GB329261A - - Google Patents

Info

Publication number
GB329261A
GB329261A GB34104/29A GB3410429A GB329261A GB 329261 A GB329261 A GB 329261A GB 34104/29 A GB34104/29 A GB 34104/29A GB 3410429 A GB3410429 A GB 3410429A GB 329261 A GB329261 A GB 329261A
Authority
GB
United Kingdom
Prior art keywords
blades
spaces
boveri
shrouded
ges
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
GB34104/29A
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.)
BBC Brown Boveri AG Germany
Original Assignee
Brown Boveri und Cie AG Germany
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 Brown Boveri und Cie AG Germany filed Critical Brown Boveri und Cie AG Germany
Publication of GB329261A publication Critical patent/GB329261A/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
    • F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers

Landscapes

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

Abstract

329,261. Akt.-Ges. Brown, Boveri, et Cie. Nov. 30, 1928, [Convention date]. Rotors.- In order to obtain a constant flow of heat through a turbine disc a, the rim is provided with hollow spaces f between the blades. The spaces may be shrouded by members g arranged between the blades, or by extensions h on the blades.
GB34104/29A 1928-11-30 1929-11-08 Expired GB329261A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE329261T 1928-11-30

Publications (1)

Publication Number Publication Date
GB329261A true GB329261A (en) 1930-05-15

Family

ID=31894850

Family Applications (1)

Application Number Title Priority Date Filing Date
GB34104/29A Expired GB329261A (en) 1928-11-30 1929-11-08

Country Status (1)

Country Link
GB (1) GB329261A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2660400A (en) * 1948-11-25 1953-11-24 Rolls Royce Blade for turbines or compressors
US3294365A (en) * 1964-12-02 1966-12-27 Rolls Royce Blade for use in a fluid-flow machine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2660400A (en) * 1948-11-25 1953-11-24 Rolls Royce Blade for turbines or compressors
US3294365A (en) * 1964-12-02 1966-12-27 Rolls Royce Blade for use in a fluid-flow machine

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