US3234052A - Beryllium sheet and method of producing same - Google Patents
Beryllium sheet and method of producing same Download PDFInfo
- Publication number
- US3234052A US3234052A US127505A US12750561A US3234052A US 3234052 A US3234052 A US 3234052A US 127505 A US127505 A US 127505A US 12750561 A US12750561 A US 12750561A US 3234052 A US3234052 A US 3234052A
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- United States
- Prior art keywords
- block
- beryllium
- rolling
- jacket
- frame
- Prior art date
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- Expired - Lifetime
Links
- 238000000034 method Methods 0.000 title description 25
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 title description 5
- ATBAMAFKBVZNFJ-UHFFFAOYSA-N beryllium atom Chemical compound [Be] ATBAMAFKBVZNFJ-UHFFFAOYSA-N 0.000 claims description 49
- 229910052790 beryllium Inorganic materials 0.000 claims description 45
- 230000009467 reduction Effects 0.000 claims description 27
- 230000015556 catabolic process Effects 0.000 claims description 23
- 230000002093 peripheral effect Effects 0.000 claims description 13
- 229910052751 metal Inorganic materials 0.000 claims description 12
- 239000002184 metal Substances 0.000 claims description 12
- 239000000203 mixture Substances 0.000 claims description 11
- 239000011248 coating agent Substances 0.000 claims description 4
- 238000000576 coating method Methods 0.000 claims description 4
- 230000003647 oxidation Effects 0.000 claims description 4
- 238000007254 oxidation reaction Methods 0.000 claims description 4
- 238000004140 cleaning Methods 0.000 claims description 2
- 238000004519 manufacturing process Methods 0.000 claims description 2
- 238000013022 venting Methods 0.000 claims description 2
- 238000005096 rolling process Methods 0.000 description 60
- 238000006722 reduction reaction Methods 0.000 description 26
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 9
- 239000000463 material Substances 0.000 description 8
- 238000003466 welding Methods 0.000 description 7
- QAOWNCQODCNURD-UHFFFAOYSA-N Sulfuric acid Chemical compound OS(O)(=O)=O QAOWNCQODCNURD-UHFFFAOYSA-N 0.000 description 6
- 150000001875 compounds Chemical class 0.000 description 5
- 239000011888 foil Substances 0.000 description 5
- 238000010438 heat treatment Methods 0.000 description 5
- 239000010935 stainless steel Substances 0.000 description 5
- 229910001220 stainless steel Inorganic materials 0.000 description 5
- 238000005253 cladding Methods 0.000 description 4
- QDOXWKRWXJOMAK-UHFFFAOYSA-N dichromium trioxide Chemical compound O=[Cr]O[Cr]=O QDOXWKRWXJOMAK-UHFFFAOYSA-N 0.000 description 4
- 238000005242 forging Methods 0.000 description 4
- 239000010439 graphite Substances 0.000 description 4
- 229910002804 graphite Inorganic materials 0.000 description 4
- 238000005554 pickling Methods 0.000 description 4
- 229910001209 Low-carbon steel Inorganic materials 0.000 description 3
- GRYLNZFGIOXLOG-UHFFFAOYSA-N Nitric acid Chemical compound O[N+]([O-])=O GRYLNZFGIOXLOG-UHFFFAOYSA-N 0.000 description 3
- 229910000831 Steel Inorganic materials 0.000 description 3
- 239000007864 aqueous solution Substances 0.000 description 3
- 238000000227 grinding Methods 0.000 description 3
- 238000002844 melting Methods 0.000 description 3
- 230000008018 melting Effects 0.000 description 3
- 238000005245 sintering Methods 0.000 description 3
- 239000007858 starting material Substances 0.000 description 3
- 239000010959 steel Substances 0.000 description 3
- 239000010455 vermiculite Substances 0.000 description 3
- 229910052902 vermiculite Inorganic materials 0.000 description 3
- 235000019354 vermiculite Nutrition 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 239000007900 aqueous suspension Substances 0.000 description 2
- 230000004888 barrier function Effects 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 238000005336 cracking Methods 0.000 description 2
- 238000005520 cutting process Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000005496 eutectics Effects 0.000 description 2
- 238000005098 hot rolling Methods 0.000 description 2
- 229910017604 nitric acid Inorganic materials 0.000 description 2
- 238000005498 polishing Methods 0.000 description 2
- 239000004576 sand Substances 0.000 description 2
- 239000007921 spray Substances 0.000 description 2
- 239000000725 suspension Substances 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- NDYMQOUYJJXCKJ-UHFFFAOYSA-N (4-fluorophenyl)-morpholin-4-ylmethanone Chemical compound C1=CC(F)=CC=C1C(=O)N1CCOCC1 NDYMQOUYJJXCKJ-UHFFFAOYSA-N 0.000 description 1
- FRWYFWZENXDZMU-UHFFFAOYSA-N 2-iodoquinoline Chemical compound C1=CC=CC2=NC(I)=CC=C21 FRWYFWZENXDZMU-UHFFFAOYSA-N 0.000 description 1
- 229910001104 4140 steel Inorganic materials 0.000 description 1
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 1
- 241000870659 Crassula perfoliata var. minor Species 0.000 description 1
- 229910000922 High-strength low-alloy steel Inorganic materials 0.000 description 1
- 238000005299 abrasion Methods 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 238000000137 annealing Methods 0.000 description 1
- 239000010425 asbestos Substances 0.000 description 1
- LTPBRCUWZOMYOC-UHFFFAOYSA-N beryllium oxide Inorganic materials O=[Be] LTPBRCUWZOMYOC-UHFFFAOYSA-N 0.000 description 1
- 230000001680 brushing effect Effects 0.000 description 1
- BRPQOXSCLDDYGP-UHFFFAOYSA-N calcium oxide Chemical compound [O-2].[Ca+2] BRPQOXSCLDDYGP-UHFFFAOYSA-N 0.000 description 1
- ODINCKMPIJJUCX-UHFFFAOYSA-N calcium oxide Inorganic materials [Ca]=O ODINCKMPIJJUCX-UHFFFAOYSA-N 0.000 description 1
- 239000000292 calcium oxide Substances 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 229910052804 chromium Inorganic materials 0.000 description 1
- 239000011651 chromium Substances 0.000 description 1
- 239000000084 colloidal system Substances 0.000 description 1
- 230000000295 complement effect Effects 0.000 description 1
- 230000002939 deleterious effect Effects 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 239000004519 grease Substances 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 230000001590 oxidative effect Effects 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
- 229910052895 riebeckite Inorganic materials 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
- 239000010409 thin film Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21B—ROLLING OF METAL
- B21B3/00—Rolling materials of special alloys so far as the composition of the alloy requires or permits special rolling methods or sequences ; Rolling of aluminium, copper, zinc or other non-ferrous metals
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/30—Foil or other thin sheet-metal making or treating
- Y10T29/301—Method
- Y10T29/302—Clad or other composite foil or thin metal making
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/4998—Combined manufacture including applying or shaping of fluent material
- Y10T29/49982—Coating
Definitions
- the present invention is directed to the hot rolling of jacketed beryllium billets into the form of plates and sheets of substantial area and thickness, as distinguished from small sheets of foil, which generally are less than 0.005 inch in thickness, and thin metal coupons of small area.
