CA2003244C - Method of manufacturing seamless tube formed of titanium material - Google Patents
Method of manufacturing seamless tube formed of titanium materialInfo
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- CA2003244C CA2003244C CA 2003244 CA2003244A CA2003244C CA 2003244 C CA2003244 C CA 2003244C CA 2003244 CA2003244 CA 2003244 CA 2003244 A CA2003244 A CA 2003244A CA 2003244 C CA2003244 C CA 2003244C
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Abstract
A method of manufacturing a seamless tube formed of a titanium material, such as pure titanium or titanium alloys, by the use of the Mannesmann's method. At first, an ingot formed of the titanium material is processed under the con-ditions that a heating temperature is 850 to 1,250 °C, the final temperature being 600 to 1,100 °C, and a working degree being 50 % or more to be turned into a solid billet.
The resulting solid billet is subjected to a piercing within a temperature range of .beta. transus - 100 to 1,250 °C to be turned into a hollow piece. In this piercing process, in-clined rolls of a piercer are descaled. The resulting hol-low piece is in case of need regulated a size thereof sub-jected to an elongating to be turned into a hollow shell.
Subsequently, the resulting hollow shell is subjected to a reducing (reducing conditions: temperature at an inlet side of the mill is 600 to 1,100 °C and a reduction of outside diameter is 80 % or more) by means of a reducer mill or to a sizing (sizing conditions: temperature at an inlet side of the mill is 550 to 1,150 °C and a reduction of outside diameter is 3 to 15 %) by means of a sizer mill.
The resulting solid billet is subjected to a piercing within a temperature range of .beta. transus - 100 to 1,250 °C to be turned into a hollow piece. In this piercing process, in-clined rolls of a piercer are descaled. The resulting hol-low piece is in case of need regulated a size thereof sub-jected to an elongating to be turned into a hollow shell.
Subsequently, the resulting hollow shell is subjected to a reducing (reducing conditions: temperature at an inlet side of the mill is 600 to 1,100 °C and a reduction of outside diameter is 80 % or more) by means of a reducer mill or to a sizing (sizing conditions: temperature at an inlet side of the mill is 550 to 1,150 °C and a reduction of outside diameter is 3 to 15 %) by means of a sizer mill.
Description
TITLE OF THE INVENTION
METHOD OF MANUFACTURING SEAMLESS TUBE
FORMED OF TITANIUM MATERIAL
BACKGROUND OF THE INVENTION
Field of the Invention The present invention relates to a method of manu-facturing a seamless tube formed of titanium materials including pure titanium and titanium alloys by the use of the Mannesmann's method.
Description of Related Art The titanium materials are classified into pure tita-nium and the titanium alloys such as a-type titanium alloys, and +~-type titanium alloys and ~-type titanium alloys. The a-type titanium alloys include Ti-0.15Pd, Ti-0.8Ni-0.3Mo, Ti-5Al-2.5Sn and the like. The a+~-type titanium alloys include Ti-8Al-lMo-lV, Ti-3Al-2.5V, Ti-6Al-4V, Ti-6Al-6V-2Sn, Ti-6Al-2Sn-4Zr-6Mo, Ti-6Al-2Sn-4Zr-2Mo and the like such as small amount of platinum group elements added alloys and platinum group elements plus small amount of Ni, Co, W, Mo added alloys. The ~-type titanium alloys include Ti-3Al-8V-6Cr-4Mo-4Zr and the like. In the present invention, the titanium materials used as subject materials are a general name of the above-mentioned all type of tita-20Q~
nium alloys. Pure titanium is a titanium material whichmainly has impurities such as H, O, N, Fe, its charac-teristic is changed according to quantity of O and Fe in particular.
These titanium materials are light and highly cor-rosion-resistant and in partlcular a seamless tube formed of them has been expected to be used for a piping for use in chemical plant, an oil pressure piping for use in aircraft, and an oil field piping.
The seamless tube has been manufactured by the extru-sion method or Mannesmann's method. The extrusion method is suitable for manufacturing a tube of materials inferior in workability, but inferior in manufacturing efficiency. On the contrary, Mannesmann's method is superior in manufactur-ing efficiency, but requires materials superior in work-ability.
Some trials for manufacturing a tube formed of a titanium material by Mannesmann's method have been per-formed, but manufacturing technique for obtaining a good tube in quality has not established yet (Reference:
"Titanium And Titanium Alloys" volume 1, 1982, P.313).
Because of such circumstances, the seamless tube formed of titanium materials, as provided by JIS H-4630 and the like, has been manufactured by the use of the extrusion method at a little sacrifice of manufacturing efficiency and yield.
.
-200'2~
In order to manufacture the seamless tube efficiently and economically in general, it is preferable to adopt a continuous seamless tube-manufacturing line including an inclined roll piercing rolling-mill represented by a Mannesmann's piercer. In this case, the seamless tube is manufactured in the following order.
At first, a heated solid billet is subjected to the piercing in the inclined roll piercing rolling-mill or the press-roll t~pe piercer to obtain a hollow piece. The ob-tained hollow piece is successively subjected to the elongating in a mandrel mill or a plug mill to obtain a hollow shell. In the case where the mandrel mill is used in the elongating, the hollow shell is reheated in case of need and then subjected to the reducing in a reducer mill while in the case where the elongating is executed in the plug mill, the hollow shell is reheated in case of need and then subjected to the sizing in a sizer mill. The hollow piece after piercing is in case of need subjected to the second piercing or the hollow piece sizing and then subjected to the elongating.
In such the case where the seamless tube formed of the titanium materials is manufactured by the Mannesmann's method, besides the inferiority in workability the following various kinds of problem have occurred.
If the deformability of the solid billet is insuf-- 200~
ficient when it is subjected to the piercing, surface de-fects, such as skin eruptions, flaws and cracks, are pro-duced on an inner surface of the pierced material. In addition, even though the solid billet having a superior deformability is used, if the piercing conditions are not suitable, similar surface defects are produced. Since the titanium materials are inferior in deformability, such the surface defects are frequently produced with ease.
Since titanium oxides formed on the surface of the titanium materials prior to the rolling are remarkably dif-ficult to be separated, these titanium oxides are not broken but deposited in a concave portion of the rolls when the titanium materials are subjected to the piercing or the second piercing. Since such the titanium oxides stuck to the roll surface are highly lubricious, a problem occurs in that the titanium materials slip and become inferior in intermeshing to the roll during the rolling process.
Furthermore, since the reducing or the sizing is the final process, the result of this reducing or sizing deter-mines the surface quality of a product. Since titanium is originally inferior in hot workability (deformability), if it is intended to secure the dimensional accuracy required in this reducing or sizing, there is a possibility that the surface quality of the product is deteriorated. In parti-cular, in using the reducer mill, it is necessary to con-20n~
trive a design of roll grooves.
