GB749997A - Process and apparatus for making turbine or compressor blades - Google Patents

Process and apparatus for making turbine or compressor blades

Info

Publication number
GB749997A
GB749997A GB1752352A GB1752352A GB749997A GB 749997 A GB749997 A GB 749997A GB 1752352 A GB1752352 A GB 1752352A GB 1752352 A GB1752352 A GB 1752352A GB 749997 A GB749997 A GB 749997A
Authority
GB
United Kingdom
Prior art keywords
strip
rolls
rolling
blade
blades
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
GB1752352A
Inventor
William Stephen Hollis
John Owen Mayer
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.)
Power Jets Research and Development Ltd
Original Assignee
Power Jets Research and Development 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 Power Jets Research and Development Ltd filed Critical Power Jets Research and Development Ltd
Priority to GB1752352A priority Critical patent/GB749997A/en
Priority to US366998A priority patent/US2972181A/en
Priority to FR1083734D priority patent/FR1083734A/en
Priority to DE1953P0010083 priority patent/DE1051615C2/en
Priority to CH319306D priority patent/CH319306A/en
Publication of GB749997A publication Critical patent/GB749997A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21HMAKING PARTICULAR METAL OBJECTS BY ROLLING, e.g. SCREWS, WHEELS, RINGS, BARRELS, BALLS
    • B21H7/00Making articles not provided for in the preceding groups, e.g. agricultural tools, dinner forks, knives, spoons
    • B21H7/16Making articles not provided for in the preceding groups, e.g. agricultural tools, dinner forks, knives, spoons turbine blades; compressor blades; propeller blades
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21KMAKING FORGED OR PRESSED METAL PRODUCTS, e.g. HORSE-SHOES, RIVETS, BOLTS OR WHEELS
    • B21K3/00Making engine or like machine parts not covered by sub-groups of B21K1/00; Making propellers or the like
    • B21K3/04Making engine or like machine parts not covered by sub-groups of B21K1/00; Making propellers or the like blades, e.g. for turbines; Upsetting of blade roots
    • 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
    • B23P15/02Making specific metal objects by operations not covered by a single other subclass or a group in this subclass turbine or like blades from one piece
    • 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
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/147Construction, i.e. structural features, e.g. of weight-saving hollow blades

