GB903792A - Blade and blade mounting assemblies for axial flow turbines, compressors or pumps - Google Patents

Blade and blade mounting assemblies for axial flow turbines, compressors or pumps

Info

Publication number
GB903792A
GB903792A GB116460A GB116460A GB903792A GB 903792 A GB903792 A GB 903792A GB 116460 A GB116460 A GB 116460A GB 116460 A GB116460 A GB 116460A GB 903792 A GB903792 A GB 903792A
Authority
GB
United Kingdom
Prior art keywords
blade
root
part
element
disposed
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
GB116460A
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
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
Priority to CH6851859A priority Critical patent/CH363754A/en
Application filed by Sulzer AG, Gebrueder Sulzer AG filed Critical Sulzer AG
Publication of GB903792A publication Critical patent/GB903792A/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
    • F01D7/00Rotors with blades adjustable in operation; Control thereof
    • 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/70Adjusting of angle of incidence or attack of rotating blades
    • F05D2260/74Adjusting of angle of incidence or attack of rotating blades by turning around an axis perpendicular the rotor centre line
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/70Adjusting of angle of incidence or attack of rotating blades
    • F05D2260/76Adjusting of angle of incidence or attack of rotating blades the adjusting mechanism using auxiliary power sources
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/70Adjusting of angle of incidence or attack of rotating blades
    • F05D2260/79Bearing, support or actuation arrangements therefor

Abstract

903,792. Turbine and compressor blades. SULZER FRERES S.A. Jan. 12, 1960 [Jan. 20, 1959], No. 1164/60. Classes 110 (1) and 110 (3). To provide damping for the oscillation of an axial flow compressor blade, or as shown a turbine blade, a resilient element is disposed between the blade mounting and the root of the blade near the profiled part, the element resiliently supporting the blade from the blade mounting in all directions transverse to the blade axis. The blade 2 is secured to the rotor 1 by a collar 7 and nuts 6 disposed on the root 4 of the blade. Clamped between that part 9 of the root near the profiled part. of the blade and a part 11 of the rotor is an annular resilient element 12 having a U-shaped cross-section. The element 12 may be of steel and may be of double U cross-section or be of a bellows-like cross-section. In the embodiment of Fig. 2, wherein the blade 2 is rotatable about its axis 13, the resilient element comprises a ring of rubber or synthetic plastics and provided with inner and outer binding rings 19, 21. The element is disposed between the part 9 of the root and a ball bearing 17.
GB116460A 1959-01-20 1960-01-12 Blade and blade mounting assemblies for axial flow turbines, compressors or pumps Expired GB903792A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CH6851859A CH363754A (en) 1959-01-20 1959-01-20 Blade attachment at a axial turbomachine

Publications (1)

Publication Number Publication Date
GB903792A true GB903792A (en) 1962-08-22

Family

ID=4528796

Family Applications (1)

Application Number Title Priority Date Filing Date
GB116460A Expired GB903792A (en) 1959-01-20 1960-01-12 Blade and blade mounting assemblies for axial flow turbines, compressors or pumps

Country Status (4)

Country Link
BE (1) BE586646A (en)
CH (1) CH363754A (en)
FR (1) FR1217446A (en)
GB (1) GB903792A (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3984194A (en) * 1974-04-12 1976-10-05 Aktiebolaget Svenska Flaktfabriken Axial flow fans
US4007998A (en) * 1975-08-22 1977-02-15 Carrier Corporation Blade assembly
US4012171A (en) * 1974-04-24 1977-03-15 Suvak Michael N Blade and mounting means
US4579510A (en) * 1983-10-07 1986-04-01 Nordisk Ventilator Co. A/S Axial flow fan impeller
US4606702A (en) * 1985-01-10 1986-08-19 Huber Reversible Fan, Inc. Reversible fan with cylindrical resilient rubber spring
US4934904A (en) * 1989-01-31 1990-06-19 Tcf Axial Division, Inc. Axial fan
US4988303A (en) * 1989-01-23 1991-01-29 Thomas William K Adjustable agitator assembly
GB2418709A (en) * 2004-09-29 2006-04-05 Rolls Royce Plc Damped assembly
GB2511125B (en) * 2013-02-26 2020-01-08 Solyvent Flaekt Ab An axial air movement fan

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3251555A (en) * 1963-03-21 1966-05-17 Aerojet General Co Rocket guidance device
NL123379C (en) * 1963-11-01

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3984194A (en) * 1974-04-12 1976-10-05 Aktiebolaget Svenska Flaktfabriken Axial flow fans
US4012171A (en) * 1974-04-24 1977-03-15 Suvak Michael N Blade and mounting means
US4007998A (en) * 1975-08-22 1977-02-15 Carrier Corporation Blade assembly
US4579510A (en) * 1983-10-07 1986-04-01 Nordisk Ventilator Co. A/S Axial flow fan impeller
US4606702A (en) * 1985-01-10 1986-08-19 Huber Reversible Fan, Inc. Reversible fan with cylindrical resilient rubber spring
US4988303A (en) * 1989-01-23 1991-01-29 Thomas William K Adjustable agitator assembly
US4934904A (en) * 1989-01-31 1990-06-19 Tcf Axial Division, Inc. Axial fan
GB2418709A (en) * 2004-09-29 2006-04-05 Rolls Royce Plc Damped assembly
GB2418709B (en) * 2004-09-29 2007-10-10 Rolls Royce Plc Damped assembly
GB2511125B (en) * 2013-02-26 2020-01-08 Solyvent Flaekt Ab An axial air movement fan

Also Published As

Publication number Publication date
BE586646A1 (en)
BE586646A (en) 1960-07-18
FR1217446A (en) 1960-05-03
CH363754A (en) 1962-08-15

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