- the sheets contemplated range, for example, from 0.020" to 0.375 in thickness, from 20" to 36" in width, and from 60" to 96 in length.
- a method disclosed in Creutz Patent No. 2,653,494, issued September 29, 1953, is directed to the forging of cast beryllium ingots and recognizes that unjacketed cast beryllium ingots cannot be forged at temperatures ranging from 500 C. to about 1200 C., without cracking, but that beryllium can be forged at temperatures in the neighborhood of 700 C. up to the melting point of the eutectic of beryllium and iron, if jacketed in a suitable
- the patent shows that at temperatures above the minimum melting eutectic point of beryllium and the jacket metal, the beryllium tends to fuse and alloy with the jacket material.
- refractory barrier material such as a layer of calcium oxide is interposed between the beryllium and jacket.
- the purpose of the jacket is to prevent oxidation of the beryllium at the elevated temperatures exceeding 865 C. which are required for forging beryllium into products having satisfactory mechanical and physical properties.
- the higher temperature is to obtain the extremely rapid flow of beryllium necessary for forging.
- the results obtained in the rolling of beryllium billets into sheets of substantial area depend upon a number of factors, including the material used as the starting material for the rolling operation, the manner of enclosing the beryllium billets or partially formed sheets or plates in suitable jackets, and the steps and manner of initially seating the billet in the jacket, and of rolling, and in some instances, recladding, annealing, and subsequent rolling to the desired thickness.
- a most critical step is the initial cladding and the breakdown rolling step both as to the original billet and, if recladding is necessary, as to the newly reclad partially rolled beryllium.
- the starting material is vacuum hot-pressed beryllium, preferably such as made in accordance with Dodds US. Patent No. 2,818,- 339, issued December 31, 1957.
- the billet is formed first by combined heat and vacuum below sintering temperature for a predetermined period, followed by continuance of the vacuum and an increase of the temperature into the sintering range while maintaining the beryllium mass under pressure to compact it during sintering into a billet which is of substantially theoretical density, for example, about 1.85 grams per cubic centimeter.
- the billet selected should be free from cavities and variations in density and substantially free from occlusions.
- the surface should be free from voids and cracks.
- This particular billet is preferred because it has random grain distribution, i.e., isotropic properties. It is preferred over other beryllium bodies which are extruded, cast, or otherwise formed which have anisotropic properties. Billets formed by well-known melting and casting techniques have too low a density and too large a grain size to permit their being formed into sheets of substantially theoretical density, which is the preferred sheet with which the present invention is concerned.
- the billet which is used as the starting material is generally a block or slab, a rectangular parallelepiped being preferred. The block is machined so that all faces are smooth and the corners and edges are ground or sanded to a very small radius, for example, about /s of an inch. It is cleaned to remove grease and foreign matter. As a result, it is true in shape yet free from abrupt, sharp corners and edges.
- This block is coated with a thin film of parting COlIlpound.
- a suitable composition is colloidal graphite suspension, a form of which is sold on the market under the registered trademark Aquadag of which the Acheson Colloids Company, of Port Huron, Michigan, is the proprietor.
- Another suitable composition is a high-temperature graphite in water suspension available commercially under the registered trademark Triple C of which the Pro-Chem Company of Cleveland, Ohio, is the proprietor.
- the parting compound is applied to the block in the form of a smooth coat, preferably by spraying or brushing an aqueous suspension thereof on the block with a spray gun or paint brush or the like, care being taken that no lumps are present, and then allowing the coating to dry.
- the coated block is then placed in a jacket of metal which has been similarly coated on the surfaces which are to contact the beryllium block.
- a metal jacket protects the beryllium from oxidation and confines it during the breakdown step of the rolling method employed.
- the jacketing is effected by enclosing the peripheral edge faces of the block in a frame of rails formed of cold-rolled, mild steel bar stock of rectangular cross section.
- These rails have smooth planar faces adapted to engage the peripheral edge faces of the block. They are coated with the parting composition the same as the surfaces of the block. These rails are then clamped tightly in juxtaposition with the edge faces of the block and are welded together with mitered or butt joints, so that the block is confined peripherally.
- the thickness of the rails, relative to the thickness of the block, in the breakdown rolling step, is critical.
- rails may be equal to, but must not exceed, the thickness of the block is generally about equal to the thickness of the block.
- The-interior'length and width of the frame as a whole are substantially equal to the like dimensions of the block itself.
- cover plates are of hot-rolled and pickled steel; for example,
- Each plate is about one-half the thickness of the beryllium block and extends laterally and end- Wise of the frame a distance such that its peripheral edges are substantially flush with the outermost peripheral edges of the assembled rails.
- the inner faces of the cover plates are coated with the parting compound preparatory to applying them to the block.
- the plates are clamped in position and welded to the rails. are charnfered for Welding purposes at their junctures with Preferably, the rails the plates, and the welding is done by means of welding rod. Molten welding rod material is interposed to. fill up the chamfers so that the outer surfaces of the jacket define a rectangular parallelepiped.
- a suitable vent is provided in the jacket to permit escape of the variousgase's and the like
- it is formed in one of the side rails, usually the side rail which is to be in the trailing direction in the initial or breakdown rolling operation-
- One or more vent holes of about AV'in diameter are adequate for this purpose.
- the jacketed block assembly is heated to a temperature of from about 675 C. to about 860 0, about 760 C. being preferred.
- the initial passes of the breakdown step are referred to herein as the seating passes and the first one of these is used to effect approximately 0.1 to 0.5% reduction in thickness of the block and may be accomplished under the mere weight of the upper'r'oll of the mill stand.
- This first pass is to compress the juxtaposed surfaces of the jacket and block throughout their extent into contact and conformitywith each other, thus assuring that the billet fills the jacket uniformly.
- the seating passes are prefer-.
- the first of these passes causes 0.1 to 0.5% reduction in thickness of the block and may be effected-by the more weight of the upper roll of the mill stand.
- Breakdown rolling follows seating and may be unidimensional, alternating in direction of rolling 180 at suc-.
- An indefinite number of passes may be used in the breakdown rolling step, but if the overall thickness of the jacketed block is oneinch or more, the temperature should preferably remain about 760 C., and if the thickness is less thanone inch, then generally it is preferable to heat to 760 C. and employ one pass per heat.
- the total reduction per pass during the breakdown rolling step should not be greater than15% nor less than 6% of the thickness of the beryllium metal existing *at the beginning-of the particular pass. reduction, regardless of the-number of passes, during the breakdown operation should not be greater than a maximum of 8:1 for any single .jacketing or cladding of the block.
