GB374383A - Improvements in turbine blades - Google Patents

Improvements in turbine blades

Info

Publication number
GB374383A
GB374383A GB587/32A GB58732A GB374383A GB 374383 A GB374383 A GB 374383A GB 587/32 A GB587/32 A GB 587/32A GB 58732 A GB58732 A GB 58732A GB 374383 A GB374383 A GB 374383A
Authority
GB
United Kingdom
Prior art keywords
core
rotor
welded
blade
cores
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
GB587/32A
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
BBC Brown Boveri France SA
Original Assignee
Brown Boveri und Cie AG Germany
BBC Brown Boveri France SA
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, BBC Brown Boveri France SA filed Critical Brown Boveri und Cie AG Germany
Publication of GB374383A publication Critical patent/GB374383A/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

Landscapes

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

Abstract

374,383. Turbine blades. AKT.- GES. BROWN, BOVERI, ET CIE, Baden, Switzerland. Jan. 8, 1932, No. 587. Convention date, Jan. 19, 1931. [Class 110 (iii).] A gas turbine blade consists of a cooled core rigidly connected to the rotor, and an uncooled sheath which is slipped over the core and forms the blade proper. In Fig. 1 the cores 1 are machined out of the rim of the rotor 2, the cooling water channels 3 being stopped by plugs 4 which may be welded to the shrouding band 7. The blade forming sheaths 6, which are slipped over the cores, are retained in position by the band 7. In the modification shown in Figs. 4 and 5, the core 8 is screwed into the rotor 9 and welded at 10. The blade forming sheath 12 may be welded to the core at the bottom or at the top.
GB587/32A 1931-01-19 1932-01-08 Improvements in turbine blades Expired GB374383A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE374383X 1931-01-19

Publications (1)

Publication Number Publication Date
GB374383A true GB374383A (en) 1932-06-09

Family

ID=6343447

Family Applications (1)

Application Number Title Priority Date Filing Date
GB587/32A Expired GB374383A (en) 1931-01-19 1932-01-08 Improvements in turbine blades

Country Status (1)

Country Link
GB (1) GB374383A (en)

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