US3263670A

US3263670A - Wafering machine

Info

Publication number: US3263670A
Authority: US
Inventors: Thomas D Bushman; George J Seymour
Original assignee: Norton Co
Current assignee: Saint Gobain Abrasives Inc
Priority date: 1962-05-14
Filing date: 1964-11-19
Publication date: 1966-08-02
Anticipated expiration: 1983-08-02

Description

Aug. 2, 1966 T. D. BUSHMAN ETAL WAFERING -lvmcHINE 2 sheets-sheet 1 Original Filed May 14, 1962 INVENTORS. F10/WAS D. BUSHMAN GEORGE J" SEV owe ATToe/VEY Aug. 2, 1966 '1'. D. Busi-:MAN ETAL 3,263,670

WAFERING MACHINE 2 Sheets-Sheet 2 Original Filed May 14, 1962 INVENTORS 'f7/@MAS D. Bus/#MAN G50/fees J SEYMOUR ,1 a 7 /7 l 4 v Y w wb/712% f' ATTORNEY 'I Mmom rw, /7 4 5 7 3 M .g H Z F 4 ,h

United States Patent O 3,263,670 WAFERING MACHINE Thomas D. Bushman, Holden, and George J. Seymour, Leicester, Mass., assignors to Norton Company, Worcester, Mass., a corporation of Massachusetts Original application May 14, 1962, Ser. No. 194,356, now Patent No. 3,168,087, dated Feb. 2,` 1965. Divided and this application Nov. 19, 1964, Ser. No. 412,419 4 Claims. (Cl. 12S- 16) This application is a divisie-n of application Serial No. 194,356, led May 14, 1962, and now Patent No. 3,168,087, dated February 2, 1965.

The instant invention relates to improvements `in wafering machines for cutting hard materials such as quartz, silicon, germanium and the like, and more particularly to improvements in the blade head assembly for` such` wafering machines including the provision of anintegrated blade package including multiple blades adhered to intervening spacers.

While there are various types of watering machines for cutting hard materials including machines arranged to be provided with a diamond wheel with a peripheral cutting edge and machines arranged to be provided. with an annular diamond blade with an internal cutting edge, this application relates particularly to the type of wafering machine which may be described as a multiple` blade power hacksaw, characterized by a reciprocating` blade head assembly supporting a large number of closely spaced parallel blades. j

In one embodiment descri-bed and illustrated in Patent No. 3,079,908, dated March 5, 1963,0f Grover C. Hunt, the last named type of waferingmachine comprises a base supporting a spaced pair of ways generally disposed in a horizontal plane and arranged to slidably support a blade head assembly for reciprocation by a suitable drive motor. This blade head assembly consists of a generally rectangular frame` connected to and supported by members shaped and disposed for engagement with. the spaced parallel ways mounted on the base of the machine and in turn is arranged to support and tension a large plurality of closely spaced parallel blades comprising elongated sections of thi-n strip material and disposed in a, horizontal plane` for reciprocation in engagementl with an` ingot of hard material forced upwardly against the blades by suitable biasing means such as a lever pivotally mounted intermediate its ends for rotation about a horizontal axis and arranged to support the hardmaterial to be cut at one end thereof and an adjustable weightjat the. other end thereof.

The instant invention contemplates improvements in the fblade head assembly of watering machines of the type which may be described as multiple blade power hacksaws which derive from the incorporation in the blade head assembly of an integrated multiple blade package.

An object of this invention is the provision of a` blade head assembly for a wafering machine characterized by provision for the rapid installation o-f a large multiplicity of blades therein in a precisely controlled spaced parallel relationship.

Another object is the provision of a blade head assembly for a wafen'ng machine arranged to support a multiplicity of blades selectively in a first position to present a first series of working edges to a work piece and in a second position to present a second series of working edges to a work piece.

Yet another object is the provision of integrated blade packages for incorporation in the blade head assembly of a wafering machine so arranged that these blade packages may tbe mounted` in the blade` head assembly first in one working position and then in another working position in order to use a first series of blade working edges and ICC theny a-second series of blade working edges before each blade package isV replaced.