Because of such the state of matters, an art of manu-facturing a seamless tube formed of titanium materials by the use of the Mannesmann's method has not been established yet.
SUMMARY OF THE INVENTION
The present invention has been achieved in view of such the state of matters and proposes suitable conditions in each process of the Mannesmann's method properly including a piercing, a second piercing, a hollow piece sizing, an elon-gating, a sizing and a reducing so that a seamless tube formed of titanium materials may be manufactured with high accuracy by the use of the Mannesmann's method.
According to the method of the present invention, when an ingot is worked to produce a solid billet, the ingot is heated to a temperature of 850 to 1,250 C and the final temperature is set at 600 to 1,100 C and the working degree at 50 % or more. In addition, the piercing of the solid billet is executed within a temperature range of ~ transus - 100 to 1,250 C. Furthermore, in this piercing of the solid billet, a high-pressure water of 50 kg/cm2 or more is blasted onto the inclined rolls used and the descaling of the inclined rolls is executed by means of a brush. Also when the hollow piece is subjected to the second piercing, 200~
the descaling is similarly executed. In addition, in the case where the reducer mill is used in the reducing, a tem-perature of the hollow shell at an inlet side of the mill is set at 600 to 1,100 C, a reduction of outside diameter being set at 80 % or less, and a rectangular ratio (A) of roll grooves of the reducer mill being set as follows de-pending upon a wall-thickness (t) and an outside diameter ~D) of the product. In the case where t/D is less than 10 %, A ~ 0.7, in the case where t/D is 10 -% or more but less than 15 %, l ~ 0.8, and in the case where t/D is 15 % or more, A ~ 0.9. In the sizing process, in the case where a sizer mill is used, a temperature of the hollow shell at an inlet side of the mill is set at 550 to 1,150 ~C and the reduction in outside diameter is set at 3 to 15 %.
It is one object of the present invention to provide a method of manufacturing a seamless tube formed of titanium materials capable of manufacturing a seamless tube formed of titanium materials exhibiting no surface defect, such as skin eruption, flaw and crack, being superior in mechanical characteristics, by the use of the Mannesmann's method.
It is another object of the present invention to pro-vide a method of manufacturing a seamless tube formed of titanium materials capable of manufacturing a seamless tube formed of titanium materials with high efficiency and producing no miss-roll by the use of the Mannesmann's - zoo~
method.
The above and further objects and features of the invention will more fully be apparent from the following detailed description with accompanying drawings.
BRIEF DESCRIPTION OF THE DRAWINGS
Fig. 1 is a chart showing processes of a method of manufacturing a seamless tube formed of titanium materials according to the present invention;
Fig. 2 is a schematic diagram showing a piercing pro-cess of a solid billet by means of an inclined roll type piercer;
Fig. 3 and Fig. 4 are diagrams showing a polygon phase;
Fig. 5 is a perspective view showing a shape of a con-tact surface of rolls;
Fig. 6 is a graph showing a relation between a rec-tangular ratio of roll grooves and a degree of polygon formation for plain carbon steels and pure titanium; and Fig. 7 is a graph showing a range of the rectangular ratio of roll grooves effective for a polygon formation.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
Fig. 1 is a chart showing main processes of a method of manufacturing a seamless tube formed of titanium material by 200.~
the use of the Mannesmann's method according to the present invention. At first, an ingot formed of pure titanium or titanium alloys is heated to produce a solid billet. In this time, a heating temperature is set at 8~0 to 1,250 C, the final temperature being set at 600 to 1,100 ~C, and a working degree being set at 50 % or more. Here, the working degree is (cross sectional area of the ingot - cross sec-tional area after the process) cross sectional area of the ingot X 100 (~).
Then, this solid billet is subjected to the piercing by means of a piercer to produce a first hollow piece. In this time, a temperature range is set ~ transus - 100 to 1,2~0 ~C. In addition, here ~ transus is a temperature of a transformation from ~ single phase to a+~ dual phases.
Here, three courses can be thought as a course reaching the subsequent elongating process. A first course is a course (R1 in Fig. 1) directly reaching the elongating pro-cess. A second course is a course (R2 in Fig. 1) in which the first hollow piece is subjected to a second piercing (elongating) process by means of an elongator to be turned into a second hollow piece and then this second hollow piece arrives at the elongating process. A third course is a course (R3 in Fig. 1) in which this first hollow piece is subjected to a hollow piece sizing process by means of a shell-sizer to be turned into a third hollow piece and then - 200~
this third hollow piece arrives at the elongating process.
The process, in which the solid billet is subjected to the piercing to be turned into the first hollow piece, and the process, in which the fist hollow piece is subjected to the second piercing to be turned into the second hollow piece, are executed with blasting a high-pressure water of 50 kg/cm or more onto the inclined rolls of the rolling mill and descaling the inclined rolls by means of a brush.
The following process is divided into two courses. The first course is a course (R4 in Fig. 1) in which the hollow piece is subjected to the elongating by means of a mandrel mill to produce a hollow shell and then this hollow shell is subjected to the reducing by means of the reducer mill. The second course is a course ~R5 in Fig. 1) in which the hollow piece is subjected to the elongating by means of a plug mill to be turned into a hollow shell and then the hollow shell is subjected to the sizing by means of a sizer mill. Here, in case of the reducing by means of the reducer mill, a temperature at an inlet side of the mill is set at 600 to 1,100 C and the reduction of outside diameter at 80 % or less. In case of the sizing by means of the sizer mill, the temperature at an inlet side of the mill is set at 550 to 1,150 C and the reduction of outside diameter at 3 to 15 %.
After a series of these hot working processes, the hollow shell is in case of need subjected to the cold working and z~?~
then subjected to the heat treatment, and finally the pro-duct (a seamless tube formed of titanium materials) is manufactured.
The details of the respective processes will be below described with reasons why the conditions in the respective processes are limited as center.
An ingot as it has been cast shows a coarse cast struc-ture which is remarkably inferior in deformability. In addition, it contains also voids. Accordingly, if such the ingot is heated and subjected to the piercing by means of the piercer as it is, surface defects, such as flaws and cracks, are produced on an inner surface of the hollow piece due to the insufficient deformability when pierced.
So, according to the method of the present invention, at first the ingot is subjected to a suitable working to be tuned into a billet having a structure suitable for the piercing process. The ingot is heated to temperatures of 850 to 1,250 C but the absorption of hydrogen gases and/or stable oxidized layer are produced at high temperatures ex-ceeding 1,250 C. Forging cracks are generated at the beginning of process due to the worsened deformability of the ingot at temperatures lower than 850 C.
