US1021472A

US1021472A - Blading for turbines.

Info

Publication number: US1021472A
Application number: US38009407A
Authority: US
Inventors: James Walter Wilson; John Ford
Original assignee: Individual
Current assignee: Individual
Priority date: 1907-06-21
Filing date: 1907-06-21
Publication date: 1912-03-26
Anticipated expiration: 1929-03-26

Description

C, A. PARSONS, J. W. WILSON 6L FORD. BLADING FOR TURBINBS. 'i

APPLIOATION FILED JUNE 21, 1907.

1,021,4721 Patented Mar. 26, 1912. v

2 SHEETS-SHEET 1.

f Wig" 10 .Charles .Pw-

c. A. PARSONS, J. W. WILSON 11;' J. P01111. BLADING POR TURBINBS.

APPLICATION FILED JUNE 21, 1907.

Patented' 111211.26, 1912.

2 SHEETS-SHEET 2.

111g. 1v w n `'sin/rifas PATENT orrion.

CHARLES ALGERNON PARSONS AND JAMES WALTER WILSON, OF NWCASTLE-UPON- 4 I TYNE, AND JOHN FORD, OF WALLSEND, ENGLAND; SAID WILSON .ANDI'ORD AS-j SIGNORS TO SAID PARSONS.

BLADING FOB TURIBINES.

Application led Iiin 21,'1907. Serial No. 380,094.

To all whom t may concern.' Y f Be it `known that we, CHARLES ALGERNON PAiisoNs, J Aims WALTER WILSON, andvJoHN FORD, subjects of the King of Great Britain and Ireland, residing the two former at Heaton W'orks, Newcastle upon Tyne, v in the county of Northumberland, -England, and the latter at Turbinia Works, Wallsend, Northumberland county, England, have invented certain new and useful. Improvements in and Relating to Bladings for Turbines, Compressors, and the Like, of which the following is a specification.l V

This invention relates to improvements in bladingv for turbines, turbo-compressorsv and the like.

The object of this invention is to effect improvements in the assemblage of'blades in segments, complete rings orV in plain straight lengths in' such a manner that the assembled port-ions are' ready for application in the grooves, ofthe casing and rotor of turbines or turbo-compressors, with or ing the blades and. packing pieces over al wire or strip of suitable section, a tube or the like, the blades and distance pieces being then driven one or more at a time, tightly and solidly against each other on a former which prevents the metal from flowing latrally whereby the distance pieces and blades are tightened firmly upon lthe binding wire, strip' or tube and are consequently held together in a. manner which permits of transference to the turbine or the store as a bladed ring, segment or strip on removal from the former.

The invention further consists in assembled turbine blading strips in which the roots of the blades and their distance p-ieces firmly grip a wire, metallic strip or the like serving to hold the blades together so that they may be transferred after calking or the blades.

ystead of a wire,` the lstrip bein Patented MarZ, 1.912. ,l

Istaving u as a se ment, complete ring or comparatively ilexi le strip' into lthe groove j,

or drum of the turbine casing.

The inventionfurther consists in serrat' the strip through milling rollers of suitable form.

The invention further consists in forming the blade or the distance pieces with one or more projections and recesses engaging with each other, or in providing the distance pieces with slots or saw-cuts or stamped pro- ]ections and recesses, into which said portions of adjacent blades are to enter, the blades and distance'pieces being consolidated on a former with the'holding wire or strip above referred to and giving a mutual chain grippbetween the blades and sections.

The invention further .consists in the blade segments, rings or strips hereinafter' described.