Other objects and advantages of the instant invention will be apparent from consideration o-f the following description inrelation tothe showing in the accompanying drawings wherein:

FIG. l i-s-a three dimensional view of a representative blade package fabricated according to the teachings of the instant invention,

FIG. 2 is a side elevation of a reversibleblade package fabricated according to the teachings of the instant invention` indicating in. dot-dash. lines the manner in which the respective working edges of each blade.` are worn in use in. the blade head assembly of a wafering machine,

FIG. 3 is a plan view of the preferred embodiment of a jig assembly suitable for the fabrication of the integral blade package illustrated in FIG. 1,

FIG. 4 is a side elevation of the jigl assembly shown in. FIG. 3sectioned substantially on line 4-4 of FIG. 3,

FIG. 5 is a three dimensional exploded view of an alternate embodiment of a jig assembly forfabricating an integrated bladerpackage as illustrated .in FIG. l,

FIG.A 6 is a plan` View of the blade head assembly of the instant invention, and

FIG. 7 is a vertical `section taken on line 7-7 ofv FIG. 6.

Referringnow to thedrawings wherein the respective numerals refer tolike or corresponding parts, FIG. 6 illustratesga blade head` assemblygenerally designated by the reference numeral 20 providedwith aV-.slide 21 and a flat-slide 22 respectively disposed in sliding engagement with a V-way ll-andiaflat-way 12 secured to the` horizontalv upper surface of the base 10 of a multiple blade wafering machine. The blade head `assembly 20 includes a first longitudinal. frame member 25. anda second` longitudinal frame member 26 to` which the respective slides 21 Iand, 22 are xedly secured by suitable attachment means such as. machine screws,` not shown, in order to simplify the showingin- FIG.` 6. The respective longitudinal` frame membersl25 `and 26y are interconnected at oneend by a` first end frame member 27 and at' the other end by a secondendV frame member28.

A blade supporting element 31, cooperating with the rst and frame member 27 to support and tension a blade package .70 is supported transversely of thetblade head assembly 20 adjacent to but spaced from the. second end frame member 28. The supporting element31 may be supportedin` sliding relation to the longitudinal`

frame members

25 and 26 by guides 33i1and 34 projecting from the opposite ends thereof and slidable in

channels

35 and 36 in the respective4 longitudinanl .frame members.25 and 26. With a blade packagev 70,-supported in theblade head assembly 20 in the manner described in detail4 further below, the supporting element 31 is adjustably positioned in relation to the-second end` frame 28 by suitable connecting means such as one or more machine screws 38 .seated androtata'ble within suitable `recesses in the second `end frame. member 28` and threadably engaged with the Supporting element 31. As illustrated -in\FIG. 6, the blade head assemblyaincludes three` screws 38"supported .by the end frame, member-28 and threfadablytengaging the supporting element 31.

The means forsupportingabladepackage in the blade head assembly 20 as illustrated in FIGS, 6 and 7, includes first and second pairs of jaws ,and first and,` second pairs of clamp members operativelyengagingv the respective ends of a blade package 70. The first pair of jaws consists of la lower jaw 41a which may be formed integrally wit-l1V tllefirst4 end frame member 217 andV an upper jawl 42a which maybe formedintegrally with a first cap member 47 whichr is releasably securedto the first end frame member 27 by a plurality of cap screws 51 as shown best in FIG. 7. The second pair of jaws consists of a lower jaw 41b which may be formed integrally with the supporting element 31 and an upper jaw 42b which may be formed integrally with a second cap member 48 releasably secured to the supportlng member 31 by a plurality of cap screws 51 as shown best in FIG. 7. The first pair of clamp members consists of va block 61a disposed within a channel formed between the end -frame member 27 and the cap member 47 by the rst pair of jaws 41a and 42a, and against the surface of a projecting side portion 65a of the end frame member 27 and a second block 62a positioned within the same channel formed by the first pair of jaws 41a and 42a by an adjusting screw 53a extending through a suitable opening in longitudinal frame member 26 and threadably engaged with the projecting side portion 66a of the end frame member 27 as shown in FIG. 6. The second pair of clamp members consists of a block 61b disposed within the channel formed between the supporting element 31 and the cap member 48 by the second pair of jaws 4111 and 42b and against the projecting side portion 65b of supporting element 31 and a second block 6211 p-ositioned within the same channel formed by the second pair of jaws 41b^and 42b by an adjusting screw 53b extending through an enlarged clearance hole in the longitudinal frame member 36 and threadably engaged with the projecting side portion 66h of supporting element 31 as shown in FIG. 6.

