FR1192696A - Axial turbomachine - Google Patents

Axial turbomachine

Info

Publication number
FR1192696A
FR1192696A FR1192696DA FR1192696A FR 1192696 A FR1192696 A FR 1192696A FR 1192696D A FR1192696D A FR 1192696DA FR 1192696 A FR1192696 A FR 1192696A
Authority
FR
France
Prior art keywords
axial turbomachine
turbomachine
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
French (fr)
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.)
Rheinmetall Air Defence AG
Maschinenfabrik Oerlikon AG
Original Assignee
Werkzeugmaschinenfabrik Oerlikon Buhrle AG
Maschinenfabrik Oerlikon 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 Werkzeugmaschinenfabrik Oerlikon Buhrle AG, Maschinenfabrik Oerlikon AG filed Critical Werkzeugmaschinenfabrik Oerlikon Buhrle AG
Application granted granted Critical
Publication of FR1192696A publication Critical patent/FR1192696A/en
Expired legal-status Critical Current

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
    • F01D5/30Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3023Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses
    • F01D5/303Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses in a circumferential slot
    • F01D5/3038Fixing 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR1192696D 1957-03-05 1958-03-05 Axial turbomachine Expired FR1192696A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH1192696X 1957-03-05

Publications (1)

Publication Number Publication Date
FR1192696A true FR1192696A (en) 1959-10-28

Family

ID=4562285

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1192696D Expired FR1192696A (en) 1957-03-05 1958-03-05 Axial turbomachine

Country Status (1)

Country Link
FR (1) FR1192696A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1122551B (en) * 1960-05-09 1962-01-25 Sulzer Ag Fastening of austenitic blades in a circumferential groove of a ferritic blade carrier
US3172641A (en) * 1962-11-23 1965-03-09 Allis Chalmers Mfg Co Casing construction
EP0388286A1 (en) * 1989-03-15 1990-09-19 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Blades with hammer-type feet for improved angular positioning
FR2971541A1 (en) * 2011-02-16 2012-08-17 Snecma Device for blocking hammer attachment blade in circumferential groove of wheel disk of e.g. high pressure compressor in aircraft turbojet, has semi-bases occupying radially deployed position to place device in deployed configuration
EP2918784A1 (en) * 2014-03-13 2015-09-16 Siemens Aktiengesellschaft Blade foot for a turbine blade

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1122551B (en) * 1960-05-09 1962-01-25 Sulzer Ag Fastening of austenitic blades in a circumferential groove of a ferritic blade carrier
US3172641A (en) * 1962-11-23 1965-03-09 Allis Chalmers Mfg Co Casing construction
EP0388286A1 (en) * 1989-03-15 1990-09-19 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Blades with hammer-type feet for improved angular positioning
US5044886A (en) * 1989-03-15 1991-09-03 Societe Nationale D'etude Et De Moteurs D'aviation "S.N.E.C.M.A." Rotor blade fixing providing improved angular alignment of said blades
FR2971541A1 (en) * 2011-02-16 2012-08-17 Snecma Device for blocking hammer attachment blade in circumferential groove of wheel disk of e.g. high pressure compressor in aircraft turbojet, has semi-bases occupying radially deployed position to place device in deployed configuration
EP2918784A1 (en) * 2014-03-13 2015-09-16 Siemens Aktiengesellschaft Blade foot for a turbine blade

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