975-12-15 1977-04-12 United Technologies Corporation Turbine rotor construction

Also Published As

Publication number Publication date
JPS56124603A (en) 1981-09-30
IT8147655A0 (it) 1981-01-28
ES8204058A1 (es) 1982-04-01
ES498630A0 (es) 1982-04-01
DE3103821A1 (de) 1981-12-03
DE3103821C2 (de) 1985-04-04
SE8100355L (sv) 1981-08-05
FR2475113B1 (it) 1985-03-22
FR2475113A1 (fr) 1981-08-07
GB2069065A (en) 1981-08-19

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