As best illustrated in FIG. 1, the integral blade package generally designated by reference numeral 70 incorporated in the blade head assembly of the instant invention consists of rst and second spaced parallel series of thin flat spacer elements and a multiplicity of elongated relatively narrow blades 73 of thin strip material with their respective ends disposed between and bonded to adjacent spacer elements 71 of the respective series of spacer elements by suitable means such as a thermosetting adhesive material 75.

Noting that the working edges of the respective blades are worn away to `a substantial degree in use by interaction with a work piece in the presence of an abrasive slurry, the utility of such blades is limited by the amount vof wear sufcient to reduce the minimum cross section area of each blade to the critical amount suicient to withstand the tension force exerted on each blade by the adjustment of t-he supporting element 31 within the blade head assembly 20. Thus, this critical minimum area is determined by the strength of the blade material, the thickness of the blade material, and the magnitude of the tension force applied to each blade. In order to achieve the most favorable distribution of the force applied to each blade as the critical minimum cross section area is approached due to Wear of the working edge 74, the blades may conveniently be fabricated from stock of suflicient initial width between the respective Working edges 74, as illustrated in FIG. 2, so that the blades may be worn first a predetermined amount on one side along a rst working edge and then substantially the same predetermined amount on the other side along a second working edge by reversing the blade package in the blade head assembly so that a symmetric-al configuration of each blade is approached as the safe mini- .mum cross section -area limiting blade use is approached.

vside in a blade head assembly of suflicient width to support two or more blade package segmental units. In this embodiment of the instant invention, one pair of spacers 71 may be omitted on one side of eac-h blade package `segmental unit so that a single pair of spacers will be interposed between the outermost blades 73 of adjoining segmental units.

`In assembling an integral blade package or the 'respective segmental units of a blade package, it 1s 1mportant that each integral assembly be fabricated under conditions fully compatible with the critica-l conditlons under which multiple blades must be installed in a blade head assembly 20 including the requirement that the facing edges of the respective series of spacer elements 71 must fall in spaced parallel planes perpendicular to the respective blades 73, the requirement that equal lengths of the respective blades 73 be exposed between the facing edges of the respective series of the spacer elements 71, and the requirement that the respective pairs of spacer elements 71 and the interfitted blades 73 be disposed in spaced parallel planes all perpendicular to the spaced parallel planes including the facing edges of the respective series of spacer elements 71 and to spaced parallel planes intersecting the respective working edges 74 of the multiple blades 73. All these requirements can be met by assemblying an integral blade package or segmental units thereof in a suitable jig assembly such as that illustrated in FIGS. 3 and 4 or such as that illustrated in FIG. 5.

Each of the jig assemblies illustrated is characterized by a jig body 81 having an elongated planar surface 82 terminating at its opposite ends in oppositely facing parallel shoulders 83a and 83h perpendicular thereto for engagement with the facing edges of the respective series of spacer elements 71. Relatively `depressed coplanar surfaces 84a and 84b parallel to surface 82 and projecting beyond the respective shoulders 83a and 83b support the lower edges of the respective series of spacer elements 71. The respective series of spacer elements 71 are also supported during assembly by removable jig end blocks 85a and 85b which may be provided with locating and supporting pins 87 cooperating with locating holes 88 in the jig body 81. With the exception of end block 85b in the embodiment illustrated in FIGS. 3 and 4, each of these end blocks is provided with upstanding shoulders 86a and 86b adjoining relatively depressed coplanar extensions 84e and 84d of the respective surfaces 84a and 84b. The pair of spacer elements 71 at one side of the blade package are supported in the proper lposition in the jig by a common planar face 89 as shown in FIG. 5 or coplanar faces 89a and 8911 as shown in FIG. 3 in a plane perpendicular to the surface 82 and also perpendicular to the shoulders 83a and 83b.

