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GB115231A - - Google Patents

Info

Publication number
GB115231A
GB115231A GB636518A GB636518A GB115231A GB 115231 A GB115231 A GB 115231A GB 636518 A GB636518 A GB 636518A GB 636518 A GB636518 A GB 636518A GB 115231 A GB115231 A GB 115231A
Authority
GB
United Kingdom
Prior art keywords
pieces
packing
oesterreichische
turbinen
dampf
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
GB636518A
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 filed Critical
Publication of GB115231A publication Critical patent/GB115231A/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)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Control Of Turbines (AREA)

Abstract

115,231. Oesterreichische Dampf-Turbinen Ges. Feb. 12, 1914, [Convention date]. Blades. - The blade roots f and the packing- pieces t are formed with one or more bends. The bent packing- pieces may be made in one piece or in two, as shown in Fig. 4, and are provided with shoulders z by which they they are held in the groove n of the drum r.
GB636518A 1914-02-12 1918-04-15 Expired GB115231A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
AT76502T 1914-02-12
US493123A US1476626A (en) 1914-02-12 1921-08-17 Means for fastening the blades of steam and gas turbines

Publications (1)

Publication Number Publication Date
GB115231A true GB115231A (en) 1921-01-13

Family

ID=23958992

Family Applications (1)

Application Number Title Priority Date Filing Date
GB636518A Expired GB115231A (en) 1914-02-12 1918-04-15

Country Status (5)

Country Link
US (1) US1476626A (en)
AT (1) AT76502B (en)
DE (1) DE315943C (en)
FR (1) FR516377A (en)
GB (1) GB115231A (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE545574A (en) * 1955-02-26
DE1005530B (en) * 1955-06-23 1957-04-04 Paul Miesbeck Fastening of the rotor blades of centrifugal machines, in particular steam and gas turbines
EP1028231B1 (en) * 1999-02-12 2003-09-03 ALSTOM (Switzerland) Ltd Fastening of turbomachine rotor blades
EP1674734A1 (en) * 2004-12-21 2006-06-28 ALSTOM Technology Ltd Method for improving the flow stability of a turbo compressor
EP2999855A1 (en) * 2013-05-23 2016-03-30 General Electric Company Composite compressor blade and method of assembling

Also Published As

Publication number Publication date
AT76502B (en) 1919-05-26
DE315943C (en) 1919-11-17
US1476626A (en) 1923-12-04
FR516377A (en) 1921-04-18

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