CH488939A - Bucket for turbo machinery - Google Patents

Bucket for turbo machinery

Info

Publication number
CH488939A
CH488939A CH446168A CH446168A CH488939A CH 488939 A CH488939 A CH 488939A CH 446168 A CH446168 A CH 446168A CH 446168 A CH446168 A CH 446168A CH 488939 A CH488939 A CH 488939A
Authority
CH
Switzerland
Prior art keywords
bucket
turbo machinery
turbo
machinery
Prior art date
Application number
CH446168A
Other languages
German (de)
Inventor
Ferdinand Dipl Ing Zerlauth
Original Assignee
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 filed Critical Sulzer Ag
Priority to CH446168A priority Critical patent/CH488939A/en
Priority to NL6805582A priority patent/NL6805582A/xx
Priority to US759111A priority patent/US3521974A/en
Priority to FR6906019A priority patent/FR2004710A1/fr
Priority to GB04991/69A priority patent/GB1192159A/en
Priority to BE730456D priority patent/BE730456A/xx
Publication of CH488939A publication Critical patent/CH488939A/en

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
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S416/00Fluid reaction surfaces, i.e. impellers
    • Y10S416/50Vibration damping features

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
CH446168A 1968-03-26 1968-03-26 Bucket for turbo machinery CH488939A (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
CH446168A CH488939A (en) 1968-03-26 1968-03-26 Bucket for turbo machinery
NL6805582A NL6805582A (en) 1968-03-26 1968-04-19
US759111A US3521974A (en) 1968-03-26 1968-09-11 Turbine blade construction
FR6906019A FR2004710A1 (en) 1968-03-26 1969-03-05
GB04991/69A GB1192159A (en) 1968-03-26 1969-03-21 Blades for Turbomachines
BE730456D BE730456A (en) 1968-03-26 1969-03-26

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH446168A CH488939A (en) 1968-03-26 1968-03-26 Bucket for turbo machinery

Publications (1)

Publication Number Publication Date
CH488939A true CH488939A (en) 1970-04-15

Family

ID=4276544

Family Applications (1)

Application Number Title Priority Date Filing Date
CH446168A CH488939A (en) 1968-03-26 1968-03-26 Bucket for turbo machinery

Country Status (6)

Country Link
US (1) US3521974A (en)
BE (1) BE730456A (en)
CH (1) CH488939A (en)
FR (1) FR2004710A1 (en)
GB (1) GB1192159A (en)
NL (1) NL6805582A (en)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4012171A (en) * 1974-04-24 1977-03-15 Suvak Michael N Blade and mounting means
US4245954A (en) * 1978-12-01 1981-01-20 Westinghouse Electric Corp. Ceramic turbine stator vane and shroud support
GB2234299B (en) * 1989-07-06 1994-01-05 Rolls Royce Plc Mounting system for engine components having dissimilar coefficients of thermal expansion
GB2278647B (en) * 1990-12-27 1995-04-05 Snecma Method of fixing flow-straightening blades in a turboshaft engine
FR2671133B1 (en) * 1990-12-27 1994-10-21 Snecma RAPIDLY FIXED PIVOT BLADE FOR TURBOMACHINE RECTIFIER BLADE AND METHOD FOR FIXING SAID BLADE.
US6435821B1 (en) * 2000-12-20 2002-08-20 United Technologies Corporation Variable vane for use in turbo machines
US8092165B2 (en) * 2008-01-21 2012-01-10 Pratt & Whitney Canada Corp. HP segment vanes
US8894370B2 (en) * 2008-04-04 2014-11-25 General Electric Company Turbine blade retention system and method
IT1393757B1 (en) * 2008-07-28 2012-05-08 Ansaldo Energia Spa CONNECTION GROUP TO CONNECT A PALLET TO A SUPPORT RING, IN PARTICULAR TO AN INTERNAL RING OF A COMPRESSOR STATOR
US8485784B2 (en) * 2009-07-14 2013-07-16 General Electric Company Turbine bucket lockwire rotation prevention
DE102009047006A1 (en) * 2009-11-23 2011-05-26 Robert Bosch Gmbh charging
BE1023290B1 (en) * 2015-07-22 2017-01-24 Safran Aero Boosters S.A. AUBE COMPOSITE COMPRESSOR OF AXIAL TURBOMACHINE
FR3127533A1 (en) * 2021-09-28 2023-03-31 Safran Aircraft Engines Wedging system for articulated turbomachine blade, turbomachine blade equipped with this wedging system and method of mounting such wedging system on an articulated blade

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE724793C (en) * 1940-04-16 1942-09-05 Sulzer Ag Conveyor machine with mainly axially acting blades
US2955799A (en) * 1957-02-11 1960-10-11 United Aircraft Corp Blade damping means

Also Published As

Publication number Publication date
GB1192159A (en) 1970-05-20
BE730456A (en) 1969-09-26
NL6805582A (en) 1969-09-30
US3521974A (en) 1970-07-28
FR2004710A1 (en) 1969-11-28

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Legal Events

Date Code Title Description
PL Patent ceased