Referring more particularly to the jig assembly illustrated in FIGS. 3 and 4, it will be noted that the jig body 81 in this embodiment comprises a relatively fixed body portion 81a which may conveniently be supported on a plurality of legs 91 projecting from the underside thereof and a relatively movable body portion 81b mounted for sliding movement longitudinally of the body portion 81a and constrained by suitable means such as pins 93 so that its upper surface g2b is maintained coplanar with the upper surface 82a of body portion 81a. A positioning screw 95 threadably engaging body portion 81b with one end thereof bearing against body portion 81a may be rotated to move body portion 81h lengthwise of body portion 81a into engagement with a suitable stop such as stop pin 97 projecting from body portion 81a. The jig assembly illustrated in FIGS. 3 and 4 also includes a positioning block 10151 provided with a shoulder 103a located coplanar with the shoulder 83a by locating pins 105 and secured by cap screws 107 threadably engaging the jig body portion 81a, and a positioning block 101b with a shoulder 103b located coplanar with vshoulder 8321 by locating pins 10S and secured by cap `screws 107 threadably `engaging the body portion 81b. Thus, the shoulders 83a,

103a and 83h, 103b correspond to the coplanar inner surfaces of the jaws 41a, and 42a and 41h, 42b of the blade head assembly 20.

The embodiment of the jig assembly illustrated in FIGS. 3 and 4 is -also provided with a pair of transverse clamping means corresponding to the first and second pairs of clamp members incorporated in the bladehead assembly 20 consisting of clamp blocks 111a and 111b respectively slidably supported upon body portion81a andY upon body portion 81b so that they may be advanced toward the respective faces 89a and 89b by positioning -screws112a and 112b `respectively threadably engaging the body portions 81a and 81b as illustrated in FIG. 3.

Referring more particularly to the jig assembly illustrated in FIG. 5, it will be noted that substantially elongated temporary spacer elements 77 of the same thickness as the pairs of spacer elements 71 are inserted in the jig assembly on each side of each blade 73 .and thus between and in line with the respective pairs of spacer elements 71, in lieu of the relatively movable body portion 81b and the positioning screw 95 therefor provided in the embodiment of the jig assembly illustratedin FIGS. 3 and 4.

In the embodiment of the jig assembly illustrated in FIG. 5, the transverse clamping means corresponding to the pairs of members provided in the blade head assembly 20 consists of an elongated clamping member 131 slidably supported upon the surface 82 of the jig body 81 and having a working face 132 disposed in a plane parallel to the plane of face 89 for coaction therewith. The elongated clamping member 131 is provided with a longitudi nally extending shoulderr133`engaged by the outermost edges of a plurality of clamping blocks 135 respectively secured in bearing engagement with' the elongated clamping member 131 by a corresponding plurality of positioning screws 138 Ithreadably engaged in an upstanding shoulder portion 139 formed integrally with or fixedly secured to the jig body 81.

In order to assemble a blade package as illustrated in FIG. l in the jig assembly illustrated in FIGS. 3 and 4, the positioning screw 95 is rotated so that Ithe jig body portion 81b may be moved all the way to the left as seen in FIGS. 3 and 4 into engagement with the facing surface of the body portion 81a. The end blocks 85a andv 85h lare installed as shown by inserting the pins 87 in the cooperating holes 88 and the positioning blocks 101a and 101b are removed after the cap screws 107 are disengaged from the respective body portions 81a and 81b.` After the positioning screws 112a and 112b have been rotated to permit full retraction of the clamp blocks 111e and 111b, pairs of spacer elements 71 and the blades 73 are stacked alternately in the jig assembly as indicated in FIG. 3 preferably starting with a pair of spacer elements disposed against the faces 89a and 89b. When a com plete lset of spacer elements 71 and blades 73 has been placed in the jig assembly, omitting thelast pair of spacer elements 71 outside the last blade 73 in thecase of a segmental unit of a blade assembly, the positioning screws 112a and 112b are rotated to advance the clamping blocks 111a and 111b into light clamping engagement with the assembled blades and spacer elements.

The positioning blocks 101:1. and 101b` are mountedon the body portions 81a and 81b, respectively, as shown in FIGS. 3 and 4 and secured thereto by cap screws 107. The positioning screw 95 is then rotated to displace the body portion 81b relative to the body portion 81a until the body portion 81b engages the stop pin 97 projecting from the body portion 81a. Next, the respective positioning screws 112a and 112b are further rotated to clamp` the respective series of spacer elements 71 and the intervening ends of the respective blades 73 tightlyl between clamp block 111a and face 89a and between clamp block 111b and face 89h.