- the block Upon completion of the :breakdown rolling, the block is clad stress relieved in its original jacket. Preferably, this done'by raising it to a temperature of about 760 C. and holding it at that temperatureufor a period of about ten minutes after it is heated uniformly throughout, following which. the clad blockassembly is;.slow cooled in vermiculite to a temperature below red heat and preferably to about room temperature. latter temperature, the jacket is removed, either by torch cutting or otherwise, care being taken that the torch doesnot impinge upon the block and subjectthe beryllium metal to thermal shock which is aptto cause cracking and other deleterious effects.
- the block is stress relieved, preferably by heating it to about 760 C., maintaining. thattemperature from about ten to aboutthirty minutesdependent upon the gauge -or thickness of the block. It is then slid from the furnace onto an asbestos board which allows it to lie flat. When it starts to lose color, it is turned over and after all color is gone,;it is stood on edge and allowed to cool to room. temperature If badly warped, 'it may be fiattened by heating it in the same manner and then placing it under pressure between hot or :insulated platens for about ten minutes, and then removing it from the platens and allowing it to cool as above.
- intermediate rolling operations may be provided and these are generally termed intermediate rolling operations. How-' ever, it is to be borne. in mind that the'number of these will be determined by the thickness of the starting block 1 and the thickness desired in the finished pieces Sometimes a single so-called intermediate rolling operation is all that is necessary.
- nitric acid and one-half of .one' percent sulfuric acid.
- Abrasion and pickling of the surface is continueduntil thetsurfaceflis freefrom beryllium oxide.
- the plate is -fiu shed.with water. and allowed to 1 7 dry. Thereupon, the plate thus produced is cut;to-size 1 in any suitable manner, .such as by abrasive or band saws.
- edges are then sanded andabraded so as to remove.
- sharp corners preferably to a radius ofabont, of an inch, and the entire surface of the workpiece may be smoothed. if..desi-red "by grinding, polishing and the like.
- the sheets have a width and length such that they extend beyond the outer peripheral edge face of the frame an amount equal to about one-half the thickness of the rails in a direction parallel to the plane of the major faces of the block.
- the plates when clamped in this position, are then welded in place and the space between the outer edge of the frame and the overhanging margins of the cover plates is filled with molten welding material so that the outer surface of the jacketed piece is again substantially a rectangular parallelepiped. If the rails are one inch or more in thickness, they are chamfered and the mitered ends V-grooved and filled with the welding material. If the rails are less than one inch in thickness, this is not necessary. The trailing edge rail is vented.
- the jacketed block is preheated uniformly to from about 650 C. to about 860 C., and preferably to 760 C., and the latter temperature maintained for an hour per inch overall thickness of the jacketed assembly to assure uniform heating. It is reheated between passes, if necessary, to provide and maintain a temperature ranging from about 650 C. to about 860 C. during rolling.
- the initial pass effects a reduction of 0.1 to 0.5% which may be accomplished under the mere weight of the upper roll of the mill stand.
- the reduction effected in each of the next two seating passes is increased to approach the reduction employed in subsequent rolling passes.
- Reductions per pass, after the initial passes, shall not exceed nor be less than 6% of the beryllium metal thickness at the beginning of the pass.
- An overall reduction of 6:1 shall be the maximum for each cladding.
- the intermediate rolling shall generally be unidimensional, alternating rolling directions 180 each pass. Bidimensional rolling will only be used in special cases. However, the intermediate slab rolling, when unidimensional, will generally be in a cross dimension, that is, a dimension 90 to the dimension in which the breakdown rolling was carried out. Generally, only one pass per heating is used so as to assure that the rolling temperature is not less than 650 C., and preferably is about 760 C., when the metal becomes relatively thin. Reduction less than the 6% lower and greater then the 15 upper critical limits described above results in defestive plates or sheets. If bidimensional rolling is used, then the intermediate rollingmay start in any direction, but preferably at right angles to the initial pass of the breakdown rolling operation. After the rolling operation, the jacketed sheet is clad stress relieved in the same manner as after the breakdown operation, usually heating it to about 760 C. for about ten minutes and cooling it in vermiculite. Thereafter, the jacket is removed.
- the stock can be reclad and rolled any number of times until the final thickness is reached.
- the stock is bare stressrelieved when the jacket is removed prior to each recladding operation, followed ⁇ by clad stress relief of the assembly.
- the sheet is bare stress relieved, and also flattened, if required, as above described. Thereafter, it is cleaned by grinding and is pickled, as above mentioned, in an aqueous solution of nitric and sulfuric acid, following which it is dried and trimmed to size.
- EXAMPLE 1 A beryllium billet of dimensions 0.770 x 13" X 16', vacuum hot pressed in accordance with the teachings of U.S. Patent No. 2,818,339, was encased in a picture frame assembly as h-ereinbefore described, the mild steel rails of the picture frame assembly were machined at their top edges so that their vertical height was about 0.005" less than the 0.770 vertical height of the beryllium billet. The mild steel covers were each about one half the thickness of the beryllium billet.
- the assembly was then welded together as described above, so that the beryllium billet was tightly sealed in the covered frame, the interior peripheral edge faces of the rails and the inner faces of the cover plates having been coated with Aquadag, an aqueous colloidal graphite suspension, prior to welding rails and cover plates into a unit assembly containing the beryllium block.
- the picture frame assembly was then heated to about 790 C. and passed through the rolls of a twohigh Mesta mill with the initial seating passes made under only the weight of the top roller of the two 30-inch wide rollers to properly seat the assembly. Four initial successive seating passes were made in a clockwise direction alternating 90 per pass.
- the heated assembly while being maintained at a temperature of between 760 C.
- the clad block was stress relieved at a temperature of about 760 C., maintained for about 10 minutes, and followed by cooling in vermiculite.
- the jacket assembly was removed by torch cutting.
- the dimensions of the beryllium block at this state of the operation were 0.178" x 47% x 18%".
- the clad-rolled beryllium plate was then bare stress-relieved for about 10 minutes at about 760 C. after which it was cooled to room temperature on a flat insulated surface.
- the plate After being cooled, the plate was lightly sanded with sand and water to remove the parting compound and subsequently further sand cleaned alternated with pickling in an aqueous solution containing 25% nitric acid and 0.5% sulfuric acid until the surface was free from excessive oxides.
- the beryllium plate was then sawed in half to provide two plates each having the dimensions of 0.178" x '22 x 18%. The edges were then sanded to remove sharp corners and burrs.
- the surfaces of the plate adjacent to the frame were then coated with a composition of Aquadag and the top and bottom faces of the rails coated with chromium sesqui-oxide, and the coating dried.
- each plate was then encased in a picture frame assembly in a similar manner as in the above breakdown rolling operation.
- the cover plates extended beyond the outer peripheral edge or face of the frame an amount equal to about one half the thickness of the rails in a direction parallel to the plane of the plate.
- the assembly was then uniformly heated to a temperature of 745 C. to 760 C. and unidimensionally rolled to an overall reduction ratio of 2.84:1, in a direction transverse to that of the breakdown roll-ing.