Referring now to the accompanying drawings which illustrate various waysof carrying the invention into effect and form part of the specification, Figure 1 is an elevat-ion of .a -segment of blades on a binding Wire passing through holes in theroots of Fig. 2 is a bottom View of the same. Fig. 3 is an elevation of the root of one of the blades shown in Fig. l, and Fig. 4 is a similar view of a corresponding distanceA 'calking piece. 5 is an elevat-ion of a part of a bladed segment or straight length of blades in which al strip is used ininserted in slots cut-in ,the bottom of the distance pieces andblades. Figs 6 and 7 arevsectional elevation and bottom view respectively of Fig. 5. Figs. 8, 9 and 10 are side and end elevations and plan respectively of a modilication in which the strip is in the side ofthe distance pieces-and blades. Fig. l1 is a1 sectional view showing a form of serrated strip. Figs.12

and 13 are elevation and sectional plan respectively of the blade roots and distance pieces showing a device in which projections are formed on the blades and holes in the distance pieces. Figs. 14 and 15 are similar views to Figs. 12 and 13 of a modiiication in Whichprojections are formed on the distance pieces .and holes or slots in the blades. Figs. 16y and 17 are elevation and cross sectional views of a part of a former, in Which the calking is effected to consolidate the blades and interlocking links or pieces to form a bladed strip segment or the like.

`In carrying the invention into effect according to the manner illustrated With reference to Figs. 1 to 4, ordinary turbine or compressorblades, a, and packing sections or distance pieces,` Z, suchas those described for example in Parsons English Pat-ent No. 8698 of 1906 are drilled at about their centers. Through the holes, c, in the blades and distance pieces a Wire, d, is threaded. The blades and distance piecesv are placed in the groove, e, of a former, g, such as that shown in Figs. 16 and 17, and by a suitable calking tool, f, are driven up solidly and tightly one or more at a time. The groove, e, in the former is lslightly narrower than the groove in the turbine or compressor drum or casing and the stemming up action of the calking tool not only forces the blades and distance pieces into intimate contact f with each other but also tightens the pieces and blades solidly upon the binding Wire, the Walls of the former preventing lateral flow of the metal during the operation. One side of the groove of the former is provided With a removable flange, h, held firmly by strong bolts, z', distance packing, j, being interposed to allow adjustability of the Width of the groove of the former t0 suit various desired Widths of bladed strips. If desired the terminal blades of the assembled strips or segment may be soldered or otherwise treated to insure their solidity before insertion in the groove of the turbine. Instead of using a solid Wire such as that shown at d, in Figs. 1 to 4, 'a tube may be used, or as shown in Figs. 5 and 6, the distance pieces and the roots may have slots cut in their bottoms 'into which a strip, 7c, is pressed. The strip is preferably slightly fWedge-shaped While the sldes of the slots in ffthe blades and distance pieces are parallel. The assembling of the blades and distance pieces is done in the vformer groove When the Wedge shaped strip imparts a slightly dovetailed shape to the distance pieces and blade roots. The `connecting strip may be serrated as shown in Fig. 11 to increase its hold; When staved up as above described, the blades and distance pieces firmly grip the strip, k, 4which thus acts as an interconnectingl means and binds them 4all together as asegment, straight length or ring of blades. Slmilarly the Wire when used .5 may be serrated, roughened or iluted Afor i the same purpose. A side strip, m, (Figs.

8, 9 and 10) may be used instead of a bottom strip.

In cases where the blade is formed with an enlarged root integral with' the blade, one 0r more holes or slot/s may be formed in it for the purposes above indicated.

When the assembled blades are on the former their tips may be shrouded With any convenient devlces or in any suitable manner, as-shoWn for example at a, in Fig. 1.

The segments, rings or strip lengths When transferred to their grooves on the drum or casing, may be secured therein in any convenient manner With or Without calking strips.y The manner of fixing described in English Patent No. 8698 of 1906 may be convenient-ly adopted. holding strip is employed on both sides of the blade roots or a plurality of strips may be used in the bottom or sides of the distance pieces land blades.

Ina further modification of the invention shown in Figs. 12 and 13, projections, t, are formed on the blades by punching them partially through or by other means, the distance pieces being provided with corresponding recesses so that When the blades and distance 'pieces are .driven together on the former, projections on the one enter the recesses on ,the other so that the Whole is consolidated.