The relative displacement of the respective body portions 81a and 81b with the blades and spacer elements lightly clamped results in` relative displacement of the respective blades 73 and the spacer elements 71 by the respective pairs of shoulders 83a, 1031/1 and 83h, 103b, under the constraint imposed by sliding friction between adjacent parts. This procedure assures that all of the spacer elements 71 of one series will be disposed in engagement with the shoulders 83a and 103a and that all of the spacer elements of the other series will be disposed in engagement with the shoulders `83b and 1031i. This procedure further assures that 4the blades 73 will be drawn into the precise spaced parallel relationship required for uniform tensioning of the respective blades in a blade headassembly by positioning allof the blades so that the portions thereof extending between the respective series of spacers are equal.

The procedure for the assembly of a blade package as shown inl-TIG. 1 in the jig assembly illustrated in FIG. 5 is similar to that described above in` connection with the jig assembly shown in FIGS. 3 and 4. The end blocks 85a and 85b` are mounted on` the jig body 81 by inserting the pins 87 in the cooperating holes` 88. A spacer element 71 is placed in the channel formed by the shoulder 83a and a shoulder 85 so that it is disposed in engagement with one end of lthe face 89 and a spacer element 71 is placed in the channel formed by the shoulder 8311 and a shoulder 85 so that it is disposed in engagement with ythe other end of the face 89. A temporary elongated spacer 77 is placed upon the surface 82 in en gagement with the face 89 substantially midway between the respective spacer elements 71 referred to above. A blade 73 is placed upon the surface 82 in engagement with the respective spacer elements 71 and the spacer element 77 referred to above. This sequence of steps is repeated until a blade package of the desired Width is assembled in the jig assembly, and the package is completed by adding a nal pair of spacer elements 71 and a final spacer element 77 outside the last blade 73, except in the case of a segmental unit of a blade package when thiswlast set of spacer elements is preferably omitted.

The elongated clamping member 131 is placed. upon the surface 82 of the jig body 81 with its face 132 in engagement with the assembled blade package as shown in FIG. 5 and the clamping blocks 135 coacting therewith are inserted between the shoulder 133 of the clamping member 131 tand the respective positioning screws 138. The endmost positioning screws 13S are rotated within the shoulder portion 139 to lightly clamp the` respective series of spacer elements 71 and the respective ends of 4the blades 73 interposed therebe-tween. The intermediate positioning screws 138 arev also rotated in the shoulder portion 139 to force `the corresponding clamping blocks into engagement with the intermediateportion of the clamping member 131 in order to maintain the face 132 of `the clamping `member 131 parallel to the `face 89 of the jig body 81 and thereby `to position the respective blades 73 between the temporary spacer elements 77 so that corresponding surfaces thereof coincide with spaced parallel planes perpendicular -to the planar surface` 82.

After all of the spacer elements 71 have been checked to be sure that the adjacent edges of all of the spacer elements 71 of one series are in engagement with the shoulder 83a and that all of the adjacent edges of the spacer elements 71 lof the other series are in engagement with the shoulder 83b, the assembly blade package is clamped tightly rbetween the base 89 and the elongated clamping member 131 by further rotation of the respective positioning screws 138 with the respective blades 73 all seated firmly on surface 82 and with all of the spacer elements 71 seated rmly on the respective surfaces 84.

Noting that the spacer elements 71 fora given integral blade package lmay have a uniform thickness for each of from .012" to .024" and that spacer elements of a uniform `thickness as low as .007 or less may be used in certain applications, and further that blades 73 may be used in a given blade package of a uniform thickness commonly .004 to .008 and down to a thickness of .002" or less for certain application, it will be evident that the bonding agent applied must be carefully selected so that it will ilow readily into the relatively ylimited spaces between adjacent blades and into the even more limited spaces between adjacent spacer elements. In addition, the bonding agent must demonstrate good wetting properties when applied to the metallic surfaces of the blades and spacer elements. Moreover, the bonding agent must consist of a material which does not shrink as it sets up. Finally, the bonding agent selected must be suitable for application at a temperature below that which will adversely affect the heat treatment of the blades. Since there are sevenal bonding agents commercially available which meet these requirements, it is `deemed suflicient to describe `the application of one such bonding agent below.

In the preferred embodiment of the blade package 70 characterizing -the instant invention, the respective blades 73 and spacer elements 71 of the blade package are bonded together by the application thereto of a suitable thermosetting adhesive material 75 such as the epoxy composition available commercially under the name of Tygoweld PB-l cement.