- the encased beryllium sheet after being clad-annealed, cooled, and removed from the jacket as in the above breakdown rolling step, had the dimensions of 0.06" x 22" x 53".
- the sheet was subequently bare stress relieved, sanded and pickled as in the breakdown rolling operation, and trimmed to dimensions of 0.055" x 22" x 50 /2".
- the beryllium sheet was then coated with Aquadag, the top and bottom edge faces coated with chromium sesqui-oxide, and the sheet encased in a picture frame assembly in the same manner as for the intermediate rolling operation, with the ex- Said stainless steel interleaves were unattached to and supported only by the welded assembly.
- the assembly was then uniformly heated to a temperature range of between about 745 C. to 760 C. and unidimensionally rolled to an overall reduction ratio of 1.275 :1 in the same direction as in the first above intermediate rolling operation, then clad stress relieved and removed from the jacket.
- the sheet having the dimensions 0.045" x 22%;" X 64 was then cleaned by grinding and pickling and bare-annealed as in the first intermediate rolling step.
- EXAMPLE 2 The same procedure was'followed as in Example 1 with the exception that the block used for breakdown rolling had the dimension 1.05 x 17" x 17 which after being subjected to an overall reduction ratio of 4.62-lhad the dimensions 0.222 x 19 ,5 x 68". This plate was sawed into three equal sections, and one section having the dimensions 0.222 x l9% x 22", after being reclad following the procedure of 'Example'lgwas rolled to an overall reduction ratio of'2.8:l to the dimensions of 0.076 x 55" X 22".
- This sheet was then trimmed to the dimensions of 0.076" X 46%" x 21 and clad in the aforedescribedpicbody, and thickness, and having sufficient strength and I rigidity for use in fabricatedstructures, as distinguished from foils of small size, and 'smallthin coupons having negligible strength for structural purposes, as disclosed in the prior art methods he'reinbefore described. Typical dimensions, physical and other properties of sheets made by the present process are shown in the examples. listed hereinbefore.
- the breakdown :rolling step comprising providing a beryllium blockof substan'tiallyi' theoretical density anduin the form of a right angled parallelepiped. of accurate .dimension'and having its opposite major faces and its'edge faces smooth and planar and its: corners and corner edges'roundedto a short radius, snugly embracing ;the block peripherally.
- Example 3 had the properties 'noted above, in Table I.
- two stainless steel sheets of 0.035" of the same. length and width as the block,-may' of metal may be removed from each face of the sheet, for
- composition is a colloidal graphite composition.
- each of said successive passes provides a reduction from about 6% to about of the thickness of the beryllium block existing at the start of the particular pass.
- the method according to claim 9 wherein the rerolling is by an initial light pressure seating pass, followed by additional seating passes at greater pressure, and is carried out one reduction pass per heat, and the reduction per pass is from 6% to v 12.
- the block is cleaned and pickled preparatory to rejacketing, the rejacketing is in a frame comprising rails having a thickness in a direction normal to the plane of the major faces of the block equal approximately to the block thickness and of a width at least as great as the block thickness, and cover plates equal to one-half to four times the thickness of the block being rejacketed, and each cover plate extends outwardly beyond each peripheral face of the frame approximately one-half of the rail thickness, the channels defined by the outer peripheral edge faces of the frame and the adjacent faces of the plates outwardly therefrom being filled with weld metal.
- composition is disposed between the faces of the rejacketed block and the cover plates and rails, and also between the margins of the cover plates and the rail faces contacting said margins.
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- Engineering & Computer Science (AREA)
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Description
metallic jacket.
United States Patent 3,234,052 BERYLLIUM SHEET AND METHOD OF PRODUCING SAME Keith G. Wikle, Oak Harbor, Ohio, assignor to The Brush Itlelryllium Company, Cleveland, Ghio, a corporation of [0 No Drawing. Filed July 28, 1961, Ser. No. 127,505 13 Claims. (Cl. 148-115) This invention relates to a method of producing relatively large, flat sheets and plates of beryllium by rolling a beryllium billet while the billet is clad in a removable metal jacket.
The present invention is directed to the hot rolling of jacketed beryllium billets into the form of plates and sheets of substantial area and thickness, as distinguished from small sheets of foil, which generally are less than 0.005 inch in thickness, and thin metal coupons of small area. The sheets contemplated, range, for example, from 0.020" to 0.375 in thickness, from 20" to 36" in width, and from 60" to 96 in length. In order to disclose fully the advance made in the art by the present invention, the pertinent practices heretofore performed in forming beryllium are reviewed briefly.
The prior methods contemplated the forging of beryllium andalso the rolling of beryllium into coupons, foils, and shapes of limited area and thickness. There appears to be no prior method of rolling beryllium sheets and plates of substantial area and thickness.
A method disclosed in Creutz Patent No. 2,653,494, issued September 29, 1953, is directed to the forging of cast beryllium ingots and recognizes that unjacketed cast beryllium ingots cannot be forged at temperatures ranging from 500 C. to about 1200 C., without cracking, but that beryllium can be forged at temperatures in the neighborhood of 700 C. up to the melting point of the eutectic of beryllium and iron, if jacketed in a suitable The patent shows that at temperatures above the minimum melting eutectic point of beryllium and the jacket metal, the beryllium tends to fuse and alloy with the jacket material. To avoid this, refractory barrier material such as a layer of calcium oxide is interposed between the beryllium and jacket. The purpose of the jacket is to prevent oxidation of the beryllium at the elevated temperatures exceeding 865 C. which are required for forging beryllium into products having satisfactory mechanical and physical properties. The higher temperature is to obtain the extremely rapid flow of beryllium necessary for forging.
Another prior method is that disclosed in Macherey Patent No. 2,872,363, issued February 3, 1959. This method is concerned with the rolling of beryllium metal into foil. It contemplates starting with a'beryllium coupon of the thickness of about 0.004" and 2.5" x 2 and rolling the coupon to a thickness of about 0.002" at about 300 to 400 C., which are lower temperatures than used in Creutz. The beryllium is jacketed in a single jacket of stainless steel or is put between a folded sheet of stainless steel. Apparently, it was not considered necessary that the coupon be sealed to exclude outside air. The patent does not indicate any kind of barrier or non-oxidizing material is to be placed between the stainless steel and the beryllium coupon to prevent sticking. The method is not adapted for making sheets and plates of substantial size and thickness, but is limited rather specifically to the range of small coupons and foils, such as therein described.
In accordance with the present invention, it has been found that the results obtained in the rolling of beryllium billets into sheets of substantial area depend upon a number of factors, including the material used as the starting material for the rolling operation, the manner of enclosing the beryllium billets or partially formed sheets or plates in suitable jackets, and the steps and manner of initially seating the billet in the jacket, and of rolling, and in some instances, recladding, annealing, and subsequent rolling to the desired thickness. A most critical step is the initial cladding and the breakdown rolling step both as to the original billet and, if recladding is necessary, as to the newly reclad partially rolled beryllium.
