US2651099A - Method of rolling titanium sheets - Google Patents
Method of rolling titanium sheets Download PDFInfo
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- US2651099A US2651099A US196352A US19635250A US2651099A US 2651099 A US2651099 A US 2651099A US 196352 A US196352 A US 196352A US 19635250 A US19635250 A US 19635250A US 2651099 A US2651099 A US 2651099A
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- Prior art keywords
- titanium
- sheets
- rolling
- gauge
- sheet
- Prior art date
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- 239000010936 titanium Substances 0.000 title claims description 133
- 229910052719 titanium Inorganic materials 0.000 title claims description 133
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 title claims description 132
- 238000000034 method Methods 0.000 title claims description 30
- 238000005096 rolling process Methods 0.000 title description 45
- 238000010438 heat treatment Methods 0.000 claims description 45
- 239000000463 material Substances 0.000 claims description 32
- 229910052751 metal Inorganic materials 0.000 claims description 30
- 239000002184 metal Substances 0.000 claims description 30
- 230000003647 oxidation Effects 0.000 claims description 9
- 238000007254 oxidation reaction Methods 0.000 claims description 9
- 229910000831 Steel Inorganic materials 0.000 description 27
- 239000010959 steel Substances 0.000 description 27
- 238000005098 hot rolling Methods 0.000 description 7
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 6
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 6
- 229910052799 carbon Inorganic materials 0.000 description 6
- 230000003750 conditioning effect Effects 0.000 description 6
- 230000009467 reduction Effects 0.000 description 6
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 5
- 238000005242 forging Methods 0.000 description 5
- 238000004519 manufacturing process Methods 0.000 description 5
- 238000001816 cooling Methods 0.000 description 4
- 230000001143 conditioned effect Effects 0.000 description 3
- 229910052742 iron Inorganic materials 0.000 description 3
- 229910052757 nitrogen Inorganic materials 0.000 description 3
- 238000003303 reheating Methods 0.000 description 3
- 230000006698 induction Effects 0.000 description 2
- 229910001200 Ferrotitanium Inorganic materials 0.000 description 1
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- GWEVSGVZZGPLCZ-UHFFFAOYSA-N Titan oxide Chemical compound O=[Ti]=O GWEVSGVZZGPLCZ-UHFFFAOYSA-N 0.000 description 1
- 238000005275 alloying Methods 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- -1 basic steel sheets Chemical compound 0.000 description 1
- 238000005422 blasting Methods 0.000 description 1
- 238000005282 brightening Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- OJJLEPPNZOMRPF-UHFFFAOYSA-J dimagnesium;tetrachloride Chemical compound Cl[Mg]Cl.Cl[Mg]Cl OJJLEPPNZOMRPF-UHFFFAOYSA-J 0.000 description 1
- 229910052500 inorganic mineral Inorganic materials 0.000 description 1
- QWXYZCJEXYQNEI-OSZHWHEXSA-N intermediate I Chemical compound COC(=O)[C@@]1(C=O)[C@H]2CC=[N+](C\C2=C\C)CCc2c1[nH]c1ccccc21 QWXYZCJEXYQNEI-OSZHWHEXSA-N 0.000 description 1
- IXQWNVPHFNLUGD-UHFFFAOYSA-N iron titanium Chemical compound [Ti].[Fe] IXQWNVPHFNLUGD-UHFFFAOYSA-N 0.000 description 1
- YDZQQRWRVYGNER-UHFFFAOYSA-N iron;titanium;trihydrate Chemical compound O.O.O.[Ti].[Fe] YDZQQRWRVYGNER-UHFFFAOYSA-N 0.000 description 1
- 239000011777 magnesium Substances 0.000 description 1
- 229910052749 magnesium Inorganic materials 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 239000011707 mineral Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 238000005554 pickling Methods 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 229910000104 sodium hydride Inorganic materials 0.000 description 1
- 239000012312 sodium hydride Substances 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- OGIDPMRJRNCKJF-UHFFFAOYSA-N titanium oxide Inorganic materials [Ti]=O OGIDPMRJRNCKJF-UHFFFAOYSA-N 0.000 description 1
- XJDNKRIXUMDJCW-UHFFFAOYSA-J titanium tetrachloride Chemical compound Cl[Ti](Cl)(Cl)Cl XJDNKRIXUMDJCW-UHFFFAOYSA-J 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
- Y10T29/303—Method with assembling or disassembling of a pack
- Y10T29/304—Using transitory solid cover material
Definitions
- Titanium has been used Widely for many years 7 in the form of ferro-titanium or ferrocarbontitanium as a deoxidizing material in the manufacture of basic steel, because of its high afiinity for both oxygen and nitrogen. It also has been -.used as an alloying agentin steel and aluminum.
- Pure titanium ingots have only been available in weights ranging from 40 to 650 pounds and wound in shape, being produced either by are or induction melting of sponge titanium.
- Sponge v titanium is produced by separating the iron and titanium from ilmenite (iron-titanium ore) to form titanium oxide which is converted to titanium tetrachloride. u The latter, when redu'ced with molten magnesium, forms sponge titanium and magnesium tetrachloride.
- the nature of the discoveries and improvements in methods of rolling titanium sheets may be stated in general terms as preferably including the steps of providing pure titanium sheet bar as by forging or rolling the same from titanium ingots; conditioning the surfaces of the sheet bar; repeatedly heating and elongating the same by single-ply'rolling to heavy gauge sheet form; matching, reheating and rolling such sheets in pairs to further reduce and elongate the same; sandwiching such titanium sheets between basic steel sheets; and reheating and rolling such sandwich packs to desired gauge preferably accompanied by doubling.