In order to achieve an effective bond by means of such an adhesive, the end blocks 85a and 8511 are removed from the jig assembly with `the parts of a blade package clamped tightly therein as described above. The jig assembly and the parts of a blade package supported thereby are heated in an oven to a suitable predetermined temperature, for example 350 F. when the adhesive used is Tygoweld PB-l cement. After the entire jig assembly and the blade package supported thereby have reached the desired predetermined temperature, the jig assembly is removed from the oven and the thermosetting adhesive 75 =is applied to the spacer elements 71 and to the projecting end portions of the blades 73 at each end of the blade package, so that the adhesive penetrates all Of the spaces between adjacent parts of the blade package to secure each end of each blade to the adjoining spacer elements. After the Iadhesive 75 has been applied to both ends of `the blade package clamped in a jig assembly, the jig assembly is returned to an oven held at a predetermined temperature, for example 350 F. in the case of Tygoweld PB-l cement, for a period suicient to cure the adhesive 75.

When the thermosetting adhesive 75 has been cured, the jig assembly is removed lfrom the oven and cooled before the nished blade package 70 is removed from the jig assembly. When the jig assembly used is constructed according to FIG. 5, the temporary elongated spacer elements 77 may then be stripped from between the respective blades 73.

When the adhesive used for bonding the respective elements of an integral blade package is not characterized by thermosetting properties, the heating cycle following the application of the ladhesive may be omitted. However, preheating of the jig assembly and the blade package parts `supported thereby to a relatively low temperature above room temperature still may be desirable as a means of facilitating the ow of adhesive into the very limited spaces between adjacent blades and between adjacent spacer elements.

The luse -of integral blade packages fabricated in the manner described above greatly `facilitate-s the proper installation of a large multiplicity of elongated blades in the blade head assembly of a multiple blade power hacksaw with the added advantage that the proper precise alignment of all of the blades 73 is assured by the fact that the integral blade package is fabricated Iunder conditions which assure the precise orientation of all the respective blades and which are compatible with the conditions imposed on'the blades when they are installed in a blade head assembly.

From inspection of the showing in FIG. 7, it will be evident that the use of an integral blade package 70 in the blade head assembly of a multiple blade wafering machine further facilitates the proper precise alignment of all the blades 73 by virtue of the fact that the pairs of jaws 41a, 42a and 41b, 42h arranged to coact with an integrated blade package rather than individual blades and spacer elements may be relieved along their opposing faces as shown in FIG. 7 so that neither one of these faces eng-ages the edges of the blades. Thus the orientation of the respective blades depends entirely upon the intervening spacer elements and is not affected by `any direct interaction between the pairs of jaws and the blades.

The use of an integral blade package in the blade head assembly as a means of assuring the proper precise alignment of all the blades is particularly effective with respect to the vertical alignment of the blades in the horizontally disposed blade head assembly so that all of the blades are supported perpendicular to the plane of the respective working edges 74 of the multiple blades, within extremely close tolerances of the order of ten minutes of arc or less from true vertical. This extremely precise vertical alignment of the respective blades in turn makes it possible to substantially increase the width of the blades between the respective edges 74 thereof so that the tension force applied to each blade may be increased rand/or so that the thickness of the blades may be further reduced to reduce the width of the kerf and thereby reduce the amount of material wasted as a result of the watering operation.

The yuse of blade packages according to the teachings of the instant invention characterized by the precise vertical alignment of the blades within extremely close tolerances offers the additional advantages inherent in reversing the blades for wear in the manner indicated in FIG. 2. In a blade package characterized by blades 73 of substantially increased width between the respective working edges 74, the amount of blade wear which can be tolerated in relation to the minimum necessary blade cross section area is substantially increased. In addition, the reversal of such `blades midway of their use-ful life provides for equalized wear of the respective blades .along the opposite working edges 74 so that the respective blades once again approach a symmetrical configuration as illustrated in FIG. 2 as they approach their fully wornout condition.

The precision installation of properly selected multiple blades and associated spacer elements in a blade head assembly is further assured by the assembly of these blades and spacer elements in integral blade packages, because these integral blade packages may be checked readily on the commercially available Optical inspection equipment commonly used for the critical inspection of precision parts.