In accordance with the present invention, the starting material is vacuum hot-pressed beryllium, preferably such as made in accordance with Dodds US. Patent No. 2,818,- 339, issued December 31, 1957. In accordance with this patent, the billet is formed first by combined heat and vacuum below sintering temperature for a predetermined period, followed by continuance of the vacuum and an increase of the temperature into the sintering range while maintaining the beryllium mass under pressure to compact it during sintering into a billet which is of substantially theoretical density, for example, about 1.85 grams per cubic centimeter. The billet selected should be free from cavities and variations in density and substantially free from occlusions. The surface should be free from voids and cracks.
This particular billet is preferred because it has random grain distribution, i.e., isotropic properties. It is preferred over other beryllium bodies which are extruded, cast, or otherwise formed which have anisotropic properties. Billets formed by well-known melting and casting techniques have too low a density and too large a grain size to permit their being formed into sheets of substantially theoretical density, which is the preferred sheet with which the present invention is concerned. The billet which is used as the starting material is generally a block or slab, a rectangular parallelepiped being preferred. The block is machined so that all faces are smooth and the corners and edges are ground or sanded to a very small radius, for example, about /s of an inch. It is cleaned to remove grease and foreign matter. As a result, it is true in shape yet free from abrupt, sharp corners and edges.
This block is coated with a thin film of parting COlIlpound. A suitable composition is colloidal graphite suspension, a form of which is sold on the market under the registered trademark Aquadag of which the Acheson Colloids Company, of Port Huron, Michigan, is the proprietor. Another suitable composition is a high-temperature graphite in water suspension available commercially under the registered trademark Triple C of which the Pro-Chem Company of Cleveland, Ohio, is the proprietor.
The parting compound is applied to the block in the form of a smooth coat, preferably by spraying or brushing an aqueous suspension thereof on the block with a spray gun or paint brush or the like, care being taken that no lumps are present, and then allowing the coating to dry. The coated block is then placed in a jacket of metal which has been similarly coated on the surfaces which are to contact the beryllium block. Such a metal jacket protects the beryllium from oxidation and confines it during the breakdown step of the rolling method employed. Preferably, the jacketing is effected by enclosing the peripheral edge faces of the block in a frame of rails formed of cold-rolled, mild steel bar stock of rectangular cross section. These rails have smooth planar faces adapted to engage the peripheral edge faces of the block. They are coated with the parting composition the same as the surfaces of the block. These rails are then clamped tightly in juxtaposition with the edge faces of the block and are welded together with mitered or butt joints, so that the block is confined peripherally.
The thickness of the rails, relative to the thickness of the block, in the breakdown rolling step, is critical. The
rails may be equal to, but must not exceed, the thickness of the block is generally about equal to the thickness of the block. The-interior'length and width of the frame as a whole are substantially equal to the like dimensions of the block itself.
With the block thus confined within the frame provided 1 by the rails, suitable cover plates are attached. The cover plates are of hot-rolled and pickled steel; for example,
commercial steel containing from 0.05 to 0.25%, by-
weight, of carbon generally .is' used. However, stiffer varieties of high strength-low alloy steel, suchas SAE 4140 steels, maybe used. Those faces of the cover plates which are to be juxtaposed against the block are smooth and, polished. This may be accomplished by sanding the faces free and smooth from oxide, scale, and pits, and
preferably by then polishing them with a fine sanding disc using 80C grits. Each plate is about one-half the thickness of the beryllium block and extends laterally and end- Wise of the frame a distance such that its peripheral edges are substantially flush with the outermost peripheral edges of the assembled rails. The inner faces of the cover plates are coated with the parting compound preparatory to applying them to the block. The plates are clamped in position and welded to the rails. are charnfered for Welding purposes at their junctures with Preferably, the rails the plates, and the welding is done by means of welding rod. Molten welding rod material is interposed to. fill up the chamfers so that the outer surfaces of the jacket define a rectangular parallelepiped.
A suitable vent is provided in the jacket to permit escape of the variousgase's and the like Preferably, it is formed in one of the side rails, usually the side rail which is to be in the trailing direction in the initial or breakdown rolling operation- One or more vent holes of about AV'in diameter are adequate for this purpose.
With the block jacketed as above described, the break-.
down rolling is initiated. For this purpose, the jacketed block assembly is heated to a temperature of from about 675 C. to about 860 0, about 760 C. being preferred.
Care is taken that the temperature is relatively uniform throughout.
The initial passes of the breakdown step are referred to herein as the seating passes and the first one of these is used to effect approximately 0.1 to 0.5% reduction in thickness of the block and may be accomplished under the mere weight of the upper'r'oll of the mill stand. This first pass is to compress the juxtaposed surfaces of the jacket and block throughout their extent into contact and conformitywith each other, thus assuring that the billet fills the jacket uniformly. The seating passes are prefer-.
ably bidimensional, comprising four successive passes in a rolling direction which is shifted progressively either:
counterclockwise or clockwise at 90 per pass.- As men-- tioned, the first of these passes causes 0.1 to 0.5% reduction in thickness of the block and may be effected-by the more weight of the upper roll of the mill stand. In
the next three passes, each reduction .is increased over" the preceding one from the 0.1 to 0.5% of the first pass up to a maximum of 10%, a reduction of from 6%- to 10% is preferred.
Breakdown rolling follows seating and may be unidimensional, alternating in direction of rolling 180 at suc-.
cessive passes, that is, rolling from one edge to 'the opposite edge, and then from said opposite edge to the one edge. .Passes subsequent toseatingcan approach maximum permissible reduction per pass of 15% of the thickness of the block at the start, of thepass, and as mentioned,-can be either unidirnensionalor bidimensional, thus alternating in direction per pass or .90'per pass. Usually unidimensional rolling is preferred.
An indefinite number of passes may be used in the breakdown rolling step, but if the overall thickness of the jacketed block is oneinch or more, the temperature should preferably remain about 760 C., and if the thickness is less thanone inch, then generally it is preferable to heat to 760 C. and employ one pass per heat.
The total reduction per pass during the breakdown rolling step should not be greater than15% nor less than 6% of the thickness of the beryllium metal existing *at the beginning-of the particular pass. reduction, regardless of the-number of passes, during the breakdown operation should not be greater than a maximum of 8:1 for any single .jacketing or cladding of the block.
Upon completion of the :breakdown rolling, the block is clad stress relieved in its original jacket. Preferably, this done'by raising it to a temperature of about 760 C. and holding it at that temperatureufor a period of about ten minutes after it is heated uniformly throughout, following which. the clad blockassembly is;.slow cooled in vermiculite to a temperature below red heat and preferably to about room temperature. latter temperature, the jacket is removed, either by torch cutting or otherwise, care being taken that the torch doesnot impinge upon the block and subjectthe beryllium metal to thermal shock which is aptto cause cracking and other deleterious effects.