- This slab was then cut in two to form two blanks 5" x 5 x 13",and one blank was subjected to three heating and forging steps to form a sheet bar x 12" x 3e", and the second blank was subjected to two heating and forging operations to reduce the same to a sheet bar of similar size.
- the five sheet bars thus forged from the 40# and 100# ingots were then surface conditioned by shot blasting and grinding over all, the ends thereof where not square being machined to provide square ends.
- the piece was thenreheated to 1580" F. and given two passes on the 3jhigh mill to elongate the same to about b'linches.
- the piece was then heated in a continuous pack heating furnace under a reducing (atmosphere with the furnace temperature maintained at approximately 1480" F. to
- the sheet was then sheared in half, matched inapair, and thepair heated in the continuous pack furnaee to; lii hflf Ffa ndgiven four passes on the Z-highhot mill to 74" x .059".
- the pack was then reheated and hot-doubled without roll- .ing and again reheated to 1350? R, and given four passes on theJ2-high hot mill, producing four sheets in the pack each .029 thick.
- the doubled endof the pack containing the four sheets was shearedaway, andthe four sheets matched with two ordinary or basic steel sheets of approximately the same size and gauge in a sandwich with the fourtitaniumsheets in the center and one basic steel sheetabove and another below the four titanium sheets.
- This sandwich pack was heatedin a continuous pack furnace to 1350 F. and given two passes on the Z-high hot mill to .023" gauge, then hot-doubled, reheated, and given twopasses on the 2-high mill.
- the eight tita niumand four steel sheets in the pack were then separated, the gauge of the eight titanium sheets therein being from .013" to .014".
- the finishing temperatureof the titanium sheets in the pack wasapproximately 1100 F. to 1150" F.
- metal temperaturezand given three single-ply passes on ax2-highyhot mill to an elongation of 80" and-a thickness of .'1-19, finishing at about 225 feet per'minute.
- Thesheet was sheared in half, matched in apairyandthe pair reheated to 1350 F.-in the continuous pack furnace and then given three passes on-the Z-high hot mill to 62" x .053.
- one ofthe" titanium sheets in the pack was sandwiched between twobasic steel sheets and reheated to 1350--F. and given-one pass on the 2-high hot mill and then hot-doubled, reheated, given two passes on the -2-highl1ot mill to .033" gauge, reheated to: 1350'-F.-,- and given two further passes on the Z-high hotmill to 71 X .020".
- the sheets in this pack were separated, producing two 71" x .020" titanium sheets and-four basic steel sheets.
- the other titanium sheet from the 624' x-.053" pair was similarly sandwiched between two basic steel sheets and reheated to 1350 F. and given two passes onthe 2-high'hot.-mill, then hotdoubled, reheated to 1350 and 'finishedr-with four passes on the 2-high hot millto 81 x .020", producing in the doubled" pack1tw0-81 x .020" titanium sheets and four basicfsteel sheets.
- Example I IJQ-A One of the 100# ingot sheet bars was similarly heated in a continuous bar heating furnace; under a reducing atmosphere to a l680 F. smetal temperature and given four passes on-a-3- high hot mill to a 22" elongation; with a 225-feet-perminute finishing speed. The piece was then reheated to 1480 F. and given four- :passes-on the 3-high mill-tc-van GIOIIgBItiQIIFOfAG: The-piece;
- Example 100-3 The second 100# ingotsheet bar was similarly heated in a continuous bar heating furnace under a reducing atmosphereto a 1550 F. metal.temperature'and given six'ppasseson a 3-high hot mill to an elongation of 32 with a 225-feet-perminute finishing speed. The piece was then reheated to 1500 F. and given four more passes 1 on the 3-highmill toan elongationof 57''. The piece was then takento a continuous pack heat- I ing' furnace where-it was heated under a reducing atmosphere to approximately 13505 1 metal temperature and given three single-ply passes on a 2-high hot mill to an elongation of 751'. and a --thickness of .134.
- the metal was heated to between 1700 F.
- Example IOU-A where temperatures of 1480 'F. to l550 F. were used. However, these temperatures did not damage the material since the brittleness occurring in Example IOU-A was because of the high carbon content of the titaniumrathrthan the high heating temperature. We believethat;itis'possible to heat titanium tothe temperature ranges set forth in the examples for hot rolling without damaging the material primarily because of the rapidity with which the material can be heated in continuous furnaces and of therapidity. with which the material was rolled on the 3-high and 2-high mills,
- theultimate essence of the present invention lies in the fact that sheets of a metal dissimilar to titanium, such as basic steel sheets,
- sandwich packs of the two dissimilar metal sheets may be repeatedly heated and rolled to desired gauge with the optimum number of passes as in Examples 40-1 and 40-3, or may be repeatedly heated and rolled accompanied by doubling asin Examples 40-1 and 40-3, or may be heated and rolled without doubling as in Example 40-2.
- one titanium sheet may be sandwiched between two sheets of a dissimilar metal as in Examples 40-2 and 40-3, or a plurality of titanium sheets may be sandwiched I between a plurality of sheets of a dissimilar metal ing; provides a procedure by which pure titanium .a. 91 i9na caexistinseprpb ems an stfic l encounteredin satisfying theneed for large size,
- the hot; rolled titanium sheets .made in the manner described may, afterannealing and pickling be cold rolled to lighter gauges in a usual manner to as much as 50% reduction when it-is desired to obtain cold rolled titanium sheet material, or when it, is desired to obtain titanium sheet material thinner than hot rolled titanium 1 sheet material which may be made in accordance with the presentinventi-on.
