GB315722A - - Google Patents

Info

Publication number
GB315722A
GB315722A GB21878/29A GB2187829A GB315722A GB 315722 A GB315722 A GB 315722A GB 21878/29 A GB21878/29 A GB 21878/29A GB 2187829 A GB2187829 A GB 2187829A GB 315722 A GB315722 A GB 315722A
Authority
GB
United Kingdom
Prior art keywords
blades
offset
assignees
robinson
houston
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
GB21878/29A
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.)
British Thomson Houston Co Ltd
Original Assignee
British Thomson Houston Co Ltd
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 British Thomson Houston Co Ltd filed Critical British Thomson Houston Co Ltd
Publication of GB315722A publication Critical patent/GB315722A/en
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
    • F01D5/12—Blades
    • F01D5/22—Blade-to-blade connections, e.g. for damping vibrations

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

315,722. British Thomson-Houston Co., Ltd., (Assignees of Robinson, E L.). July 16, 1928, [Convention date]. Blades, fixing.- T h e intermediate bracing pieces 4 between the blades 2 of a steam &c. turbine are formed with offset ends which are riveted to the blades. The ends may be offset in the same direction as at 5 or in opposite directions as at 8.
GB21878/29A 1928-07-16 1929-07-16 Expired GB315722A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US315722TA 1928-07-16 1928-07-16

Publications (1)

Publication Number Publication Date
GB315722A true GB315722A (en) 1930-02-27

Family

ID=31945901

Family Applications (1)

Application Number Title Priority Date Filing Date
GB21878/29A Expired GB315722A (en) 1928-07-16 1929-07-16

Country Status (1)

Country Link
GB (1) GB315722A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2772854A (en) * 1951-02-27 1956-12-04 Rateau Soc Vibration damping means for bladings of turbo-machines
US2914299A (en) * 1954-02-05 1959-11-24 Gen Electric Co Ltd Steam turbines
US3045969A (en) * 1958-09-26 1962-07-24 Escher Wyss Ag Vibration damping device for turbo-machine
US3209838A (en) * 1962-08-22 1965-10-05 Ass Elect Ind Turbine rotors
US3708244A (en) * 1970-04-13 1973-01-02 Rolls Royce Bladed rotor for a gas turbine engine
GB2251897A (en) * 1991-01-15 1992-07-22 Rolls Royce Plc Bladed rotor
GB2441543A (en) * 2006-09-07 2008-03-12 Rolls Royce Plc A bridging element for reducing vibrations in an array of elongate components

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2772854A (en) * 1951-02-27 1956-12-04 Rateau Soc Vibration damping means for bladings of turbo-machines
US2914299A (en) * 1954-02-05 1959-11-24 Gen Electric Co Ltd Steam turbines
US3045969A (en) * 1958-09-26 1962-07-24 Escher Wyss Ag Vibration damping device for turbo-machine
US3209838A (en) * 1962-08-22 1965-10-05 Ass Elect Ind Turbine rotors
US3708244A (en) * 1970-04-13 1973-01-02 Rolls Royce Bladed rotor for a gas turbine engine
GB2251897A (en) * 1991-01-15 1992-07-22 Rolls Royce Plc Bladed rotor
GB2251897B (en) * 1991-01-15 1994-11-30 Rolls Royce Plc A rotor
GB2441543A (en) * 2006-09-07 2008-03-12 Rolls Royce Plc A bridging element for reducing vibrations in an array of elongate components
GB2441543B (en) * 2006-09-07 2008-07-23 Rolls Royce Plc An array of components

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