Abstract

749,997. Making turbine and compressor blades. POWER JETS (RESEARCH & DEVELOPMENT), Ltd. July 13, 1953 [July 11, 1952; June 4, 1953], Nos. 17523/52 and 15405/53. Classes 83 (2) and 83 (4). [Also in Group XXVI] Turbine or compressor blades are made by upsetting on a strip 1 evenly spaced enlargements 2 for the blade roots, and then passing the blanks so formed, as a continuous length or as individual blade blanks, through bladeforming rolls. A length of circular section material is flattened by rolling to form the flat strip 1, Fig. 1. If the finished blades are tapered along their length, rotary swaging of the strip is carried out, preferably before flattening, to produce a strip having a succession of portions tapering from maximum to minimum width or diameter. The strip is then passed through an electrical upsetting machine, Figs. 1, 4, from which it passes through the rolls, Fig. 2. The rolls may finish the blade portion and root or they may be machined to final shape after rolling. As the blades leave the rolls they are parted off by a rotary slitting tool which travels with the moving strip. The blades are then twisted. Alternatively the blade blanks may be parted off from the strip before rolling or before the last stage of a multi-stage rolling operation especially when blade twist is to be imparted during rolling. The blades 4, Fig. 5, may have roots of fir-tree form 3a, of bulbous form 3b or of dove-tailed form 3d, Fig. 3 (not shown). In the latter case the dovetailed enlargement may form only part of the root and may fit into a dovetailed groove in a block which completes the root. Alternatively two blocks may be provided, one on each side of the enlargement. The blades are mounted in seatings 46a, 46b or 46c which are broached or milled in a stator or rotor ring 46. The bulbous root 3c has flats 3m, 3n which seat against corresponding flats in its seating 46c to prevent relative angular movement. The bulbous root 3b is secured in its seating by a key 47 which locates the root rigidly or with a slight clearance to allow a slight angular movement of blade in its seating. Upsetting.-The upsetting machine of Fig. 1, comprises a pair of vices 5, 6, having viceblocks 7, 8, respectively closable by hydraulic actuators 9, 10 respectively and connected across the secondary of a transformer 13. The strip which passes through cavities 7a, 8a in the vice blocks, is gripped thereby and the vice blocks are then moved together to upset the strip therebetween. Recesses such as 8b in the adjacent surfaces of the vice blocks form a radius where the upset merges with the strip. The upsetting may be formed as a step-by-step operation or preferably as a continuous operation. For performing the latter the vices are mounted on platforms 15, 16 respectively slidable along guides 17. Platform 15 is connected by rods 24 to small-throw cranks 22 on a crankshaft 20 driven continuously by gearing 21. Platform 16 is connected by rods 25 to largethrow cranks 23. The vices are thus moved in the same direction but due to the differences in throw of the cranks, are brought together and separated in alternate sequence. High-frequency induction heating may be used instead of resistance heating. Upsetting and rolling.-Instead of the machine of Fig. 1, the strip 1 may be upset by passing it through rolls 30, 31, Fig. 4, having recesses 30b, 31b which indent the strip across its width at spaced intervals, and shoulders 30a, 31a which form abutments for the strip whilst it is upset by a vice 33 moved along guides 36 by an hydraulic actuator 35. The strip is heated electrically by a high-frequency induction heater 39, or alternatively by resistance heating. In the latter case the rolls and the vice serve as the two electrodes. Circular section stock may be passed through these rolls and be flattened thereby besides being upset. Rolling. The strip 1 with the spaced upsets 2 is then passed through the blade-forming rolls 41, 42, Fig. 2, driven by gearing 43. These rolls have peripheral recesses 41a, 42a, which form the blade portion, and recesses 41b, 42b which form the root portion. The recesses may be tapered to produce blades with tapering chord and thickness and the recesses may also impart blade twist. These recesses may be provided by removable die inserts. The rolling may be performed cold or preferably hot, in which case the strip passes through a highfrequency induction heater 44. Alternatively resistance heating may be used. More than one pair of rolls may be used in which case the rolling is performed in stages and the strip may be reheated between adjacent rolls. Specifications 619,634, 648,783 and 660,282 also are referred to.
GB1752352A 1952-07-11 1952-07-11 Process and apparatus for making turbine or compressor blades Expired GB749997A (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
GB1752352A GB749997A (en) 1952-07-11 1952-07-11 Process and apparatus for making turbine or compressor blades
US366998A US2972181A (en) 1952-07-11 1953-07-09 Process for making turbine blades
FR1083734D FR1083734A (en) 1952-07-11 1953-07-10 Improvements in processes for manufacturing turbine blades and the like
DE1953P0010083 DE1051615C2 (en) 1952-07-11 1953-07-10 Device for manufacturing turbine or compressor blades
CH319306D CH319306A (en) 1952-07-11 1953-07-11 Process and device for the production of blades for axially loaded turbomachines

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB1752352A GB749997A (en) 1952-07-11 1952-07-11 Process and apparatus for making turbine or compressor blades
GB1540553 1953-06-04

Publications (1)

Publication Number Publication Date
GB749997A true GB749997A (en) 1956-06-06

Family

ID=46724174

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1752352A Expired GB749997A (en) 1952-07-11 1952-07-11 Process and apparatus for making turbine or compressor blades

Country Status (1)

Country Link
GB (1) GB749997A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5191711A (en) * 1991-12-23 1993-03-09 Allied-Signal Inc. Compressor or turbine blade manufacture

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5191711A (en) * 1991-12-23 1993-03-09 Allied-Signal Inc. Compressor or turbine blade manufacture

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