- the methodof hot rolling thin gauge titanium sheets including the steps of heating and rollingintermediate gauge titanium sheets from sheet bar, sandwiching at least one intermediate gauge titanium sheet between two sheets of a dissimilar metal having 'a lower heat conductivity than titanium to form a sandwich pack, heating 7 and rolling the pack to desired final titanium F. and rolling the pack to desired final titanium sheet gauge and protecting the titanium sheet material from rapid heat loss and excessive oxidation by the dissimilar metal sheets during heating and rolling of the sandwich pack to final titanium sheetgauge.
- the method of hot rolling thin gauge titanium sheets including the steps of rapidly heating titanium sheet bar to 1480 F. to 1680 F. and rapidly-rolling the same by a plurality of passes to elongate and thin the metal, rapidly reheating the material to about 1350 F., and iurtherrapidly rolling the same bysingle-ply passes to intermediate gauge; matching and rapidly heating and rolling the intermediate I gauge-material to further reduce the same; sandwiching at least one further reduced titanium sheet between two sheets of a dissimilar metal having lower heat conductivity than titanium to form a sandwich pack; rapidly heating and rolling the pack to desired final titanium sheet gauge, and protecting the titanium sheet material from rapid heat loss and excessive oxidation by the dissimilar metal sheets during heating and rolling of the sandwich pack to final titanium sheet gauge.
- the method of hot rolling thin gauge titanium sheets including the steps of rapidly heating titanium sheet bar to 1480 F. to 1680 F. and rapidly rolling the same by a plurality of passes to elongate and thin the metal, rapidly heating the material to about 1350 F. and further rapidly rolling the same by single-ply passes to intermediate gauge, matching and rapidly heating and rolling the intermediate gau ma erial t f r h r reduce the same, sandwiching at least one further reduced titanium sheet between two basic steel sheets having a lower heat conductivity than titanium to form a sandwich pack, repeatedly heating the pack to 1350 F. and rolling the same accompanied by hot doubling to desired titanium sheet gauge, and protecting the titanium sheet material from rapid heat loss and excessive oxidation by the steel sheets during heating and rolling of the sandwich pack to final titanium sheet auge.
- the method of hot rolling thin gauge titanium sheets including the steps of rapidly heating titanium sheet bar to 1480 F. to 1680" F. and rapidly rolling the same by a plurality of passes to elongate and thin the metal, rapidly heating the material to about 1350 F. and further rapidly rolling the same by single-ply passes to intermediate gauge, matching and rapidly heating and rolling the intermediate gauge material to further reduce the same, sandwiching a further reduced titanium sheet between two basic steel sheets having a lower heat conductivity than titanium to form a sandwich pack, reducing the pack to desired titanium sheet gauge by operations of heating to 1350 F. and rolling, and protecting the titanium sheet material from rapid heat loss and excessive oxidation by the steel sheets during heating and rolling of the sandwich pack to final titanium sheet gauge.
- the method of making hot rolled thin gauge titanium sheets from a titanium ingot including the steps of conditioning the ingot surfaces, repeatedly heatin the ingot to 1700 F. to 1850 F. and forming the same to sheet bar size, conditioning the surfaces of the bar, repeatedly heating and rolling the sheet bar to intermediate gauge titanium sheets, sandwiching at least one intermediate gauge titanium sheet between two basic steel sheets having a lower heat conductivity than titanium to form a sandwich pack, heating and rolling the pack to desired final titanium sheet gauge, and protecting the titanium sheet material from rapid heat loss and excessive oxidation by the steel sheets during heating and rolling of the sandwich pack to final titanium sheet gauge.
- the method of making hot rolled thin gauge titanium sheets from a titanium ingot including the steps of conditioning the ingot surfaces, repeatedly heating the ingot to 1700 F. to 1850 F. and working the same under pressure to form sheet bar, conditioning the surfaces of the sheet bar, repeatedly heating and rolling the sheet bar to intermediate gauge titanium sheets, sandwiching at least one intermediate gauge titanium sheet between two sheets of a dissimilar metal having a lower heat conductivity than titanium to form a sandwich pack, heating the pack to 1350 F. and rolling the same to desired titanium sheet gauge, and protecting the titanium sheet material from rapid heat loss and excessive oxidation by the dissimilar metal sheets during heating and rolling of the sandwich pack to final titanium sheet gauge.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Metal Rolling (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
Description
Y test purposes. been hot rolled into heavy gauge sheet on the sameequipment as used for stainless steel, but
- itself;
Patented Sept. 8, 1953 UNITED STATES PATENT OFFICE 2,651,099 METHOD OF ROLLING TITANIUM SHEETS James A. Roemer, Warren, Burt H. McKibben,
1 ,Niles, ;and Joseph R. Corry, Mineral Ridge,'
Ohio, assignors, by mesne'assignments, to Mallory-Sharon Titanium Corporation, Niles, Ohio,
a corporation of Delaware No Drawing. Application November 17, 1950, Serial No. 196,352
'physical and chemical propertiesparticularly its lightness in Weight, its strength, and its corrosion resistance-are manifold.
Titanium has been used Widely for many years 7 in the form of ferro-titanium or ferrocarbontitanium as a deoxidizing material in the manufacture of basic steel, because of its high afiinity for both oxygen and nitrogen. It also has been -.used as an alloying agentin steel and aluminum.
However, little actual experience has been had and little use. has been made of pure metallic titanium because of the present high cost of reducing the metal from ore to metallic form. As i a result, only extremely small quantities of pure -metallic titanium have been processed in an experimental manner to form small titanium bars and short, narrow sheet thickness sections for Some titanium is said to have such procedure is laborious and costly and does not provide light gauge, hot rolled titanium sheet material finished in sizes and gauges comparable to sheet steel for use in pressing, stamping, drawingor otherwise forming large sheet titanium components, parts or devices.
