GB1064400A - Welded turbine or compressor rotor - Google Patents

Welded turbine or compressor rotor

Info

Publication number
GB1064400A
GB1064400A GB5275064A GB5275064A GB1064400A GB 1064400 A GB1064400 A GB 1064400A GB 5275064 A GB5275064 A GB 5275064A GB 5275064 A GB5275064 A GB 5275064A GB 1064400 A GB1064400 A GB 1064400A
Authority
GB
United Kingdom
Prior art keywords
platforms
blades
dec
turbine
welded
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
GB5275064A
Inventor
Anthony Eugene Martin
Robert Noel Penny
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.)
Rover Co Ltd
Original Assignee
Rover 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 Rover Co Ltd filed Critical Rover Co Ltd
Priority to GB5275064A priority Critical patent/GB1064400A/en
Publication of GB1064400A publication Critical patent/GB1064400A/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
    • F01D5/3061Fixing blades to rotors; Blade roots ; Blade spacers by welding, brazing

Abstract

1,064,400. Making turbine blades; welding by fusion. ROVER CO. Ltd. Dec. 22, 1965 [Dec. 30, 1964], No. 52750/64. Headings B3A and B3R. [Also in Division F1] In a composite rotor for a turbine or compressor, platforms 2 each carrying one blade or a group of blades are welded to the periphery of the rotor disc 1 by at least one annular weld produced by electron beam welding. The blades and platforms are made from a different material to the disc, the former being, e.g., of a casting alloy and the latter of a material having good ductility and strength. In the embodiment shown two annular welds are prevented from overlapping and providing a weak double weld, by a buffer cavity 8 in accordance with Specification 1,064,399. Adjacent platforms may abut and be welded together or be spaced apart and the spaces filled with a suitable material.
GB5275064A 1964-12-30 1964-12-30 Welded turbine or compressor rotor Expired GB1064400A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB5275064A GB1064400A (en) 1964-12-30 1964-12-30 Welded turbine or compressor rotor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB5275064A GB1064400A (en) 1964-12-30 1964-12-30 Welded turbine or compressor rotor

Publications (1)

Publication Number Publication Date
GB1064400A true GB1064400A (en) 1967-04-05

Family

ID=10465146

Family Applications (1)

Application Number Title Priority Date Filing Date
GB5275064A Expired GB1064400A (en) 1964-12-30 1964-12-30 Welded turbine or compressor rotor

Country Status (1)

Country Link
GB (1) GB1064400A (en)

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