Relatively wide blade packages including very large numbers of blades may conveniently be made up of several segmental units in the manner referred to above to good advantage for various reasons. For example, when the ingot to be sliced is substantially shorter than the maximum capacity of a particular blade head assembly, the blade head assembly may be loaded with a reduced number of segmental Iunits suflicient to span the particular work piece being cut. In addition, it may be desirable to cut groups of wafers of different thicknesses from the same ingot by installing segmental units in a blade head assembly each having spacer elements of a different thickness in order to produce wafers of the desired different thicknesses simultaneously.

From consideration of the above disclosure, it will be evident that the instant invention provides an improved blade Ahead assembly for multiple blade wafering machines characterized by the inclusion therein of an integral blade package, and further provides satisfactory methods for fabricating such an integral blade package with the requisite precision.

Since various details of this invention are subject to modification, it is to be understood that the embodiment described above and illustrated in the accompanying drawings is to be interpreted as illustrative and not in a limiting sense, `and that the scope of this invention is deand to a second reference plane parallel thereto interned by the claims 4appended hereto. secting the other longitudinal edge of each blade, and We claim: a plurality of pairs of substantially identical short and 1. An integrated reversible blade package for mouiitrelatively wider spacer elements of thin at sheet maing under tension in a multiple blade watering machine 5 terial of uniform thickness throughout, comprising each pair of spacer elements being disposed adjacent a plurality of relatively wide fiat thin spacer elements one surface of one of said blades at the opposite ends of equal uniform thickness arrayed in equal first thereof for engagement with the adjoining surface and second spaced parallel series, and of an adjacent blade and bonded to the abutting sura multiplicity of relatively narrow elongated blades of faces of said blades adjacent thereto with each spacer thin llat strip material of constant thickness and with element projecting equidistantly beyond the respecopposed parallel longitudinal working edges arrayed perpendicular to and with one longitudinal edge of each blade intersecting a reference plane,

each blade having one end disposed between and bonded to adjacent spacer elements or the first series and the other eiid disposed between and bonded to adjacent spacer elements of the second series so that the respective opposite edges of said spacer elements project beyond the respective longitudinal edges of said elongated blades.

tive longitudinal edges of said blades adjacent thereto,

whereby a multiplicity of spaced parallel blades and a plurality of pairs of spacer elements adhered thereto together form a unitary blade package for mounting in either a rst working position or in a reversed second working position in a multiple blade wafering machine.

4. A blade head assembly for a multiple blade wafering machine comprising an elongated multiple blade package,

the width of said blades between the longitudinal edges said blade package including a plurality 0f nat thin relathei'eof being selected in relation -to the blade material, the blade thickness and the tension load to tively wideV spacer elements ariayed in first and second spaced parallel series, and

be applied lo ldie blades in a Wafering machine so a multiplicity of relatively narrow elongated blades of that with substantially one third ef the blade widih ihinnai strip material each with Opposed parallel worn away from one longitudinal edge of each blade ionglilldmal Working edges, and substantially one third of the blade width worn eeh blade Wliil one end disposed between and bonded away from the other longitudinal edge of each blade to adjacent spacer elements of the iirst series and the the remaining reduced cross-section area of e-acli 3o other end disposed between and bonded to adjacent `blade is suflieiem to wilhslland the tension load apspacer elements of the second series with each spacer plied to each blade of said blade package by a multielement Projecting equidisianly beyond the respecple blade Wafering machine tive longitudinal edges of the blades adjacent thereto, 2. A double edged reversible blade package for a mula generally reoiangillar supporting frame Sldably suptiple blade wefering maehine Comprising ported in a horizontal plane by the base of a Wafering -a plurality of relatively wide ilat thin square spacer ele maeillne,

ments of equal uniform thickness arrayed in equal s iirsi blade Package engaging means disposed 'fransiirst and second spaced parallel sei-ies and versely or one end of said supporting frame including -a multiplicity of relatively narrow spaced parallel a first Pair of opposed elongated reieasabie laws and elongated blades having opposed longitudinal Work- 40 a irsi Pair of opposed reieasabio Clamp members dising edges and of thin dat strip material arrayed perposed adlacenr the OPPoslie ends of said first Pair of pendiculai to and with one longitudinal edge of each Jaws? blade intersecting a reference plane, an adjustable supporting element disposed adjacent each blade having one end disposed between and bondthe other end of said supporting frame,