Pure titanium ingotshave only been available in weights ranging from 40 to 650 pounds and wound in shape, being produced either by are or induction melting of sponge titanium. Sponge v titanium is produced by separating the iron and titanium from ilmenite (iron-titanium ore) to form titanium oxide which is converted to titanium tetrachloride. u The latter, when redu'ced with molten magnesium, forms sponge titanium and magnesium tetrachloride.
The problem of rolling pure titanium into large size, thin gauge hot rolled sheets from such availtitanium when rolled tosheet form,which prevents it from being satisfactorily doubled, upon An approach-to the problem is further complicated by the. belief of those Who have I investigated the properties of titanium that the material could not beheated to a high enough ;;temperature,for obtaining those'reductions in hot rolling which are. necessary to produce large 12 Claims. (Cl. 29-9-19) 1 size, light gauge, titanium sheets without damaging the material.'-'
Another factor complicating the problem is the relatively high heat conductivity of pure titanium which results in rapid cooling of the heated material during rolling. This rapid cooling characteristic; in addition to the relatively low temperatures believed to be required for avoiding damage tothe material, has indicated that great difliculties would be encountered in obtaining desired reductions and uniformity of gauge in attempting to hot roll large size, light gauge, titanium sheets".
Notwithstanding these difficulties, we approached the problem from the standpoint of proper controls of rapid heating, rapid and extensive reductions, and surface protection against heat loss and excessive oxidation, and discovered that puretitanium sheets could be economically and satisfactorily rolled in sizes, for example, of 36" x 95" x .020 to 36" x 96" x .014", with satisfactory surfaces, free from mill marks, and with uniform gauge. I
Accordingly,-it is an object of the present invention to provide a method or procedure of rolling pure titanium into large size, thin gauge sheets of the orderof-36" x 96"- x .020" to 36" x 96" x .014".
Furthermore, it is an object of the present invention to provide a method or procedure of hot-rolling, pure-titanium to light gauge sheet form with relatively-high rolling temperatures protecting the material during'final-stages. of
reduction from rapid loss of heat and from excessive oxidation.
Also, it is an object of the present invention to provide a new method or procedure by which pure titanium'sheets'may be hot rolled economically with existing modern sheet mill equipment.
It is a further object of the present invention to advance the artby providing an economical method or procedure for the successful production of large-size, light gauge, ductile, pure titanium sheets while avoiding diificulties heretofore believed to be so inherently associated with titanium as to prevent the economicaland satisfactory Droduction'of such sheets.
- Finally,-it is an object of the-present invention to satisfy the existing need for large size,
light gauge, ductile, hot rolled, titanium sheets, to solve problems existing in the manufacture of the same, to eliminate difficulties believed to be inherent in this field, and to obtain the fore- P going advantages and desiderata in a simple. I
economical, and effective manner.
These and other objects andadvantages apparent to those skilled in the art from the following description and claims may be obtained, the stated results achieved, and the described difhculties overcome by the discoveries, methods, steps, operations and procedures which. comprise the present invention, the nature of which is set forth in the following general statement preferred procedural embodiments of which-illustrative of the best mode in which applicants have contemplated applying the principles-are set forth in the following description, and which are particularly and distinctly pointed out and set forth in the appended claims forming part hereof.
The nature of the discoveries and improvements in methods of rolling titanium sheets may be stated in general terms as preferably including the steps of providing pure titanium sheet bar as by forging or rolling the same from titanium ingots; conditioning the surfaces of the sheet bar; repeatedly heating and elongating the same by single-ply'rolling to heavy gauge sheet form; matching, reheating and rolling such sheets in pairs to further reduce and elongate the same; sandwiching such titanium sheets between basic steel sheets; and reheating and rolling such sandwich packs to desired gauge preferably accompanied by doubling.
By way of example, the improved methods and procedures of the present invention may be understood by reference to examples hereinafter described in detail. Three round, LO-pound, arcmelted, pure titanium ingots, 5 in diameter and 12 long and containing up to 99.24% tita nium and 36% carbon, after being surface con ditioned in the same manner as other metal ingots to remove scale and surface imperfections by turning, grinding, etc., were heated in a reducing atmosphere in a gas-fired furnace to approximately 1700" F. to 1800" F. metal temperature,-
and forged on a drop hammer to flatten the same. After the first forging operation, the surfaces of the blanks were reconditioned with chipping hammers and grinding wheels in a usual manner, and the blanks were reheated, further hammer forged, again reheated, and finally hammer forged to provide from each ingot one rectangular sheet bar approximately thick by 12" wide by 28" long.
One round, IOU-pound, induction-melted, pure.
titanium ingot,'8" in diameter and 14%;" long, and containing 98.5? titanium, 56% carbon, 22% iron, and 06% nitrogen, was similarly surface conditioned to remove scale and surface imperfections, and then heated in a reducing atmosphere to approximately 1750 F. to 1850 F, metal temperature, forged on a drop hammer, reheated, and further forged to form a 5 x 5" x 26" slab. This slab was then cut in two to form two blanks 5" x 5 x 13",and one blank was subjected to three heating and forging steps to form a sheet bar x 12" x 3e", and the second blank was subjected to two heating and forging operations to reduce the same to a sheet bar of similar size.
The five sheet bars thus forged from the 40# and 100# ingots were then surface conditioned by shot blasting and grinding over all, the ends thereof where not square being machined to provide square ends.
'4 Example: 40 1 One of the 40t ingot sheet bars was heated in a continuous bar heating furnace under a reduc- :-ing atmosphere to 1520 F. metal temperature and given six passes on a 3-high hot mill to elongate the 12"width of the slab to 43", with a finishing speed of about 225 feet per minute. The
piece was thenreheated to 1580" F. and given two passes on the 3jhigh mill to elongate the same to about b'linches. The piece Was then heated in a continuous pack heating furnace under a reducing (atmosphere with the furnace temperature maintained at approximately 1480" F. to
approximately 1350 F. metal temperature and given two single-ply passes on a 2-high hot sheet mill to elongate the piece to 74" long by ,115 thick, finishing at a speed of about 225 feet per minute.