The final temperature is set at 1,100 C or less but 600 C or more. The final temperature has important influence upon the minute structure of the billet after the zoo~
process. If the final temperature is higher than 1,100 C, the structure after the process is not minute and the ob-tained billet does not have a superior deformability. If the lower limit temperature after the process is too low, the cracks are produced in the forging process due to the worsened deformability, so that it is necessary that the lower limit temperature is set at 600 C or more. In addition, here the temperature may be selected with a sur-face temperature of the ingot or billet as standard in the actual operation.
It is another important matter in this process that the working degree is set at 50 % or more. The inhomogenous structure and voids within the ingot can be cancelled and the obtained billet can be superior in deformability by set-ting the working degree at 50 % or more within the above described temperature range.
The billet, which has been produced in the preceding process, is subjected to the piercing within a temperature range from 1,250 C to ~ transus - 100 C. In this case, the billet, which has been obtained in the preceding pro-cess, may be supplementarily heated in case of need and successively subjected to the piercing or the billet, which has been once cooled to normal temperature, may be heated again and then subjected to the piercing. If the piercing is executed at temperatures exceeding 1,250 C, a fragile 200.'27~
phase called a-case due to the absorption of oxygen and nitrogen is formed on the surface of the billet and this a-case induces cracks in the piercing process to generate sur-face defects, such as cracks, on the outer surface of the hollow piece.
The deformability of the billet is reduced with a re-duction of the piercing temperature. If the piercing is executed at temperatures lower than ~ transus - 100 C, the deformability becomes insufficient, whereby surface defects, such as skin eruptions, flaws and cracks, are produced on the inner surface of the hollow piece after the piercing.
In addition, the piercing temperature is a surface temperature of the solid billet before the piercing.
Ti-6Al-4V (~ transus -. 990 C) was used as a representative a+~-type titanium alloy. Its chemical composition is shown by (a~ in Table 1.
A material having a size shown in Table 2 was cut out from an ingot cast having an outside diameter of 750 mm and a length of 3,000 mm and subjected to a hot forging under the conditions also shown in Table 2. The finishing outside diameter size was set at 0 70 mm in case of the material for an inclined roll type piercer, which will be mentioned later, and ~ 65 mm in case of the material for a press roll type piercer. The finishing temperature of the forging was controlled by the surface temperature.
- 200~
The piercing tests were carried out by the use of a two-roll Mannesmann's piercer (of inclined roll type) with barrel type rolls and a press roll type piercer.
In the case where the inclined roll type piercer was used, a cylindrical billet having an outside diameter of 60 mm and a length of 250 mm was taken out from a forging material having an outside diameter of 70 mm by the machin-ing and heated at a heating temperature shown in Table 2 for 2 hours followed by piercing at a piercing ratio (a ratio of a length after the piercing to that before the piercing) of 2.1. In this time, an angle of inclination of rolls was set at 12 . The piercing was executed for 3 pieces under the respective conditions. The surface temperature of the bil-let immediately before the piercing in this time is shown in Table 2 by a mean value for 3 pieces of material to be pierced.
In the case where the press roll type piercer was used, a billet having a rectangular cross section with a side length of 60 mm and a length of 250 mm was taken out from a forging material having a rectangular cross section with a side length of 65 mm by the machining and heated at a tem-perature shown in Table 2 for 2 hours followed by piercing at a piercing ratio of 1.3. The piercing was executed for three pieces under the respective conditions. The surface temperature of the billet immediately before the piercing in 200.'2~
this time is shown in Table 2 by a mean value for 3 pieces of material to be pierced.
The evaluation after the piercing was conducted for all of 3 pieces of material to be tested on the piercing obtain-ed under the respective conditions of the piercing test.
The material for the piercing test was longitudinally divided into 8 equal parts in a circumferential direction all over the length thereof and then descaled all over the length of an inner surface and an outer surface thereof by the sand-blasting followed by investigating the existence of flaws by the penetration test. The investigation was exe-cuted for 48 surfaces (3 pieces of material to be tested on the piercing X number of divided parts of 8 X 2 surfaces of the inner surface and the outer surface) under the re-spective conditions of the piercing test. The penetration test was conducted in compliance with JIS Z-2343 by the use of a washable dyeing penetrant. In the case where a defect having a length of 1 mm or more was detected at at least one place on the inner surface and the outer surface (48 sur-faces) by this penetration test, the result of the penetra-tion test was evaluated by X in Table 2. In addition, in the case where no defect was detected on the inner surface and the outer surface (48 surfaces), the result of the penetration test was evaluated by 0.
It is found from the results shown in Table 2 that in -i 200~
both the case where the inclined roll type piercer is used and the case where the press roll type piercer is used, a pierced material having no surface defect, such as skin eruption, flaw and crack, on both the inner surface and the outer surface can be obtained merely in the case where a temperature of an ingot at the completion of the forging is 1,100 C or less but 600 C or more, the working degree from the ingot to the billet being 50 % or more, and the piercing being executed within the temperature range from 1,250 C or less to ~ transus - 100 C or more.
A Ti-6Al-2Sn-4Zr-6Mo alloy (~ transus , 960 C) shown by (b) in Table 1 was used as another material. In this time, the rolling was used as the working method for turning the ingot into the billet. The rolling conditions are shown in Table 3. In addition, the piercing test was conducted by means of merely the inclined roll type piercer in view of the matter that no difference was found between the case where the press roll type piercer was used and the case where the inclined roll type piercer was used in previous example (Table 2). The finishing size, the piercing test method and the evaluation method after the piercing are same as in previous example. The results are shown in Table 3.
It is found from the results shown in Table 3 that in the case where the ingot is worked (production of the bil-let) and subjected to the piercing within the conditions 200~
according to the present invention, a hollow piece having no surface defect, such as skin èruption, flaw and crack, on both the inner surface and the outer surface thereof can be obtained in the same manner as in previous example.
According to the present invention, when a solid billet is subjected to the piercing by means of an inclined roll type piercer, the surface of the inclined rolls of the piercer is descaled by blasting the high-pressure water thereonto. Fig. 2 is a schematic diagram showing the pierc-ing process of the solid billet by means of the inclined roll type piercer. Referring to Fig. 2, a left side is an inlet side and the solid billet 1 is subjected to the pierc-ing by means of the piercer to produce a first hollow piece 2. The piercer is provided with a piping 4 for supplying the high-pressure water in the vicinity of two pieces of barrel type rolls 3 thereof. The piping 4 is provided with a plurality of nozzle 5 and the high-pressure water is blasted onto the surface of the rolls 3 through the nozzles 5. In addition, the rolls 3 are provided with a brush 6 for descaling the surface thereof. And, when the solid billet 1 is subjected to the piercing, the high-pressure water is blasted through the nozzles 5 to remove titanium oxides stuck to the surface of the rolls 3 by means of said brush 6.
