GB169913A - Improvements in and relating to methods of making blade rings for elastic-fluid turbines - Google Patents

Improvements in and relating to methods of making blade rings for elastic-fluid turbines

Info

Publication number
GB169913A
GB169913A GB3002720A GB3002720A GB169913A GB 169913 A GB169913 A GB 169913A GB 3002720 A GB3002720 A GB 3002720A GB 3002720 A GB3002720 A GB 3002720A GB 169913 A GB169913 A GB 169913A
Authority
GB
United Kingdom
Prior art keywords
blades
relating
elastic
methods
blade rings
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
GB3002720A
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Priority to GB3002720A priority Critical patent/GB169913A/en
Publication of GB169913A publication Critical patent/GB169913A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • B23P15/006—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass turbine wheels

Landscapes

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

Abstract

169,913. British Thomson - - Houston Co., Ltd., (General Electric Co.). Oct. 23, 1920. Blades have blocks 6 at both ends which fit in and completely fill grooves 8 in the blade rings. The blocks are formed integrally with the blade portions, preferably by upsetting the ends of straight blade stock. The blades may be held in place initially by tightness of fit or by spot welding and when all the blades are assembled, the whole is permanently united by brazing, soldering or the like. The structure may be subsequently machined and may have a suitable groove 9 for an expansion ring attachment to the rotor.
GB3002720A 1920-10-23 1920-10-23 Improvements in and relating to methods of making blade rings for elastic-fluid turbines Expired GB169913A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3002720A GB169913A (en) 1920-10-23 1920-10-23 Improvements in and relating to methods of making blade rings for elastic-fluid turbines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3002720A GB169913A (en) 1920-10-23 1920-10-23 Improvements in and relating to methods of making blade rings for elastic-fluid turbines

Publications (1)

Publication Number Publication Date
GB169913A true GB169913A (en) 1921-10-13

Family

ID=10301080

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3002720A Expired GB169913A (en) 1920-10-23 1920-10-23 Improvements in and relating to methods of making blade rings for elastic-fluid turbines

Country Status (1)

Country Link
GB (1) GB169913A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2681500A (en) * 1949-07-18 1954-06-22 Bristol Aeroplane Co Ltd Method of manufacturing turbine or the like blades

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2681500A (en) * 1949-07-18 1954-06-22 Bristol Aeroplane Co Ltd Method of manufacturing turbine or the like blades

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