The distance pieces may in some cases (Figs. 14 and 1-5) be provided with projections, u, engaging in corresponding recesses or slots in the blades. When consolidated on a former, the blades make a strip, segment or ring which may be transferred Without displacement to the turbine carrying member and then be secured in position inthe groove by any convenient means. A strip, k, or a Wire or tube is preferably used i in dies before or after being cut 0H from the rod of suitable form or they may be other- Wise formed in any Well known manner by p pressing. These means of forming strips In some cases a' -in conjunction with the projection and reor segments may be used independently of-` or in combination with the connecting Wire, strip or tube before described.

To insure accuracy and reliability of the operations of forming the holes or slots, jigs with suitable attachments 'are employed. Jigs and blocks carrying the sections can be arranged either singly or in multiple-and may be arranged horizontally or vertically or any desired angle to the drilling or shaping machines which are preferably high speed sensitive tools. Suitable feeding attachments are arranged so that the sections to bevdealtgor shaped are automatically fed forward to the tool. Ramming of thedistance'pieces and blades in the former may be effected by means of groovedv calking tools or by hydraulic or pneumatica-ily operated means.

Hitherto in strips or the like of blades ready for insertion in the groove of the turbine member it has been usual to make the element which connects the blades 'and holds them in consolidated form, of a Width which is at leastequal to the Width of the blade measured parallel to the axis of rotation of the turbo machine shaft. According to the present invention however the piece or pieces which effect the actual connection'of the sepa rate distance pieces and blades before they are inserted in strip form into the turbine groove consists Ior consist of pieces of m'etal which are of much less Width than the blade root measured as above indicated and which are of very small cross sectional area in relat-ion to the cross sectional area. of the part of the strip which is gripped in vthe groove. In Figs. 1 to 11 the connecting means consists of the `vire like connectors, d, In, and m; in Figs. 12, 13 and 14 the connectingmeans consists of the tongues, n, p, and s; in Figs. 15, 16, 17 and 18 the connecting means consists of wire like connecting means, le, together with projections t and u.

Having now described our invention what lWe claim as new and desire to `secure by Letters Patent is 1. A substantially flexible bladed strip ready for insertion in a ,turbo-machine groove comprising blades, separate dlstance pieces and substantially flexible connecting means consolidated therewith. y l

:'2. A substantially flexible bladed strip ready for insertion in a vturbo-machine groove comprising blades, separate distance pieces and substantially flexible connecting solidated.l 6. A substantially flexible bladed strlp 65 y pieces.

means continuous of--a plurality of said blades and distance pieces consolidated therewith.

3. A substantially flexible bladed strip pieces.

4. A substantially flexible bladed `strip rea-dy for lnsertion 1n a turbo-machine groove comprismg blades, separate distance,

pieces and Wire like connecting means passedinto openings in the distance pieces and blades, the whole being consolidated.

5. A substantially flexible bladed strip readyfor insertion in a turbo-imlchine groove comprising blades, separate distance pieces and round metallic wire like connecting lneans passed into holes 1n thel d1s. v tance pieces and blades. the whole being conreadyy for insertion in a turbo-nmehine groove comprising blades, separate distance pieces and a metallic connecting wire consolidated with said blades and distance 7. A substantially flexible bladed Istrip ready for lnsertion in a turbo-niaclnne ,f rroore comprising blades,- separate distance pieces and a metallic connecting Wire passed into holes in said distance pieces and croots 75 ofsaid blades and consolidated therewith.

In testimony Whereof,we atlix our signatures in presence of two witnesses.

CHAR-LES ALGERNON PARSONS. i JAMES WALTER, WILSON'. JOHN FORD. lVitnesses HENRY GRAHAM Dxiirxs. Jr., -FREDER1GK GonDoN HAY BEDFORD.

said blades and distance 50