The respective solid billets were subjected to the 4~1 _ piercing with descaling under the descaling conditions shown in Table 4 to produce the first hollow piece. A piercing efficiency and the miss-roll rate in this time are shown in Table 4. In addition? a substance A in Table 4 is formed of pure titanium (JIS H-4630) and a substance B is formed of a titanium alloy (Ti-6Al-4V).
It is found from the results shown in Table 4 that the slip of the solid billet due to titanium oxides left on the surface of the inclined rolls can be prevented by providing the brush on the inclined rolls and descaling the inclined rolls by blasting the high-pressure water having a water pressure of 50 kg/cm2 or more to enhance the stability of the p-iercing, by means of the inclined roll type piercer.
In addition, such the descaling treatment is effective for an increase of the stability of the operation also in the second piercing process from the first hollow plece to the second hollow piece.
Next, the reducing process using the reducer mill will be described.
Characteristics of titanium are greatly dependent upon temperature and in particular when it is subjected to the reducing under the condition that the temperature at the in-let side of the reducer mill is lower than 600 C, its deformability is worsened, so that flaws, such as skin erup-tion-like, striped, edge marks and holes due to the jamming 200t~
of the rolls, are produced. In addition, titanium alloys produce voids on the boundary surface between the a-phase and the ~-phase when they are subjected to the deformation due to a difference between the a-phase and the ~-phase in deformability. On the contrary, when they are subjected to the reducing under the condition that the temperature at the inlet side of the reducer mill exceeds 1,100 C, coarse acicular structures are produced due to the cooling after the reducing. These acicular structures have a poor room-temperature ductility and deteriorate mechanical properties of the product. Accordingly, the temperature of the hollow shell at the inlet side of the reducer is set at 600 to 1 , 1 00 C .
If the reduction of outside diameter in the reducing exceeds 80 %, outer-surface flaws, such as stripe-like and edge marks due to the jamming of the rolls, are produced and the surface properties of the product are deteriorated even though the temperature of the hollow shell at the inlet side of the reducer mill is suitably controlled. Accordingly, the reduction of outside diameter in the reducing is set at 80 % or less. In addition, the reducer mill is used as shape-regulating and correcting means at the small reduction of outside diameter according to circumstances. In this case, no evil influence occurs, so that the lower limit of the reduction of outside diameter is not specially limited.
200.'2~
A solid billet having an outside diameter of 187 mm and a length of 2,250 mm formed of industrial pure titanium having the composition shown in Table 5 (JIS H-4630-3) was subjected to the piercing by means of an inclined roll type piercer at the temperature at the inlet side of the piercer of 1,050 C to be turned into a first hollow piece having an outside diameter of 192 mm, a wall-thickness of 20.62 mm and a length of 5,470 mm and the resulting first hollow piece was subjected to the hollow piece sizing by means of a shell sizer at the temperature at the inlet side of the shell-sizer of 1,000 C to obtain a third hollow piece having an outside diameter of 168 mm, a wall-thickness of 22.0 mm and a length of 6,020 mm.
Successively, the obtained third hollow piece was sub-jected to the elongating by means of a 7-stand mandrel mill at the temperature at the inlet side of the mandrel mill of 900 C to obtain a hollow shell having an outside diameter of 140 mm, a wall-thickness of 6.0 mm and a length of 24,040 mm. In this time, an elongation ratio was set at 4.
Subsequently, the obtained hollow shell was reheated and subjected to the reducing by means of a 3-roll 24-stand reducer mill at the temperature at the inlet side of the re-ducer mill of 850 CC (constant) with varying the reduction of outside diameter. Properties of the seamless tube formed of pure titanium after the reducing and those of the seam-~ 20().~
less tube formed of pure titanium after annealing for 1 hourat 750 C are shown in Table 6. In addition, properties and characteristics of the hollow shell before the reducing and the standard values for the hollow shell formed of indus-trial pure titanium (JIS H-4630-3) of the same one grade produced by the hot extrusion and the cold drawing in com-bination are shown in Table 6 for reference.
In the case (No. 6~ where the reduction of outside dia-meter exceeded 80 %, a notable jamming of rolls and edge marks were produced while in the case where the reduction of outside diameter was 80 % or less, good surface properties were obtained and also mechanical characteristics meet all of the standard values for the hollow shell produced by the hot extrusion and the cold drawing in combination.
The results obtained when the same one hollow shell was subjected to the reducing until an outside diameter of 63.6 mm and a wall-thickness of 5.75 mm (reduction of outside diameter: 54.6 %~ at various temperatures are shown in Table 7. In the case where the temperature at the inlet side of the mill is 500 DC (No. 1), a rough skin is produced on an inner surface of the hollow shell but in the case where the temperature at the inlet side of the mill is 600 to 1,100 C
(No. 2 to 4), both the surface properties and the mechanical characteristics are good.
Subsequently, a Ti-6Al-4V alloy having a composition 20(~
shown in Table 8 was subjected to the same test as above described. The results are shown in Tables 9, 10.
As obvious from Tables 9, 10, the reducing conditions according to the present invention in using the reducer mill are effective also for the hollow shell formed of titanium alloys.
The titanium material is anisotropic in deformation, so that its degree of polygon formation is increased in com-parison with that of plain carbon steels and also its phase characteristics are difference from those of plain carbon steels in the hollow reducing such as the reducing.
Figs. 3, 4 are graphs showing a polygon formation phase produced in the case where the reducing is conducted in a 3-grooved roll stand. Fig. 3 shows a positive phase and Fig.
4 shows a negative phase. Although it is described in de-tail later, most of plain carbon steels show the positive phase while titanium is apt to show the negative phase.
In order to suppress the polygon formation in the re-ducing, it has been known that the regulation of the projec-tion shape of the roll-contact surface hatched in Fig. 5 when projected in a direction shown by an arrow is effec-tive. In case of plain carbon steels, the roll groove is designed so that the projection shape of this roll-contact surface may be rectangular. That is to say, in the reducing of plain carbon steels, the rectangular ratio of rolls ZOO.~
(contact-length LE of an edge portion / contact-length LG of a groove portion) is brought close to 1 and a uniform out-side pressure deformation is added in a circumferential direction to make a quantity of deformation in wall-thick-ness uniform in the circumferential direction, whereby sup-pressing the polygon formation.