ed to adjacent spacer elements of the first series and a second blade Package engaging means disposed trans" the other end disposed between and bonded to ad- Veisoiy of sold supporting frame and supported by jacent spacer elements of the second series so that the Said supporting element including a second Pair of respective opopsite edges of each said spacer element opposed elongated reieassbie laws and a second Pair project equidistantly beyond the respective longitu- 50 of opposed relessable Clamp members disposed addinal edges of said elongated blades and the facing Jacobi ibo opposite ends of said second Pair of J'aWS, edges of the spacer elements io the respective series the respective series of spacer elements of said blade lie in spaced parallel planes perpendicular to the ref- Package boing soourod m the respectivo Pairs of laws ei-enee plane and the bladesa and the respective ends of the blade package being whereby said blade package may be mounted in a rst Secured oeiWF/on the rosPoCilVe Pairs of CismP mem- Working position in a multiple blade Wafering ma bers with said blade package selectively in either a chine until each said blade is reduced in cross secirst horizontal Working Position o1' in an inVeIted tion a substantial predetermined amount by wear .Second horizontal ,Woikmg Position, and along its iirst longitudinal edge and then in a reversed adjustableblade tensioning lmeans interconnecting said second working position until each said blade is re- Supporting frame arid ssld slipporimg element and duced in cross section substantially the same prede- OPorobie to dispiace said supporting element lontermined amount by Wear along its second longitugitndinally relative to said supporting frame to tendioal edge sion the blades of said elongated multiple blade pack- 3. A reversible blade package for a multiple blade ago watering machine comprising l.

a multiplicity of substantially identical elongated rela- 60 References Cited by the Examiner tively narrow blades having opposed longitudinal FOREIGN PATENTS workingedges and of thin lat sheet material of uni- 570,624 2/1959 Canada form thickness throughout disposed 1n spaced par- 106,804 6/1917 Great Britain' allel planes all perpendicular to a rst reference 7o plane intersecting one longitudinal edge of each blade HAROLD D. WHITEHEAD, Primary Examiner.

Claims

1. AN INTEGRATED REVERSIBLE BLADE PACKAGE FOR MOUNTING UNDER TENSION IN A MULTIPLE BLADE WAFERING MACHINE COMPRISING A PLURALITY OF RELATIVELY WIDE FLAT THIN SPACER ELEMENTS OF EQUAL UNIFORM THICKNESS ARRAYED IN EQUAL FIRST AND SECOND SPACED PARALLEL SERIES, AND A MULTIPLICITY OF RELATIVELY NARROW ELONGATED BLADES OF THIN FLAT STRIP MATERIAL OF CONSTANT THICKNESS AND WITH OPPOSED PARALLEL LONGITUDINAL WORKING EDGES ARRAYED PERPENDICULAR TO AND WITH ONE LONGITUDINAL EDGE OF EACH BLADE INTERSECTING A REFERENCE PLANE, EACH BLADE HAVING ONE END DISPOSED BETWEEN AND BONDED TO ADJACENT SPACER ELEMENTS OF THE FIRST SERIES AND THE OTHER END DISPOSED BETWEEN AND BONDED TO ADJACENT SPACER ELEMENTS OF THE SECOND SERIES SO THAT THE RESPECTIVE OPPOSITE EDGES OF SAID SPACER ELEMENTS PROJECT BEYOND THE RESPECTIVE LONGITUDINAL EDGES OF SAID ELONGATED BLADES. THE WIDTH OF SAID BLADES BETWEEN THE LONGITUDINAL EDGES THEREOF BEING SELECTED IN RELATION TO THE BLADE MATERIAL, THE BLADE THICKNESS AND THE TENSION LOAD TO BE APPLIED TO THE BLADES IN A WAFERING MACHINE SO THAT WITH SUBSTANTIALLY ONE THIRD OF THE BLADE WIDTH WORN AWAY FROM ONE LONGITUDINAL EDGE OF EACH BLADE AND SUBSTANTIALLY ONE THIRD OF THE BLADE WIDTH WORN AWAY FROM THE OTHER LONGITUDINAL EDGE OF EACH BLADE THE REMAINING REDUCED CROSS-SECTION AREA OF EACH BLADE IS SUFFICIENT TO WITHSTAND THE TENSION LOAD APPLIED TO EACH BLADE OF SAID BLADE PACKAGE BY A MULTIPLE BLADE WAFERING MACHINE.