GB811407A - Fabricated blade root - Google Patents

Fabricated blade root

Info

Publication number
GB811407A
GB811407A GB10207/57A GB1020757A GB811407A GB 811407 A GB811407 A GB 811407A GB 10207/57 A GB10207/57 A GB 10207/57A GB 1020757 A GB1020757 A GB 1020757A GB 811407 A GB811407 A GB 811407A
Authority
GB
United Kingdom
Prior art keywords
blocks
blade portion
brazing
blade
lips
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
GB10207/57A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of GB811407A publication Critical patent/GB811407A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • B23P15/04Making specific metal objects by operations not covered by a single other subclass or a group in this subclass turbine or like blades from several pieces

Landscapes

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

Abstract

811,407. Making gas turbine blades; brazing. AVERY, B. A. March 28, 1957 [Aug. 15, 1956], No. 10207/57. Classes 83 (2) and 83 (4). A fabricated turbine blade is made by brazing a pair of root blocks 18, 19 to a blade portion 10 with concave and convex surfaces 21, 23, the blocks having internal surfaces 20, 22 corresponding to the surfaces 21, 23 and shoulders 33 which lie adjacent to each other when the blocks are assembled on a blade portion, and protrusions 31 are provided on the blocks for ensuring a close uniform space between the blade portion and the blocks and thus produce a constant thickness of braze therebetween. The blocks also have lips 32. Side extensions 24 with slots 25 enable the assembly of the blade portion and blocks to be clamped together by bolts 26. The assembly is then brazed in an oven after brazing metal in rod or strip form has been placed on the lips 32. The extensions are finally cut off and the blade root is then milled to fir-tree or other form, Fig. 1 (not shown). Specification 784,196, [Group XXVI], is referred to.
GB10207/57A 1956-08-15 1957-03-28 Fabricated blade root Expired GB811407A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US811407XA 1956-08-15 1956-08-15

Publications (1)

Publication Number Publication Date
GB811407A true GB811407A (en) 1959-04-02

Family

ID=22162336

Family Applications (1)

Application Number Title Priority Date Filing Date
GB10207/57A Expired GB811407A (en) 1956-08-15 1957-03-28 Fabricated blade root

Country Status (1)

Country Link
GB (1) GB811407A (en)

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