SE8100355L - CERAMIC GAS TURBIN ROTOR - Google Patents

CERAMIC GAS TURBIN ROTOR

Info

Publication number
SE8100355L
SE8100355L SE8100355A SE8100355A SE8100355L SE 8100355 L SE8100355 L SE 8100355L SE 8100355 A SE8100355 A SE 8100355A SE 8100355 A SE8100355 A SE 8100355A SE 8100355 L SE8100355 L SE 8100355L
Authority
SE
Sweden
Prior art keywords
ceramic
ceramic gas
wheel
rotor
gas turbin
Prior art date
Application number
SE8100355A
Other languages
Unknown language ( )
Swedish (sv)
Inventor
Cain E F Cool
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 SE8100355L publication Critical patent/SE8100355L/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
    • F01D5/30—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)

Abstract

The rotor comprises a ceramic wheel 14 having an inner row of turbine blades 16 and an outer row of compressor blades 18 separated by a mid-blade shroud 20, and an outer shroud 22 filament wound with a composite so as to form a hoop 24 providing compression loading of the ceramic components during rotation. The wheel 14 has a ceramic or metallic hub 12 for attachment to a shaft. <IMAGE>
SE8100355A 1980-02-04 1981-01-22 CERAMIC GAS TURBIN ROTOR SE8100355L (en)

Applications Claiming Priority (1)

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

Publications (1)

Publication Number Publication Date
SE8100355L true SE8100355L (en) 1981-08-05

Family

ID=22377719

Family Applications (1)

Application Number Title Priority Date Filing Date
SE8100355A SE8100355L (en) 1980-02-04 1981-01-22 CERAMIC GAS TURBIN ROTOR

Country Status (7)

Country Link
JP (1) JPS56124603A (en)
DE (1) DE3103821C2 (en)
ES (1) ES8204058A1 (en)
FR (1) FR2475113A1 (en)
GB (1) GB2069065A (en)
IT (1) IT1142247B (en)
SE (1) SE8100355L (en)

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 (en) * 1985-03-13 1992-02-20 Alpine Ag, 8900 Augsburg Air classifier with wear-free classifying wheel
FR2613772B1 (en) * 1987-04-13 1991-06-28 Gros Jean Marc COMPRESSOR, MONOBLOCK TURBINE WHEEL. RECTIFIER, MONOBLOCK DISTRIBUTOR. AIR INLET, MONOBLOCK EXHAUST NOZZLE
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 (en) * 2009-03-12 2012-08-30 Siemens Aktiengesellschaft Power amplifier with fiber composite
FR2951226B1 (en) * 2009-10-14 2013-01-04 Turbomeca AIR FILTERING DEVICE INTO INTERNAL COMBUSTION ENGINE INPUT WITH VENTILATION MEANS
CN103975141A (en) * 2011-09-23 2014-08-06 索克普拉科学与工程公司 Rotor assembly having a concentric arrangement of a turbine portion, a cooling channel and a reinforcement wall
FR3005690B1 (en) * 2013-05-16 2018-07-06 Gerard Cerdan COMPRESSOR TURBOREACTOR AND MONOBLOCS TURBINE (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 turbomachinery

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 (en) * 1970-06-06 1973-12-06 Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen Disc-shaped impeller for high-speed axial turbines
IT975329B (en) * 1972-10-23 1974-07-20 Fiat Spa STRUCTURE OF STATIC OR ROTATING METALLIC AND NOM METALLIC PARTS FOR HIGH TEMPERATURE ENVIRONMENTS ESPECIALLY FOR ROTORS AND STATE OF GAS TURBINES
SE375583B (en) * 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
ES498630A0 (en) 1982-04-01
IT8147655A0 (en) 1981-01-28
ES8204058A1 (en) 1982-04-01
IT1142247B (en) 1986-10-08
GB2069065A (en) 1981-08-19
FR2475113B1 (en) 1985-03-22
FR2475113A1 (en) 1981-08-07
DE3103821C2 (en) 1985-04-04
JPS56124603A (en) 1981-09-30
DE3103821A1 (en) 1981-12-03

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