The sheet was then sheared in half, matched inapair, and thepair heated in the continuous pack furnaee to; lii hflf Ffa ndgiven four passes on the Z-highhot mill to 74" x .059". The pack was then reheated and hot-doubled without roll- .ing and again reheated to 1350? R, and given four passes on theJ2-high hot mill, producing four sheets in the pack each .029 thick. The doubled endof the pack containing the four sheets was shearedaway, andthe four sheets matched with two ordinary or basic steel sheets of approximately the same size and gauge in a sandwich with the fourtitaniumsheets in the center and one basic steel sheetabove and another below the four titanium sheets. This sandwich pack was heatedin a continuous pack furnace to 1350 F. and given two passes on the Z-high hot mill to .023" gauge, then hot-doubled, reheated, and given twopasses on the 2-high mill. The eight tita niumand four steel sheets in the pack were then separated, the gauge of the eight titanium sheets therein being from .013" to .014". The finishing temperatureof the titanium sheets in the pack wasapproximately 1100 F. to 1150" F.
During some of the later rolling steps on the V Z-high hot mill, gasflames were impinged on the rolls in an attempt to keep the rolls as hot as possible to prevent cooling of the titanium sheets during rolling.
We discovered in carrying out the foregoing procedure in rolling titaniumto sheets as thin as .013-014" thick, that excellent metal surfaces resulted on the titanium sheets, with little oxide formed thereon and no mill marks, and the gauge of each sheet was substantially uniform throughout. We further discovered in separating the sheets in the pack that; the titanium sheets did not stick to'the basic steel sheets between which the titanium shects wre sandwiched, and that the titanium sheets did not stick to each other.
W also discovered that the lower heat conductivity of the steel sheets between which the titanium sheetswere sandwiched held heat in the titanium sheets longer and enabled more elongation of the titanium sheets in the pack in one heating than could have otherwise been obtained. Furthermore, the relatively high rollin temperaturesused'in rolling the titanium sheets enabled the necessary elongation to take place required for producing titaniumsheets'as thin as .013- .014" thick.
Also, the sandwiching of the titanium sheets between the basic steel sheets, in the later stages high temperaturesused.
hot mill to an'elongation of ,73
under a reducing atmosphere to la 1580 FL metal" temperature and givensix passes ona 3;]rii'gh hot mill to an elongation of $91, with a 225-feetper-minute finishing speed. The-piece was then taken to a continuous pack heating furnace where it was, heated, under a receding arm es-' phere o a m me ely B twesterne ature and given twosingle-ply, passeson a z high c. 9 3 hickee of 122"; finishing t.abqui2 51esL 9rm'm The sheet was sheared in halL-matched in a pair, and the pair reheated to l 3 50ffi. in the continuous pack furnace, and then given three s e th .ziehh g i 'tq.6 1122. 11
At t s a es-ti .ot.j h .ten u i hee s. in
t e a kw s 11 1 9 orte-Ste...ansitlieethe tit nium sheet was matchedwith and ';sandw i ched between two'basic steel sheets and reheated to 1350 F., and given three passesgon the Z high hot mill, finishing, the titaniurn sheet at 18". x
. 4 The s e v th a'qk weresen rat kr u ng o t t n um's eet andtw basicf sheets.
. mpl 1 -3 The third 40'# ingot sheet at was similarly heated in acontinuous bar heating furnace under a reducing atmosphere toa 1520 ;F'.-:metal temperature and given four passeson-a-3-high hot mill to an elongation of 22",witha'225-feet-perminute finishing speed. 'I'hepiece-wasjthenreheated to 1550 F. and given twoiipasses to an elongation of 40". The piece was: then taken to a continuous pack heating'furnacewhere it was heated under a reducing atmosphere to approximately 1350 F. metal temperaturezand given three single-ply passes on ax2-highyhot mill to an elongation of 80" and-a thickness of .'1-19, finishing at about 225 feet per'minute. Thesheet was sheared in half, matched in apairyandthe pair reheated to 1350 F.-in the continuous pack furnace and then given three passes on-the Z-high hot mill to 62" x .053.
At this stage; one ofthe" titanium sheets in the pack was sandwiched between twobasic steel sheets and reheated to 1350--F. and given-one pass on the 2-high hot mill and then hot-doubled, reheated, given two passes on the -2-highl1ot mill to .033" gauge, reheated to: 1350'-F.-,- and given two further passes on the Z-high hotmill to 71 X .020". The sheets in this pack were separated, producing two 71" x .020" titanium sheets and-four basic steel sheets. v
The other titanium sheet from the 624' x-.053" pair was similarly sandwiched between two basic steel sheets and reheated to 1350 F. and given two passes onthe 2-high'hot.-mill, then hotdoubled, reheated to 1350 and 'finishedr-with four passes on the 2-high hot millto 81 x .020", producing in the doubled" pack1tw0-81 x .020" titanium sheets and four basicfsteel sheets.
Example I IJQ-A One of the 100# ingot sheet bars was similarly heated in a continuous bar heating furnace; under a reducing atmosphere to a l680 F. smetal temperature and given four passes on-a-3- high hot mill to a 22" elongation; with a 225-feet-perminute finishing speed. The piece was then reheated to 1480 F. and given four- :passes-on the 3-high mill-tc-van GIOIIgBItiQIIFOfAG: The-piece;
was then taken to a continuous pack heatin assua e 6 I- furnace where it was heated under a reducing atmosphere to approximately 1480 F. and given I three single-ply passes on a- Z-highhotmill to an elongation of 70" and a thickness of .118".
