FR1122205A - Perfectionnements apportés aux turbines à gaz, notamment aux turbines axipètes - Google Patents

Perfectionnements apportés aux turbines à gaz, notamment aux turbines axipètes

Info

Publication number
FR1122205A
FR1122205A FR1122205DA FR1122205A FR 1122205 A FR1122205 A FR 1122205A FR 1122205D A FR1122205D A FR 1122205DA FR 1122205 A FR1122205 A FR 1122205A
Authority
FR
France
Prior art keywords
turbines
axipetal
improvements made
gas
gas turbines
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
Other languages
English (en)
Inventor
Ennemond Maillet
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.)
Office National dEtudes et de Recherches Aerospatiales ONERA
Original Assignee
Office National dEtudes et de Recherches Aerospatiales ONERA
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 Office National dEtudes et de Recherches Aerospatiales ONERA filed Critical Office National dEtudes et de Recherches Aerospatiales ONERA
Application granted granted Critical
Publication of FR1122205A publication Critical patent/FR1122205A/fr
Expired legal-status Critical Current

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
    • F01D5/12—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
    • 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
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/04—Blade-carrying members, e.g. rotors for radial-flow machines or engines
    • F01D5/043—Blade-carrying members, e.g. rotors for radial-flow machines or engines of the axial inlet- radial outlet, or vice versa, type
    • F01D5/046—Heating, heat insulation or cooling means

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Materials Engineering (AREA)
FR1122205D 1950-07-12 1950-07-12 Perfectionnements apportés aux turbines à gaz, notamment aux turbines axipètes Expired FR1122205A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1122205T 1950-07-12

Publications (1)

Publication Number Publication Date
FR1122205A true FR1122205A (fr) 1956-09-04

Family

ID=9632482

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1122205D Expired FR1122205A (fr) 1950-07-12 1950-07-12 Perfectionnements apportés aux turbines à gaz, notamment aux turbines axipètes

Country Status (1)

Country Link
FR (1) FR1122205A (fr)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4175911A (en) * 1975-06-20 1979-11-27 Daimler-Benz Aktiengesellschaft Radial turbine wheel for a gas turbine
US4335997A (en) * 1980-01-16 1982-06-22 General Motors Corporation Stress resistant hybrid radial turbine wheel
EP0276656A2 (fr) * 1987-01-24 1988-08-03 KSB Aktiengesellschaft Dispositif de fixation d'une roue à arbres de pompe centrifuge en matière fragile
US4923370A (en) * 1988-11-28 1990-05-08 Allied-Signal Inc. Radial turbine wheel
EP0408010A1 (fr) * 1989-07-12 1991-01-16 Praxair Technology, Inc. Turbomachine avec canal pour la récupération du fluide qui fuit d'un joint d'étanchéité
US20150016999A1 (en) * 2013-03-08 2015-01-15 Rolls-Royce Corporation Multi-piece impeller
EP3081747A1 (fr) * 2015-04-15 2016-10-19 Honeywell International Inc. Turbo-machine ayant des canaux de refroidissement
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
EP2653652A3 (fr) * 2012-04-19 2018-04-04 Honeywell International Inc. Turbine radiale divisée axialement
EP2650474A3 (fr) * 2012-04-11 2018-04-11 Honeywell International Inc. Turbines radiales à fentes axiales et leurs procédés de fabrication
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

Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4175911A (en) * 1975-06-20 1979-11-27 Daimler-Benz Aktiengesellschaft Radial turbine wheel for a gas turbine
US4335997A (en) * 1980-01-16 1982-06-22 General Motors Corporation Stress resistant hybrid radial turbine wheel
EP0276656A2 (fr) * 1987-01-24 1988-08-03 KSB Aktiengesellschaft Dispositif de fixation d'une roue à arbres de pompe centrifuge en matière fragile
EP0276656A3 (fr) * 1987-01-24 1989-01-04 KSB Aktiengesellschaft Dispositif de fixation d'une roue à arbres de pompe centrifuge en matière fragile
US4923370A (en) * 1988-11-28 1990-05-08 Allied-Signal Inc. Radial turbine wheel
EP0371207A1 (fr) * 1988-11-28 1990-06-06 AlliedSignal Inc. Roue de turbine radiale
EP0408010A1 (fr) * 1989-07-12 1991-01-16 Praxair Technology, Inc. Turbomachine avec canal pour la récupération du fluide qui fuit d'un joint d'étanchéité
EP2650474A3 (fr) * 2012-04-11 2018-04-11 Honeywell International Inc. Turbines radiales à fentes axiales et leurs procédés de fabrication
EP2653652A3 (fr) * 2012-04-19 2018-04-04 Honeywell International Inc. Turbine radiale divisée axialement
US9759225B2 (en) * 2013-03-08 2017-09-12 Rolls-Royce Corporation Multi-piece impeller
US20150016999A1 (en) * 2013-03-08 2015-01-15 Rolls-Royce Corporation Multi-piece impeller
US10527055B2 (en) * 2013-03-08 2020-01-07 Rolls-Royce Corporation Multi-piece impeller
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
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
US10807166B2 (en) 2014-09-22 2020-10-20 Honeywell International Inc. Methods for producing gas turbine engine rotors and other powdered metal articles having shaped internal cavities
US11305348B2 (en) 2014-09-22 2022-04-19 Honeywell International Inc. Methods for producing gas turbine engine rotors and other powdered metal articles having shaped internal cavities
US9850760B2 (en) 2015-04-15 2017-12-26 Honeywell International Inc. Directed cooling for rotating machinery
EP3081747A1 (fr) * 2015-04-15 2016-10-19 Honeywell International Inc. Turbo-machine ayant des canaux de refroidissement

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