This design method presupposes the calculation of the contact-area on the basis of the shape of the roll grooves between the preceding stand and the present stand. Since the roll groove is not perfectly filled with the tube, the actual contact-area is smaller than that calculated by the use of the design rectangular rate. One of reasons for this is the reduction of the outside diameter by the tension of the tube between the stands.
The titanium material is anisotropic in deformation, so that it is difficult to be deformed in the circumferential direction and the reduction of outside diameter between the stand is smaller in comparison with that of steels. As a result, the actual rectangular ratio of the contact-surface of the hollow shell for the roll groove is larger in com-parison with that of the plain carbon steels. Thus, the polygon phase showing the positive phase of the plain carbon steels is apt to be turned into the negative phase in case of titanium. Accordingly, the conventional measure against the polygon formation phenomenon, in which the rectangular 20~
ratio of roll grooves is brought close to 1, brings about the opposite effect in case of titanium.
Fig. 6 is a graph showing a relation between the rec-tangular ratio of roll grooves and the degree of polygon formation when the hollow shell formed of plain carbon steels (C % = 0.2 %) and pure titanium is subjected to the reducing at the reduction of outside diameter of 55 % and t/D = 17 %. In case of the plain carbon steels, the degree of polygon formation amounts to about + 20 % at the rec-tangular rate of roll grooves of 0.8 or more and it is reduced less than 10 % at the rectangular rate of roll grooves of 1Ø On the contrary, in case of pure titanium, the negative polygon formation is brought about and its rate is increased with the approach of the rectangular ratio of roll grooves to 1.
According to the investigation by the present inven-tors, the rectangular ratio A of roll grooves effective for suppressing the polygon formation in the case where titanium material is subjected to the reducing, as shown in Fig. 7, is varied depending upon the ratio t/D, which is a ratio of the wall-thickness t to the finishing outside diameter D by the reducer mill and the following relations hold good.
When t/D < 10 %, A S 0.7;
when 10 % S t/D < 15 %, A S 0.8; and when 15 % S t/D, A S 0-9-20()~
In view of this point, in the above described preferredembodimentl the roll groove is designed so that the rec-tangular ratio of all reducing rolls excepting the inter-meshing guide rolls and finishing rolls may be 0.8, whereby the degree of polygon formation is suppressed to 15 % or less in the absolute value. In addition, in view of no problem in the properties of the inner and outer sùrfaces and the completion of the reducing, the lower limit of the rectangular ratio of roll grooves is set at O or more, pre-ferably 0.2 or more when t/D < 10 %, 0.3 or more when 10 %
t/D < 15 %, and 0.4 or more when 15 ~ t/D.
Although the polygon formation after the reducing does not deal the product a fatal defect, it goes without saying that the quality of the product can be still more improved by suppressing it. In addition, the degree of polygon for-mation is a value shown by the following equation.
The degree oi polygon formation =
t - t i X 100 (%) (D/2 - tmin) X 0.135 D: Nominal diameter;
timaX: Maximum wall-thickness in one side of a hexagon;
timin: Minimum wall-thickness in one side of a hexagon;
200~
~ timaX
tmax = 6 ~ ti min tmin = 6 timin = Min (timin) Next, the sizing process using the sizer mill will be described.
The temperature of the hollow shell at the inlet side of the sizer mill is set at 550 to 1,150 C due to the same reasons as those for the above described temperature at the inlet side of the reducer mill.
On the other hand, if the reduction of outside diameter in the sizing process is less than 3 %, the object of the sizing can not be achieved and the dimensional accuracy of the product is deteriorated. On the contrary, if the reduc-tion of outside diameter exceeds 15 %, surface defects, such as stripe flaws and edge marks due to the jamming of rolls, are produced to deteriorate the surface properties of the product. Accordingly, the reduction of outside diameter in the sizing is set at 3 to 15 %.
A solid billet formed of industrial pure titanium (JIS
H-4630-3) having the composition shown in Table 11 and hav-ing an outside diameter of 173 mm and a length of 2,040 mm 20().~
-was subjected to the piercing by means of an inclined type piercer at the temperature at the inlet side of the piercer of 990 to 1,250 C to be turned into a first hollow piece having an outside diameter of 178 mm, a wall-thickness of 40 mm and a length of 2,710 mm and the resulting first hollow piece was subjected to the second piercing (elongating~ by means of an elongator at the temperature at the inlet side of the elongator of 880 to 1,200 CC to be turned into a second hollow piece having an outside diameter of 190 mm, a wall-thickness of 19.5 mm and a length of 4,500 mm.
Successively, the obtained second hollow piece was sub-jected to the elongating by means of a plug mill at the tem-perature at the inlet side of the plug mill of 660 to 1,150 C to be turned into a hollow shell having an outside diameter of 183 mm, a wall-thickness of 15 mm and a length of 5,940 mm. In this time, the elongation ratio is 1.3.
Subsequently, the obtained hollow shell was reheated to various kinds of temperature and then subjected to the sizing by means of a 2-roll-7-stand sizer mill with varying the reduction of outside diameter. Properties of a seamless tube formed of pure titanium after the sizing and room-tem-perature characteristics of the seamless tube formed of pure titanium after annealing for 1 hour at 750 C are shown in Table 12. In addition, also the standard values for a seam-less tube formed of industrial pure titanium (JIS H-4630-3) 200.~
of the same one grade manufactured by the hot extrusion and the cold drawing in combination are shown in Table 12.
In No. 1, since the temperature at the inlet side of the sizer mill is low, flaws are produced on the surface of the seamless tube, whereby the seamless tube lost the pro-duct value prior to the discussion of the mechanical proper-ties. In No. 6, since the temperature at the inlet side of the sizer mill is too high, the surface properties were good but the elongation was remarkably deteriorated. In No. 8, since the temperature at the inlet side of the sizer mill is suitable but the reduction of outside diameter is insuffi-cient, the desired dimensional accuracy could not be se-cured. In No. 10, since the reduction of outside diameter is too large, the surface defects were produced and thus the seamless tube lost the product value.
On the contrary to the above described comparative examples, in Nos. 2 to 5, 7 and 9 according to the present invention, the surface properties are good and the mechan-ical characteristics meet all the standard values for the seamless tube by the hot extrusion and the cold drawing in combination.
Next, the same one test as the above described one was conducted for a Ti-6Al-4V alloy having a composition shown in Table 13. The results are shown in Table 14.
As obvious from Table 14, the sizing method according 200~
to the present invention is effective also for the produc-tion of a hollow shell formed of titanium alloys.