After the original jacket has been removed from the.
block, the block is stress relieved, preferably by heating it to about 760 C., maintaining. thattemperature from about ten to aboutthirty minutesdependent upon the gauge -or thickness of the block. It is then slid from the furnace onto an asbestos board which allows it to lie flat. When it starts to lose color, it is turned over and after all color is gone,;it is stood on edge and allowed to cool to room. temperature If badly warped, 'it may be fiattened by heating it in the same manner and then placing it under pressure between hot or :insulated platens for about ten minutes, and then removing it from the platens and allowing it to cool as above.
Following the breakdown rolling',one or mofeaddi.
tional rolling operations may be provided and these are generally termed intermediate rolling operations. How-' ever, it is to be borne. in mind that the'number of these will be determined by the thickness of the starting block 1 and the thickness desired in the finished pieces Sometimes a single so-called intermediate rolling operation is all that is necessary.
After the block has been cooled following the stress relief, its surface. is cleaned by a lightsanding or by means of an abrasivewheel; or disc which removes the :parting compound. and surface oxides.
nitric acid and one-half of .one' percent sulfuric acid.
Abrasion and pickling of the surface is continueduntil thetsurfaceflis freefrom beryllium oxide. After final pickling, the plate is -fiu shed.with water. and allowed to 1 7 dry. Thereupon, the plate thus produced is cut;to-size 1 in any suitable manner, .such as by abrasive or band saws.
The edges are then sanded andabraded so as to remove.
sharp corners, preferably to a radius ofabont, of an inch, and the entire surface of the workpiece may be smoothed. if..desi-red "by grinding, polishing and the like.
It is :then spray coated-- with the parting compound. The
coating is applied smoothly and then allowed to. dry, and
the piece then enclosed in a frame, all as heretofore de-v scribed, with rails of athickness equal to approximately.
the block or slab thickness and of a width of approximate.
The total overall After it reaches the After. abrasive' cleaning of the clad-rolled beryllium surface,.the metal'is pickledv in an aqueous solution containing twenty-five: percent 1y one inch. Rails with square ends shall be used for a butt type frame for unidimensional rolling. Rails with mitered ends shall be used for bidimensional rolling. The faces of the rails facing the block and also those faces which will face the cover plates are then coated with the parting composition. The cover plates, prepared as here- 't-ofore described, and from one half to four times the thickness of the beryllium, are applied. The sheets have a width and length such that they extend beyond the outer peripheral edge face of the frame an amount equal to about one-half the thickness of the rails in a direction parallel to the plane of the major faces of the block. The plates, when clamped in this position, are then welded in place and the space between the outer edge of the frame and the overhanging margins of the cover plates is filled with molten welding material so that the outer surface of the jacketed piece is again substantially a rectangular parallelepiped. If the rails are one inch or more in thickness, they are chamfered and the mitered ends V-grooved and filled with the welding material. If the rails are less than one inch in thickness, this is not necessary. The trailing edge rail is vented.
For the intermediate rolling, the jacketed block is preheated uniformly to from about 650 C. to about 860 C., and preferably to 760 C., and the latter temperature maintained for an hour per inch overall thickness of the jacketed assembly to assure uniform heating. It is reheated between passes, if necessary, to provide and maintain a temperature ranging from about 650 C. to about 860 C. during rolling.
The initial pass effects a reduction of 0.1 to 0.5% which may be accomplished under the mere weight of the upper roll of the mill stand. The reduction effected in each of the next two seating passes is increased to approach the reduction employed in subsequent rolling passes. Reductions per pass, after the initial passes, shall not exceed nor be less than 6% of the beryllium metal thickness at the beginning of the pass. An overall reduction of 6:1 shall be the maximum for each cladding.
The intermediate rolling shall generally be unidimensional, alternating rolling directions 180 each pass. Bidimensional rolling will only be used in special cases. However, the intermediate slab rolling, when unidimensional, will generally be in a cross dimension, that is, a dimension 90 to the dimension in which the breakdown rolling was carried out. Generally, only one pass per heating is used so as to assure that the rolling temperature is not less than 650 C., and preferably is about 760 C., when the metal becomes relatively thin. Reduction less than the 6% lower and greater then the 15 upper critical limits described above results in defestive plates or sheets. If bidimensional rolling is used, then the intermediate rollingmay start in any direction, but preferably at right angles to the initial pass of the breakdown rolling operation. After the rolling operation, the jacketed sheet is clad stress relieved in the same manner as after the breakdown operation, usually heating it to about 760 C. for about ten minutes and cooling it in vermiculite. Thereafter, the jacket is removed.
As many intermediate rolling steps as required to reduce the sheet to the desired thickness may be employed. Furthermore, depending upon the desired reduction, the stock can be reclad and rolled any number of times until the final thickness is reached. The stock is bare stressrelieved when the jacket is removed prior to each recladding operation, followed \by clad stress relief of the assembly. After the final clad stress relief, and removal of the cladding material, the sheet is bare stress relieved, and also flattened, if required, as above described. Thereafter, it is cleaned by grinding and is pickled, as above mentioned, in an aqueous solution of nitric and sulfuric acid, following which it is dried and trimmed to size.
The following examples are illustrative of a preferred operation of the process of the invention and are not to be considered limiting thereof in any respect.
EXAMPLE 1 A beryllium billet of dimensions 0.770 x 13" X 16', vacuum hot pressed in accordance with the teachings of U.S. Patent No. 2,818,339, was encased in a picture frame assembly as h-ereinbefore described, the mild steel rails of the picture frame assembly were machined at their top edges so that their vertical height was about 0.005" less than the 0.770 vertical height of the beryllium billet. The mild steel covers were each about one half the thickness of the beryllium billet. The assembly was then welded together as described above, so that the beryllium billet was tightly sealed in the covered frame, the interior peripheral edge faces of the rails and the inner faces of the cover plates having been coated with Aquadag, an aqueous colloidal graphite suspension, prior to welding rails and cover plates into a unit assembly containing the beryllium block. The picture frame assembly was then heated to about 790 C. and passed through the rolls of a twohigh Mesta mill with the initial seating passes made under only the weight of the top roller of the two 30-inch wide rollers to properly seat the assembly. Four initial successive seating passes were made in a clockwise direction alternating 90 per pass. The heated assembly, while being maintained at a temperature of between 760 C. and 790 C., was then unidimensionally rolled to an overall reduction ratio of about 4.25:1. After completion of the breakdown rolling, the clad block was stress relieved at a temperature of about 760 C., maintained for about 10 minutes, and followed by cooling in vermiculite. The jacket assembly was removed by torch cutting. The dimensions of the beryllium block at this state of the operation were 0.178" x 47% x 18%". The clad-rolled beryllium plate was then bare stress-relieved for about 10 minutes at about 760 C. after which it was cooled to room temperature on a flat insulated surface. After being cooled, the plate was lightly sanded with sand and water to remove the parting compound and subsequently further sand cleaned alternated with pickling in an aqueous solution containing 25% nitric acid and 0.5% sulfuric acid until the surface was free from excessive oxides. The beryllium plate was then sawed in half to provide two plates each having the dimensions of 0.178" x '22 x 18%. The edges were then sanded to remove sharp corners and burrs. The surfaces of the plate adjacent to the frame were then coated with a composition of Aquadag and the top and bottom faces of the rails coated with chromium sesqui-oxide, and the coating dried. Each plate was then encased in a picture frame assembly in a similar manner as in the above breakdown rolling operation. In this case, however, the cover plates extended beyond the outer peripheral edge or face of the frame an amount equal to about one half the thickness of the rails in a direction parallel to the plane of the plate. The assembly was then uniformly heated to a temperature of 745 C. to 760 C. and unidimensionally rolled to an overall reduction ratio of 2.84:1, in a direction transverse to that of the breakdown roll-ing. The encased beryllium sheet after being clad-annealed, cooled, and removed from the jacket as in the above breakdown rolling step, had the dimensions of 0.06" x 22" x 53". The sheet was subequently bare stress relieved, sanded and pickled as in the breakdown rolling operation, and trimmed to dimensions of 0.055" x 22" x 50 /2". The beryllium sheet was then coated with Aquadag, the top and bottom edge faces coated with chromium sesqui-oxide, and the sheet encased in a picture frame assembly in the same manner as for the intermediate rolling operation, with the ex- Said stainless steel interleaves were unattached to and supported only by the welded assembly. The assembly was then uniformly heated to a temperature range of between about 745 C. to 760 C. and unidimensionally rolled to an overall reduction ratio of 1.275 :1 in the same direction as in the first above intermediate rolling operation, then clad stress relieved and removed from the jacket.