The sheet was sheared in half, matched in a pair,- and the pair reheated to 1550 F. in a continuous pack furnace, and then given four passes on the 2-high hot mill to 62 x .070". These titanium sheets at this stage were so brittle with 10 no ductility thatno attempt was made to roll them further. 7 r t 'It was impossible at this time to determine accurately whether the higher heating temperaturesor the higher carbon, -iron,-and nitrogen in the original induction melted ingot were responsible'for these brittleness and lack of ductility characteristics; 1 v
v I Example 100-3 The second 100# ingotsheet bar was similarly heated in a continuous bar heating furnace under a reducing atmosphereto a 1550 F. metal.temperature'and given six'ppasseson a 3-high hot mill to an elongation of 32 with a 225-feet-perminute finishing speed. The piece was then reheated to 1500 F. and given four more passes 1 on the 3-highmill toan elongationof 57''. The piece was then takento a continuous pack heat- I ing' furnace where-it was heated under a reducing atmosphere to approximately 13505 1 metal temperature and given three single-ply passes on a 2-high hot mill to an elongation of 751'. and a --thickness of .134. The sheetwas sheared in -"half, matched in-arpair, and the pair reheated to l350 F. in the continuous'pack furnace and then -given five passes on-the 2-high mill to .7 m 1361" v H .Hereagain, the titanium sheets were so brittle and lackin in ductility that no further rolling 40 was performed. Since these titanium sheets originated-from the-same ingot as the titanium sheets produced in Example 100-A, but 7 were heated and rolledwith temperatures and passes comparable to and on'the same equipment as the sheets rolled in Examples 40-1, 40-2,-and 40-3,
. it 'is believed, that the higher carbon'content in the 100# ingot was responsible for the brittle- .ness andlack. of ductility. 7
All of the sheetsroller from the 4c# arc-melted ingots having low carbon contents, were ductile @and could be welded;--
Although very little scale. or oxide was formed on the titanium sheets rolled-in the sandwiched packs, yetthe slight amount ofscale that did .form was very hard and tight but could be removed following heat treatment, including heati sing-to 1300 F. and-air cooling, by de-scaling in a-molten-sodium hydride bath followed by a nitric hydrofluoric acid-brightening dip, and finishing with a flattening pass on-a Z-high cold mill.
The titanium sheetsrolled in the sandwiched packs tested 104 Rockwell B-Scale hardness,
' while the basic steel sheets in said packs tested :.65-75 Rockwell B-Scale hardness. V
In forging the titanium ingots .to formsheet bar, the metal was heated to between 1700 F.
. and 1800- F. causing scaling which was removed .from the forged pieces by the surface conditioning operations. However, the ability to heat the sheet bar to froml520" F. to 1580.F., as in EX- amples 40-1, 40-2, and 40-3, and toas high as 1680 F. inExample 100-A, without damaging the-material, -,was a totally unexpected, result since those skilled inthe art indicate that 1300 ,-ra sinsecliptic umshtit nium can Safely ;'b .heais rrol in s. ndi ated in hes mplc t higher heating took place in the continuous bar furnace for lieating the sheet bar, and a somewhat lower metal temperature of about 1350" F. (also above the indicated safe 1300 F. temperature) was used in heating in the continuous pack furnace,
excepting in Example IOU-A where temperatures of 1480 'F. to l550 F. were used. However, these temperatures did not damage the material since the brittleness occurring in Example IOU-A was because of the high carbon content of the titaniumrathrthan the high heating temperature. We believethat;itis'possible to heat titanium tothe temperature ranges set forth in the examples for hot rolling without damaging the material primarily because of the rapidity with which the material can be heated in continuous furnaces and of therapidity. with which the material was rolled on the 3-high and 2-high mills,
finishing atspeeds of 225Ifeet per minute. Since a reducing atmosphere was maintained in the continuous furnaceslittle or, no scaling occurred therein, and the rapid rolling accomplished the necessary reductions to obtain the thin gauge' finished sheets of the order of .020" to .013" in thickness before any-damage to the material could occur as aresult of-the initially high temperaturesto which the material was heated for rolling.
We believe further-that it would be impossible to reduce'the material to such thin sheet gauges using the' high rolling temperatures, without finishing at metal temperatures of the order of 1 100 F, to 1150 F., and without sandwichingindividual or multiple titanium sheets between basic steel sheets not only to protect the titanium sheet surfaces inthe final rolling operations, but also to retain high heating temperatures during rolling.
Thus, theultimate essence of the present invention lies in the fact that sheets of a metal dissimilar to titanium, such as basic steel sheets,
, are used to form a sandwich pack with the dissimilar metal sheets on the outside of the pack in completing the rolling of titanium sheets to form large size, thin gauge titanium sheets. These sandwich packs of the two dissimilar metal sheets may be repeatedly heated and rolled to desired gauge with the optimum number of passes as in Examples 40-1 and 40-3, or may be repeatedly heated and rolled accompanied by doubling asin Examples 40-1 and 40-3, or may be heated and rolled without doubling as in Example 40-2. Furthermore, one titanium sheet may be sandwiched between two sheets of a dissimilar metal as in Examples 40-2 and 40-3, or a plurality of titanium sheets may be sandwiched I between a plurality of sheets of a dissimilar metal ing; provides a procedure by which pure titanium .a. 91 i9na caexistinseprpb ems an stfic l encounteredin satisfying theneed for large size,
light gauge, ductile-hot rolled, titanium sheets in a simple,- economical and effective manner.