In addition, although the hollow shell is produced by the elongating in the respective preferred examples, it is not limitative. For example, a hollow shell produced by piercing by means of the inclined roll, a hollow shell produced by the extrusion, a hollow shell produced by the simply mechanical piercing and the like can be subjected to the reducing or the sizing. Furthermore, also the reducer mill or sizer mill having a construction other than the above described ones may be used. Besides, also the sur-face-machining or cold drawing can be conducted after the reducing or the sizing.
As this invention may be embodied in several forms without departing from the spirit of essential characteris-tics thereof, the present embodiment is therefore illustra-tive and not restrictive, since the scope of the invention is defined by the appended claims rather than by the de-scription preceding them, and all changes that fall within the meets and bounds of the claims, or equivalence of such meets and bounds thereof are therefore intended to be em-braced by the claims.
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as _ -able 7 ~ ` Reducing Condition Room-temperature Tensile , Properties N~ Temperature at Inlet Reduction of Size (outside diameter mmProperty of Product Evaluation - side of Rolling Mill Outside Diameter Xwall-thickness mm) YS W mmZ) TS~kg/mm2) E ~ a , ;; (~) (%) 1 500 * 54.6 63.5 x 5.75Crack in Inner Surface 95.5 58.2 - x 2 600 54.6 63.5 x 5.75 Good 41.9 56.8 26.4 O
3 850 54.6 63.5 x5.75 Good 39.5 54.2 28.5 0 $ 4 1100 54.6 63.5 x5.75 Good 37.1 51.2 28.5 0 1150 * 54.6 63.5 X 5.75Jamming of Rolls 25.9 47.1 11.1 x JIS-H4630-3 - 49 /63 18 or more - g * Out of conditions of the invention 2~J
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' 1 850 9.2 127 x6.25 Good 92.8 100.1 17.2 0 1~
2 850 36.5 88.9 x~.o Good 93.7 l00.9 18.0 2 3 850 54.6 63.5 x 5.75 Good 94.1 101.9 17.4 0 IV
METHOD OF MANUFACTURING SEAMLESS TUBE
FORMED OF TITANIUM MATERIAL
BACKGROUND OF THE INVENTION
Field of the Invention The present invention relates to a method of manu-facturing a seamless tube formed of titanium materials including pure titanium and titanium alloys by the use of the Mannesmann's method.
Description of Related Art The titanium materials are classified into pure tita-nium and the titanium alloys such as a-type titanium alloys, and +~-type titanium alloys and ~-type titanium alloys. The a-type titanium alloys include Ti-0.15Pd, Ti-0.8Ni-0.3Mo, Ti-5Al-2.5Sn and the like. The a+~-type titanium alloys include Ti-8Al-lMo-lV, Ti-3Al-2.5V, Ti-6Al-4V, Ti-6Al-6V-2Sn, Ti-6Al-2Sn-4Zr-6Mo, Ti-6Al-2Sn-4Zr-2Mo and the like such as small amount of platinum group elements added alloys and platinum group elements plus small amount of Ni, Co, W, Mo added alloys. The ~-type titanium alloys include Ti-3Al-8V-6Cr-4Mo-4Zr and the like. In the present invention, the titanium materials used as subject materials are a general name of the above-mentioned all type of tita-20Q~
nium alloys. Pure titanium is a titanium material whichmainly has impurities such as H, O, N, Fe, its charac-teristic is changed according to quantity of O and Fe in particular.
These titanium materials are light and highly cor-rosion-resistant and in partlcular a seamless tube formed of them has been expected to be used for a piping for use in chemical plant, an oil pressure piping for use in aircraft, and an oil field piping.
The seamless tube has been manufactured by the extru-sion method or Mannesmann's method. The extrusion method is suitable for manufacturing a tube of materials inferior in workability, but inferior in manufacturing efficiency. On the contrary, Mannesmann's method is superior in manufactur-ing efficiency, but requires materials superior in work-ability.
Some trials for manufacturing a tube formed of a titanium material by Mannesmann's method have been per-formed, but manufacturing technique for obtaining a good tube in quality has not established yet (Reference:
"Titanium And Titanium Alloys" volume 1, 1982, P.313).
Because of such circumstances, the seamless tube formed of titanium materials, as provided by JIS H-4630 and the like, has been manufactured by the use of the extrusion method at a little sacrifice of manufacturing efficiency and yield.
.
-200'2~
In order to manufacture the seamless tube efficiently and economically in general, it is preferable to adopt a continuous seamless tube-manufacturing line including an inclined roll piercing rolling-mill represented by a Mannesmann's piercer. In this case, the seamless tube is manufactured in the following order.
At first, a heated solid billet is subjected to the piercing in the inclined roll piercing rolling-mill or the press-roll t~pe piercer to obtain a hollow piece. The ob-tained hollow piece is successively subjected to the elongating in a mandrel mill or a plug mill to obtain a hollow shell. In the case where the mandrel mill is used in the elongating, the hollow shell is reheated in case of need and then subjected to the reducing in a reducer mill while in the case where the elongating is executed in the plug mill, the hollow shell is reheated in case of need and then subjected to the sizing in a sizer mill. The hollow piece after piercing is in case of need subjected to the second piercing or the hollow piece sizing and then subjected to the elongating.
In such the case where the seamless tube formed of the titanium materials is manufactured by the Mannesmann's method, besides the inferiority in workability the following various kinds of problem have occurred.
If the deformability of the solid billet is insuf-- 200~
ficient when it is subjected to the piercing, surface de-fects, such as skin eruptions, flaws and cracks, are pro-duced on an inner surface of the pierced material. In addition, even though the solid billet having a superior deformability is used, if the piercing conditions are not suitable, similar surface defects are produced. Since the titanium materials are inferior in deformability, such the surface defects are frequently produced with ease.
Since titanium oxides formed on the surface of the titanium materials prior to the rolling are remarkably dif-ficult to be separated, these titanium oxides are not broken but deposited in a concave portion of the rolls when the titanium materials are subjected to the piercing or the second piercing. Since such the titanium oxides stuck to the roll surface are highly lubricious, a problem occurs in that the titanium materials slip and become inferior in intermeshing to the roll during the rolling process.
Furthermore, since the reducing or the sizing is the final process, the result of this reducing or sizing deter-mines the surface quality of a product. Since titanium is originally inferior in hot workability (deformability), if it is intended to secure the dimensional accuracy required in this reducing or sizing, there is a possibility that the surface quality of the product is deteriorated. In parti-cular, in using the reducer mill, it is necessary to con-20n~
trive a design of roll grooves.
Because of such the state of matters, an art of manu-facturing a seamless tube formed of titanium materials by the use of the Mannesmann's method has not been established yet.