The sheet having the dimensions 0.045" x 22%;" X 64 was then cleaned by grinding and pickling and bare-annealed as in the first intermediate rolling step. The sheet after being trimmed to final dimensions of 0.040" x 20 X 40", had the properties noted below in Table I.
EXAMPLE 2 The same procedure was'followed as in Example 1 with the exception that the block used for breakdown rolling had the dimension 1.05 x 17" x 17 which after being subjected to an overall reduction ratio of 4.62-lhad the dimensions 0.222 x 19 ,5 x 68". This plate was sawed into three equal sections, and one section having the dimensions 0.222 x l9% x 22", after being reclad following the procedure of 'Example'lgwas rolled to an overall reduction ratio of'2.8:l to the dimensions of 0.076 x 55" X 22". This sheet was then trimmed to the dimensions of 0.076" X 46%" x 21 and clad in the aforedescribedpicbody, and thickness, and having sufficient strength and I rigidity for use in fabricatedstructures, as distinguished from foils of small size, and 'smallthin coupons having negligible strength for structural purposes, as disclosed in the prior art methods he'reinbefore described. Typical dimensions, physical and other properties of sheets made by the present process are shown in the examples. listed hereinbefore.
Having'thus described 'my' invention, I claim:
'1. ,In the method of making fiat beryllium sheets, the breakdown :rolling step comprising providing a beryllium blockof substan'tiallyi' theoretical density anduin the form of a right angled parallelepiped. of accurate .dimension'and having its opposite major faces and its'edge faces smooth and planar and its: corners and corner edges'roundedto a short radius, snugly embracing ;the block peripherally.
edgewise in a rigid frame of metal rails of which'the thickness 'norma'l'to the planes of 'the major facesof the block,
approximates butdoes not exceed that of the block, and which are welded securely togetherat their corners, providing on the block surfaces a coatingof a composition for reducing oxidation and facilitating parting, covering the major faces of the block and of the frame by applying to opposite major faces ofthe bl ockiand the-frame metal cove'rflplates which are substantially coextensive with the outer peripheral limits of the frame, bonding each .plate along its entire peripheral edge to the frame to form a Table I PROPERTIES OF GLAD-ROLLED AND GROUND BERYLLIUM SHEET Tensile Properties Surface Example Strain Ultimate Yield Propor- Hardness Density Direction of Rate Tensile Strength tional Percent Percent Modulus of Rockwell '(g./cc.)
Test (1n./in Strength 0.2% Limit Elonga- Reduction Elasticity B Scale (k.s.i.) Offset (k.s.i.) tion in Area (10 psi.)
(k.s.i.)
1 Longitudinal. 0. 0171 77. 4 56. 5 48. 8 16. 2 1'4. 2 41. 3 *71 1. 854 Transverse 0. 0138 74. 4 52. 2 41. 2 11. 7 11. 4 41. 7 *71 1. 854 2 {Longitudinal O. 0088 72. 2 58. 9 40. 9 7. 5 8. 2 41. 8 94 1. 86. Transverse 0.0085 75. 9 58. 3 44. 6 13. 2 12. 2 41.2 94 1. 86' 3 {Longitudinal 0. 0075 77. 8 56. 3 38. 3 1'4. 0 12. 2 1 42. 0 07 1. 858 Transverse 0.0097 75.6 52. 8 39. 5 16. 5' 15. 2 t 42. 3 97 1. 855
*Rockwell 451 Scale.
EXAMPLE 3 Following the procedureof Example 1, a block of the dimensions 0.755" x 17" x 17" was rolled to an overall reduction ratio of 3.211 to dimensions of 0.204" X 54 /8" x 19 /2. This plate was then heated, cleaned and pickled in accordance with the procedure of Example 1.. The
plate was then subjected to one intermediate rolling reduc tion at a ratio 4.95 :1 on a large Hyde Park two-high roll-. ing mill to final as-rolled dimensions of 0.0425 x 38 /2" X 96 This sheet was then trimmed and ground to the dimensions of 0.040" x 36" x 78". In this example, only one intermediate rolling step was required because of the large size of the Hyde Park 'rolling mill, and this example is representative of the process of the invention where only one intermediate rolling step is required. The final sheet product of Example 3 had the properties 'noted above, in Table I.
If desired, for the final rolling, two stainless steel sheets of 0.035" of the same. length and width as the block,-may' of metal may be removed from each face of the sheet, for
jacket, relief venting the jacket, thenihe'ating the block an'd;jacket assembly into a temperature rangeQOf about 650 C. to 860- C. uniformly 'throughout,'rolling the assembly while 'it' is within said temperature range with an initial pass under relatively lig-ht'pressure sufiicient to" cause the complementary surfaces of the jacket'and' block to be in firm-contact andplanar conformity with each other throughouttheir extent, then rolling, the assembly, while it is in saidrange, at a predetermined pressure to ture of about 760 C.
2. The step according to claim 1 wherein the side rails of the frame are from 0.005" to 0.030" less in thickness than the beryllium'block.
3. The step according to claim 1 wherein the composition is a colloidal graphite composition.
4.The' stepaccordingto claim 1 wherein the composition is chromium .sesq u'i-oxide.
5. The step according to claim 1 wherein the initial pass is followed by three successive passes in directions 90 apart from each other.
