FR896520A - Turbo-machine axiale - Google Patents

Turbo-machine axiale

Info

Publication number
FR896520A
FR896520A FR896520DA FR896520A FR 896520 A FR896520 A FR 896520A FR 896520D A FR896520D A FR 896520DA FR 896520 A FR896520 A FR 896520A
Authority
FR
France
Prior art keywords
machine
axial turbo
turbo
axial
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)
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.)
Sulzer AG
Original Assignee
Sulzer AG
Gebrueder Sulzer AG
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 Sulzer AG, Gebrueder Sulzer AG filed Critical Sulzer AG
Application granted granted Critical
Publication of FR896520A publication Critical patent/FR896520A/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
    • F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3023—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses
    • F01D5/303—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses in a circumferential slot
    • F01D5/3038—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses in a circumferential slot the slot having inwardly directed abutment faces on both sides
    • 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
    • F01D5/32—Locking, e.g. by final locking blades or keys

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR896520D 1942-08-13 1943-07-13 Turbo-machine axiale Expired FR896520A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH896520X 1942-08-13

Publications (1)

Publication Number Publication Date
FR896520A true FR896520A (fr) 1945-02-23

Family

ID=4546256

Family Applications (1)

Application Number Title Priority Date Filing Date
FR896520D Expired FR896520A (fr) 1942-08-13 1943-07-13 Turbo-machine axiale

Country Status (1)

Country Link
FR (1) FR896520A (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1724442A1 (fr) * 2005-05-18 2006-11-22 Siemens Aktiengesellschaft Pied d'aube de turbine
EP1690011B1 (fr) * 2003-12-06 2017-04-26 General Electric Technology GmbH Rotor pour un compresseur

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1690011B1 (fr) * 2003-12-06 2017-04-26 General Electric Technology GmbH Rotor pour un compresseur
EP1724442A1 (fr) * 2005-05-18 2006-11-22 Siemens Aktiengesellschaft Pied d'aube de turbine

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