SUMMARY OF THE INVENTION
The present invention has been achieved in view of such the state of matters and proposes suitable conditions in each process of the Mannesmann's method properly including a piercing, a second piercing, a hollow piece sizing, an elon-gating, a sizing and a reducing so that a seamless tube formed of titanium materials may be manufactured with high accuracy by the use of the Mannesmann's method.
According to the method of the present invention, when an ingot is worked to produce a solid billet, the ingot is heated to a temperature of 850 to 1,250 C and the final temperature is set at 600 to 1,100 C and the working degree at 50 % or more. In addition, the piercing of the solid billet is executed within a temperature range of ~ transus - 100 to 1,250 C. Furthermore, in this piercing of the solid billet, a high-pressure water of 50 kg/cm2 or more is blasted onto the inclined rolls used and the descaling of the inclined rolls is executed by means of a brush. Also when the hollow piece is subjected to the second piercing, 200~
the descaling is similarly executed. In addition, in the case where the reducer mill is used in the reducing, a tem-perature of the hollow shell at an inlet side of the mill is set at 600 to 1,100 C, a reduction of outside diameter being set at 80 % or less, and a rectangular ratio (A) of roll grooves of the reducer mill being set as follows de-pending upon a wall-thickness (t) and an outside diameter ~D) of the product. In the case where t/D is less than 10 %, A ~ 0.7, in the case where t/D is 10 -% or more but less than 15 %, l ~ 0.8, and in the case where t/D is 15 % or more, A ~ 0.9. In the sizing process, in the case where a sizer mill is used, a temperature of the hollow shell at an inlet side of the mill is set at 550 to 1,150 ~C and the reduction in outside diameter is set at 3 to 15 %.
It is one object of the present invention to provide a method of manufacturing a seamless tube formed of titanium materials capable of manufacturing a seamless tube formed of titanium materials exhibiting no surface defect, such as skin eruption, flaw and crack, being superior in mechanical characteristics, by the use of the Mannesmann's method.
It is another object of the present invention to pro-vide a method of manufacturing a seamless tube formed of titanium materials capable of manufacturing a seamless tube formed of titanium materials with high efficiency and producing no miss-roll by the use of the Mannesmann's - zoo~
method.
The above and further objects and features of the invention will more fully be apparent from the following detailed description with accompanying drawings.
BRIEF DESCRIPTION OF THE DRAWINGS
Fig. 1 is a chart showing processes of a method of manufacturing a seamless tube formed of titanium materials according to the present invention;
Fig. 2 is a schematic diagram showing a piercing pro-cess of a solid billet by means of an inclined roll type piercer;
Fig. 3 and Fig. 4 are diagrams showing a polygon phase;
Fig. 5 is a perspective view showing a shape of a con-tact surface of rolls;
Fig. 6 is a graph showing a relation between a rec-tangular ratio of roll grooves and a degree of polygon formation for plain carbon steels and pure titanium; and Fig. 7 is a graph showing a range of the rectangular ratio of roll grooves effective for a polygon formation.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
Fig. 1 is a chart showing main processes of a method of manufacturing a seamless tube formed of titanium material by 200.~
the use of the Mannesmann's method according to the present invention. At first, an ingot formed of pure titanium or titanium alloys is heated to produce a solid billet. In this time, a heating temperature is set at 8~0 to 1,250 C, the final temperature being set at 600 to 1,100 ~C, and a working degree being set at 50 % or more. Here, the working degree is (cross sectional area of the ingot - cross sec-tional area after the process) cross sectional area of the ingot X 100 (~).
Then, this solid billet is subjected to the piercing by means of a piercer to produce a first hollow piece. In this time, a temperature range is set ~ transus - 100 to 1,2~0 ~C. In addition, here ~ transus is a temperature of a transformation from ~ single phase to a+~ dual phases.
Here, three courses can be thought as a course reaching the subsequent elongating process. A first course is a course (R1 in Fig. 1) directly reaching the elongating pro-cess. A second course is a course (R2 in Fig. 1) in which the first hollow piece is subjected to a second piercing (elongating) process by means of an elongator to be turned into a second hollow piece and then this second hollow piece arrives at the elongating process. A third course is a course (R3 in Fig. 1) in which this first hollow piece is subjected to a hollow piece sizing process by means of a shell-sizer to be turned into a third hollow piece and then - 200~
this third hollow piece arrives at the elongating process.
The process, in which the solid billet is subjected to the piercing to be turned into the first hollow piece, and the process, in which the fist hollow piece is subjected to the second piercing to be turned into the second hollow piece, are executed with blasting a high-pressure water of 50 kg/cm or more onto the inclined rolls of the rolling mill and descaling the inclined rolls by means of a brush.
The following process is divided into two courses. The first course is a course (R4 in Fig. 1) in which the hollow piece is subjected to the elongating by means of a mandrel mill to produce a hollow shell and then this hollow shell is subjected to the reducing by means of the reducer mill. The second course is a course ~R5 in Fig. 1) in which the hollow piece is subjected to the elongating by means of a plug mill to be turned into a hollow shell and then the hollow shell is subjected to the sizing by means of a sizer mill. Here, in case of the reducing by means of the reducer mill, a temperature at an inlet side of the mill is set at 600 to 1,100 C and the reduction of outside diameter at 80 % or less. In case of the sizing by means of the sizer mill, the temperature at an inlet side of the mill is set at 550 to 1,150 C and the reduction of outside diameter at 3 to 15 %.
After a series of these hot working processes, the hollow shell is in case of need subjected to the cold working and z~?~
then subjected to the heat treatment, and finally the pro-duct (a seamless tube formed of titanium materials) is manufactured.
The details of the respective processes will be below described with reasons why the conditions in the respective processes are limited as center.
An ingot as it has been cast shows a coarse cast struc-ture which is remarkably inferior in deformability. In addition, it contains also voids. Accordingly, if such the ingot is heated and subjected to the piercing by means of the piercer as it is, surface defects, such as flaws and cracks, are produced on an inner surface of the hollow piece due to the insufficient deformability when pierced.
So, according to the method of the present invention, at first the ingot is subjected to a suitable working to be tuned into a billet having a structure suitable for the piercing process. The ingot is heated to temperatures of 850 to 1,250 C but the absorption of hydrogen gases and/or stable oxidized layer are produced at high temperatures ex-ceeding 1,250 C. Forging cracks are generated at the beginning of process due to the worsened deformability of the ingot at temperatures lower than 850 C.
The final temperature is set at 1,100 C or less but 600 C or more. The final temperature has important influence upon the minute structure of the billet after the zoo~
process. If the final temperature is higher than 1,100 C, the structure after the process is not minute and the ob-tained billet does not have a superior deformability. If the lower limit temperature after the process is too low, the cracks are produced in the forging process due to the worsened deformability, so that it is necessary that the lower limit temperature is set at 600 C or more. In addition, here the temperature may be selected with a sur-face temperature of the ingot or billet as standard in the actual operation.