6. The method according to claim 5 wherein, after said initial and said three succeeding passes, the rolling is continued unidimensionally.
7. The step according to claim 5 wherein each of said successive passes provides a reduction from about 6% to about of the thickness of the beryllium block existing at the start of the particular pass.
8. The method according to claim 5 wherein after said initial and said three succeeding passes, the rolling is continued bidimensionally.
9. The method according to claim 1 wherein the block is rejacketed, the assembly rolled at a temperature in the range of 730 C. to 790 C. at a pressure to cause not more than an overall reduction ratio of 6:1 and stress relieved, then the block is dejacketed and bare stress relieved.
10. The method according to claim 1 wherein the bare stress relieved sheet does not exceed 0.08" in thickness, and the sheet is cleaned and reclad, then further reduced by hot rolling the assembly.
11. The method according to claim 9 wherein the rerolling is by an initial light pressure seating pass, followed by additional seating passes at greater pressure, and is carried out one reduction pass per heat, and the reduction per pass is from 6% to v 12. The method according to claim 1 wherein the block is cleaned and pickled preparatory to rejacketing, the rejacketing is in a frame comprising rails having a thickness in a direction normal to the plane of the major faces of the block equal approximately to the block thickness and of a width at least as great as the block thickness, and cover plates equal to one-half to four times the thickness of the block being rejacketed, and each cover plate extends outwardly beyond each peripheral face of the frame approximately one-half of the rail thickness, the channels defined by the outer peripheral edge faces of the frame and the adjacent faces of the plates outwardly therefrom being filled with weld metal.
13. The method according to claim 12 wherein composition is disposed between the faces of the rejacketed block and the cover plates and rails, and also between the margins of the cover plates and the rail faces contacting said margins.
References Cited by the Examiner UNITED STATES PATENTS 2/1959 Macherey 14811.5 XR
DAVID L. RECK, Primary Examiner,
RAY K. WINDHAM, Examiner.
G. HALL, H. F. SAITO, Assistant Examiners.
Claims (1)
1. IN THE METHOD OF MAKING FLAT BERYLLIUM SHEETS, THE BREAKDOWN ROLLING STEP COMPRISING PROVIDING A BERYLLIUM BLOCK OF SUBSTNATIALLY THEORETICAL DENSITY AND IN THE FORM OF A RIGHT ANLED PARALLELEPIPED OF ACCURATE DIMENSION AND HAVING ITS OPPOSITE MAJOR FACES AND ITS EDGE FACES SMOOTH AND PLANAR AND ITS CORNERS AND CORNER EDGES ROUNDED TO A SHORT RADIUS, SNUGLY EMBRACING THE BLOCK PERIPHERALLY EDGEWISE IN A RIGID FRAME OF METAL RAILS OF WHICH THE THICKNESS NORMAL TO THE PLANES OF THE MAJOR FACES OF THE BLOCK APPROXIMATES BUT DOES NOT EXCEED THAT OF THE BLOCK, AND WHICH ARE WELDED SECURELY TOGETHER AT THEIR CORNERS, PROVIDING ON THE BLOCK SURFACES A COATING OF A COMPOSITION FOR REDUCING OXIDATION AND FACILIATING PARTING, COVERING THE MAJOR FACES OF THE BLOCK AND OF THE FRAME BY APPLYING TO OPPSOSITE MAJOR FACES OF THE BLOCK AND THE FRAME METAL COVER PLATES WHICH ARE SUBSTANTIALLY COEXTENSIVE WITH THE OUTER PERIPHERAL LIMITS OF THE FRAME, BONDING EACH PLATE ALONG ITS ENTIRE PERIPHERAL EDGE TO THE FRAME TO FORM A JACKET, RELIEF VENTING THE JACKET, THEN HATING THE BLOCK AND JACKET ASSEMBLY INTO A TEMPERATURE RANGE OF ABOUT 650*C. TO 860*C. UNFORMLY THROUGHOUT, ROLLING THE ASSEMBLY WHILE IT IS WITHIN SAID TEMPERATURE RANGE WITH AN INITIAL PASS UNDER RELATIVELY LIGHT PRESSURE SUFFICIENT TO CAUSE THE COMPLETMENTARY SURFACES OF THE JACKET AND BLOCK TO BE IN FIRM CONTACT AND PLANAR COFORMITY WITH EACH OTHER THROUGHOUT THEIR EXTENT, THEN ROLLING THE ASSEMBLY, WHILE IT IS IN SAID RANGE, AT A PREDETERMINED PRESSURE TO CAUSE AN OVERALL REDUCTION RATIO NOT TO EXCEED 8:1, CHARACTERIZED IN THAT THE BREAKDOWN ROLLING STEP IS FOLLOWED BY STRESS RELIEVING THE ROLLED ASSEMBLY AT ABOUT 760*C., DEJACKETING THE STRESS RELIEVED BLOCK, CLEANING THE DEJACKETED BLOCK, AND BARE STRESS RELIEVEING IT AT A TEMPERATURE OF ABOUT 760*C.
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Cited By (6)
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US3317994A (en) * | 1964-08-19 | 1967-05-09 | Southwire Co | Method of conditioning metal for hot forming |
US3333994A (en) * | 1963-10-25 | 1967-08-01 | Commissariat Energie Atomique | Process for the manufacture of products of beryllium or beryllium alloy |
US3483047A (en) * | 1967-06-21 | 1969-12-09 | Us Air Force | Ductile polycrystalline beryllium |
US3657803A (en) * | 1970-07-17 | 1972-04-25 | Mallory & Co Inc P R | Method of making beryllium-aluminum-magnesium-silicon wrought material |
US3657804A (en) * | 1970-07-17 | 1972-04-25 | Mallory & Co Inc P R | Method of making beryllium-aluminum wrought material |
US5131958A (en) * | 1989-03-15 | 1992-07-21 | Ngk Insulators, Ltd. | Method of hot forming beryllium-copper alloy and hot formed product thereof |
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US2872363A (en) * | 1948-07-14 | 1959-02-03 | Robert E Macherey | Method of working beryllium |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3333994A (en) * | 1963-10-25 | 1967-08-01 | Commissariat Energie Atomique | Process for the manufacture of products of beryllium or beryllium alloy |
US3317994A (en) * | 1964-08-19 | 1967-05-09 | Southwire Co | Method of conditioning metal for hot forming |
US3483047A (en) * | 1967-06-21 | 1969-12-09 | Us Air Force | Ductile polycrystalline beryllium |
US3657803A (en) * | 1970-07-17 | 1972-04-25 | Mallory & Co Inc P R | Method of making beryllium-aluminum-magnesium-silicon wrought material |
US3657804A (en) * | 1970-07-17 | 1972-04-25 | Mallory & Co Inc P R | Method of making beryllium-aluminum wrought material |
US5131958A (en) * | 1989-03-15 | 1992-07-21 | Ngk Insulators, Ltd. | Method of hot forming beryllium-copper alloy and hot formed product thereof |
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