The hot; rolled titanium sheets .made in the manner described may, afterannealing and pickling be cold rolled to lighter gauges in a usual manner to as much as 50% reduction when it-is desired to obtain cold rolled titanium sheet material, or when it, is desired to obtain titanium sheet material thinner than hot rolled titanium 1 sheet material which may be made in accordance with the presentinventi-on.
In the foregoing description, certain terms have been used for-brevity, clearness and understanding; but no -unnecessary limitations areto be implied therefrom-beyond the requirements of the prior art, because such terms are utilized for descriptive purposes hereinand not for the purpose of limitation and ,are intended to be broadly construed.
- Moreover, the description of the improvements is by way of example, and the scope of the present invention isnot limited .tothe exactdetails described nor to the specific examples set forth.
Having now described the features, discoveries and principles of the invention, the methods and procedures comprehended, the characteristics of theproducts produced thereby, and the advantageous, new and useful results obtained; the new and useful discoveries, methods, steps, operations, procedures and principles, and mechanical equivalents obvious to those skilled in the art, are set forth in the appended claims.
- We claim:
1. The methodof hot rolling thin gauge titanium sheets including the steps of heating and rollingintermediate gauge titanium sheets from sheet bar, sandwiching at least one intermediate gauge titanium sheet between two sheets of a dissimilar metal having 'a lower heat conductivity than titanium to form a sandwich pack, heating 7 and rolling the pack to desired final titanium F. and rolling the pack to desired final titanium sheet gauge and protecting the titanium sheet material from rapid heat loss and excessive oxidation by the dissimilar metal sheets during heating and rolling of the sandwich pack to final titanium sheetgauge.
3. The method of hot rolling thin gauge titanium sheets including the steps of rapidly heating titanium sheet bar to 1480 F. to 1680 F. and rapidly-rolling the same by a plurality of passes to elongate and thin the metal, rapidly reheating the material to about 1350 F., and iurtherrapidly rolling the same bysingle-ply passes to intermediate gauge; matching and rapidly heating and rolling the intermediate I gauge-material to further reduce the same; sandwiching at least one further reduced titanium sheet between two sheets of a dissimilar metal having lower heat conductivity than titanium to form a sandwich pack; rapidly heating and rolling the pack to desired final titanium sheet gauge, and protecting the titanium sheet material from rapid heat loss and excessive oxidation by the dissimilar metal sheets during heating and rolling of the sandwich pack to final titanium sheet gauge.
4. The method of hot rolling thin gauge titanium sheets including the steps of rapidly heating titanium sheet bar to 1480 F. to 1680 F. and rapidly rolling the same by a plurality of passes to elongate and thin the metal, rapidly heating the material to about 1350 F. and further rapidly rolling the same by single-ply passes to intermediate gauge, matching and rapidly heating and rolling the intermediate gau ma erial t f r h r reduce the same, sandwiching at least one further reduced titanium sheet between two basic steel sheets having a lower heat conductivity than titanium to form a sandwich pack, repeatedly heating the pack to 1350 F. and rolling the same accompanied by hot doubling to desired titanium sheet gauge, and protecting the titanium sheet material from rapid heat loss and excessive oxidation by the steel sheets during heating and rolling of the sandwich pack to final titanium sheet auge.
5. The method of hot rolling thin gauge titanium sheets including the steps of rapidly heating titanium sheet bar to 1480 F. to 1680" F. and rapidly rolling the same by a plurality of passes to elongate and thin the metal, rapidly heating the material to about 1350 F. and further rapidly rolling the same by single-ply passes to intermediate gauge, matching and rapidly heating and rolling the intermediate gauge material to further reduce the same, sandwiching a further reduced titanium sheet between two basic steel sheets having a lower heat conductivity than titanium to form a sandwich pack, reducing the pack to desired titanium sheet gauge by operations of heating to 1350 F. and rolling, and protecting the titanium sheet material from rapid heat loss and excessive oxidation by the steel sheets during heating and rolling of the sandwich pack to final titanium sheet gauge.
6. The method set forth in claim 3 in which the matched intermediate gauge titanium material prior to sandwiching is heated to 1350 F., hot-doubled, reheated to 1350 F., rolled in doubled condition and sheared to remove the doubled end; and in which the four intermediate gauge titanium sheets thus produced are sandwiched between two basic steel sheets to form the sandwich pack.
'7. The method set forth in claim 4 in which the matched intermediate gauge titanium material prior to sandwiching is heated to 1350 F., hot-doubled, reheated to 1350 F., rolled in doubled condition and sheared to remove the doubled end; in which the four intermediate auge titanium sheets thus produced are sandwiched between the two basic steel sheets to form the sandwich pack; and in which the sandwich pack is heated to 1350 F., rolled by a plurality of passes, heated to 1350 F. and hot-doubled, reheated to 1350 F. and rolled by a plurality of passes to desired titanium sheet gauge.
8. The method set forth in claim 4 in which one intermediate gauge titanium sheet is sandwiched between two basic steel sheets to form the sandwich pack; and in which the sandwich pack by a plurality of 1 is heated to 1350 F., rolled, heated to 1350 F. and hot-doubled, reheated to 1350 F. and rolled by a plurality of passes to desired titanium sheet gauge.
9. The method set forth in claim 5 in which the sandwich pack of one titanium sheet and two basic steel sheets is heated to 1350 F. and rolled passes to desired final titanium sheet gauge.
10. The method of making hot rolled thin gauge titanium sheets from a titanium ingot including the steps of conditioning the ingot surfaces, repeatedly heatin the ingot to 1700 F. to 1850 F. and forming the same to sheet bar size, conditioning the surfaces of the bar, repeatedly heating and rolling the sheet bar to intermediate gauge titanium sheets, sandwiching at least one intermediate gauge titanium sheet between two basic steel sheets having a lower heat conductivity than titanium to form a sandwich pack, heating and rolling the pack to desired final titanium sheet gauge, and protecting the titanium sheet material from rapid heat loss and excessive oxidation by the steel sheets during heating and rolling of the sandwich pack to final titanium sheet gauge.
11. The method as set forth in claim 10 in which the sheet bar is rapidly heated to 1480 F. to 1680 F. and rapidly rolled by a plurality of passes to elongate and thin the same, then reheated to about 1350 F. and further rapidly rolled by single-ply passes to intermediate gauge, and then matched and rapidly heated and rolled; and in which the sandwich pack is rapidly heated to 1350 F. and rolled to desired final titanium sheet gauge.
12. The method of making hot rolled thin gauge titanium sheets from a titanium ingot including the steps of conditioning the ingot surfaces, repeatedly heating the ingot to 1700 F. to 1850 F. and working the same under pressure to form sheet bar, conditioning the surfaces of the sheet bar, repeatedly heating and rolling the sheet bar to intermediate gauge titanium sheets, sandwiching at least one intermediate gauge titanium sheet between two sheets of a dissimilar metal having a lower heat conductivity than titanium to form a sandwich pack, heating the pack to 1350 F. and rolling the same to desired titanium sheet gauge, and protecting the titanium sheet material from rapid heat loss and excessive oxidation by the dissimilar metal sheets during heating and rolling of the sandwich pack to final titanium sheet gauge.
JAMES A. ROEMER. BURT H. McKIBBEN. JOSEPH R. CORRY.
References Cited in the file of this patent UNITED STATES PATENTS Name Date Parrock June 21, 1930 OTHER REFERENCES Number
Claims (1)
1. THE METHOD OF HOT ROLLING THIN GAUGE TITANIUM SHEETS INCLUDING THE STEPS OF HEATING AND ROLLING INTERMEDIATE GAUGE TITANIUM SHEETS FROM SHEET BAR, SANDWICHING AT LEAST ONE INTERMEDIATE GUAGE TITANIUM SHEET BETWEEN TWO SHEETS OF A DISSIMILAR METAL HAVING A LOWER HEAT ONE INTERMEDIATE THAN TITANIUM TO FORM A SANDWICH PACK, HEATING AND ROLLING THE PACK TO DESIRED FINAL TITANIUM SHEET GAUGE, AND PROTECTING THE TITANIUM SHEET MATERIAL FROM RAPID HEAT LOSS AND EXCESSIVE OXIDATION BY THE DISSIMILAR METAL SHEETS DURING HEATING AND ROLLING OF THE SANDWICH PACK TO FINAL TITANIUM SHEET GAUGE.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US196352A US2651099A (en) | 1950-11-17 | 1950-11-17 | Method of rolling titanium sheets |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US196352A US2651099A (en) | 1950-11-17 | 1950-11-17 | Method of rolling titanium sheets |
GB1748353A GB740408A (en) | 1953-06-24 | 1953-06-24 | Method of rolling titanium sheets |
Publications (1)
Publication Number | Publication Date |
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US2651099A true US2651099A (en) | 1953-09-08 |
Family
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US196352A Expired - Lifetime US2651099A (en) | 1950-11-17 | 1950-11-17 | Method of rolling titanium sheets |
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Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2985945A (en) * | 1954-02-12 | 1961-05-30 | Crucible Steel Co America | Pack rolling |
US2997784A (en) * | 1958-10-21 | 1961-08-29 | Lukens Steel Co | Method of making composite metal articles and parting compound for same |
US3066384A (en) * | 1958-06-18 | 1962-12-04 | United States Steel Corp | Method of making wide flat sheets |
US5121535A (en) * | 1988-12-14 | 1992-06-16 | Sulzer Bros. Ltd. | Method for production of thin sections of reactive metals |
US5127146A (en) * | 1988-12-14 | 1992-07-07 | Sulzer Brothers, Ltd. | Method for production of thin sections of reactive metals |
US5903813A (en) * | 1998-07-24 | 1999-05-11 | Advanced Materials Products, Inc. | Method of forming thin dense metal sections from reactive alloy powders |
US20060157543A1 (en) * | 2004-11-10 | 2006-07-20 | Stanley Abkowitz | Fine grain titanium-alloy article and articles with clad porous titanium surfaces |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1744670A (en) * | 1927-03-18 | 1930-01-21 | Harry P Parrock | Production of strip steel |
-
1950
- 1950-11-17 US US196352A patent/US2651099A/en not_active Expired - Lifetime
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1744670A (en) * | 1927-03-18 | 1930-01-21 | Harry P Parrock | Production of strip steel |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2985945A (en) * | 1954-02-12 | 1961-05-30 | Crucible Steel Co America | Pack rolling |
US3066384A (en) * | 1958-06-18 | 1962-12-04 | United States Steel Corp | Method of making wide flat sheets |
US2997784A (en) * | 1958-10-21 | 1961-08-29 | Lukens Steel Co | Method of making composite metal articles and parting compound for same |
US5121535A (en) * | 1988-12-14 | 1992-06-16 | Sulzer Bros. Ltd. | Method for production of thin sections of reactive metals |
US5127146A (en) * | 1988-12-14 | 1992-07-07 | Sulzer Brothers, Ltd. | Method for production of thin sections of reactive metals |
US5903813A (en) * | 1998-07-24 | 1999-05-11 | Advanced Materials Products, Inc. | Method of forming thin dense metal sections from reactive alloy powders |
US20060157543A1 (en) * | 2004-11-10 | 2006-07-20 | Stanley Abkowitz | Fine grain titanium-alloy article and articles with clad porous titanium surfaces |
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