It is another important matter in this process that the working degree is set at 50 % or more. The inhomogenous structure and voids within the ingot can be cancelled and the obtained billet can be superior in deformability by set-ting the working degree at 50 % or more within the above described temperature range.
The billet, which has been produced in the preceding process, is subjected to the piercing within a temperature range from 1,250 C to ~ transus - 100 C. In this case, the billet, which has been obtained in the preceding pro-cess, may be supplementarily heated in case of need and successively subjected to the piercing or the billet, which has been once cooled to normal temperature, may be heated again and then subjected to the piercing. If the piercing is executed at temperatures exceeding 1,250 C, a fragile 200.'27~
phase called a-case due to the absorption of oxygen and nitrogen is formed on the surface of the billet and this a-case induces cracks in the piercing process to generate sur-face defects, such as cracks, on the outer surface of the hollow piece.
The deformability of the billet is reduced with a re-duction of the piercing temperature. If the piercing is executed at temperatures lower than ~ transus - 100 C, the deformability becomes insufficient, whereby surface defects, such as skin eruptions, flaws and cracks, are produced on the inner surface of the hollow piece after the piercing.
In addition, the piercing temperature is a surface temperature of the solid billet before the piercing.
Ti-6Al-4V (~ transus -. 990 C) was used as a representative a+~-type titanium alloy. Its chemical composition is shown by (a~ in Table 1.
A material having a size shown in Table 2 was cut out from an ingot cast having an outside diameter of 750 mm and a length of 3,000 mm and subjected to a hot forging under the conditions also shown in Table 2. The finishing outside diameter size was set at 0 70 mm in case of the material for an inclined roll type piercer, which will be mentioned later, and ~ 65 mm in case of the material for a press roll type piercer. The finishing temperature of the forging was controlled by the surface temperature.
- 200~
The piercing tests were carried out by the use of a two-roll Mannesmann's piercer (of inclined roll type) with barrel type rolls and a press roll type piercer.
In the case where the inclined roll type piercer was used, a cylindrical billet having an outside diameter of 60 mm and a length of 250 mm was taken out from a forging material having an outside diameter of 70 mm by the machin-ing and heated at a heating temperature shown in Table 2 for 2 hours followed by piercing at a piercing ratio (a ratio of a length after the piercing to that before the piercing) of 2.1. In this time, an angle of inclination of rolls was set at 12 . The piercing was executed for 3 pieces under the respective conditions. The surface temperature of the bil-let immediately before the piercing in this time is shown in Table 2 by a mean value for 3 pieces of material to be pierced.
In the case where the press roll type piercer was used, a billet having a rectangular cross section with a side length of 60 mm and a length of 250 mm was taken out from a forging material having a rectangular cross section with a side length of 65 mm by the machining and heated at a tem-perature shown in Table 2 for 2 hours followed by piercing at a piercing ratio of 1.3. The piercing was executed for three pieces under the respective conditions. The surface temperature of the billet immediately before the piercing in 200.'2~
this time is shown in Table 2 by a mean value for 3 pieces of material to be pierced.
The evaluation after the piercing was conducted for all of 3 pieces of material to be tested on the piercing obtain-ed under the respective conditions of the piercing test.
The material for the piercing test was longitudinally divided into 8 equal parts in a circumferential direction all over the length thereof and then descaled all over the length of an inner surface and an outer surface thereof by the sand-blasting followed by investigating the existence of flaws by the penetration test. The investigation was exe-cuted for 48 surfaces (3 pieces of material to be tested on the piercing X number of divided parts of 8 X 2 surfaces of the inner surface and the outer surface) under the re-spective conditions of the piercing test. The penetration test was conducted in compliance with JIS Z-2343 by the use of a washable dyeing penetrant. In the case where a defect having a length of 1 mm or more was detected at at least one place on the inner surface and the outer surface (48 sur-faces) by this penetration test, the result of the penetra-tion test was evaluated by X in Table 2. In addition, in the case where no defect was detected on the inner surface and the outer surface (48 surfaces), the result of the penetration test was evaluated by 0.
It is found from the results shown in Table 2 that in -i 200~
both the case where the inclined roll type piercer is used and the case where the press roll type piercer is used, a pierced material having no surface defect, such as skin eruption, flaw and crack, on both the inner surface and the outer surface can be obtained merely in the case where a temperature of an ingot at the completion of the forging is 1,100 C or less but 600 C or more, the working degree from the ingot to the billet being 50 % or more, and the piercing being executed within the temperature range from 1,250 C or less to ~ transus - 100 C or more.
A Ti-6Al-2Sn-4Zr-6Mo alloy (~ transus , 960 C) shown by (b) in Table 1 was used as another material. In this time, the rolling was used as the working method for turning the ingot into the billet. The rolling conditions are shown in Table 3. In addition, the piercing test was conducted by means of merely the inclined roll type piercer in view of the matter that no difference was found between the case where the press roll type piercer was used and the case where the inclined roll type piercer was used in previous example (Table 2). The finishing size, the piercing test method and the evaluation method after the piercing are same as in previous example. The results are shown in Table 3.
It is found from the results shown in Table 3 that in the case where the ingot is worked (production of the bil-let) and subjected to the piercing within the conditions 200~
according to the present invention, a hollow piece having no surface defect, such as skin èruption, flaw and crack, on both the inner surface and the outer surface thereof can be obtained in the same manner as in previous example.
According to the present invention, when a solid billet is subjected to the piercing by means of an inclined roll type piercer, the surface of the inclined rolls of the piercer is descaled by blasting the high-pressure water thereonto. Fig. 2 is a schematic diagram showing the pierc-ing process of the solid billet by means of the inclined roll type piercer. Referring to Fig. 2, a left side is an inlet side and the solid billet 1 is subjected to the pierc-ing by means of the piercer to produce a first hollow piece 2. The piercer is provided with a piping 4 for supplying the high-pressure water in the vicinity of two pieces of barrel type rolls 3 thereof. The piping 4 is provided with a plurality of nozzle 5 and the high-pressure water is blasted onto the surface of the rolls 3 through the nozzles 5. In addition, the rolls 3 are provided with a brush 6 for descaling the surface thereof. And, when the solid billet 1 is subjected to the piercing, the high-pressure water is blasted through the nozzles 5 to remove titanium oxides stuck to the surface of the rolls 3 by means of said brush 6.
The respective solid billets were subjected to the 4~1 _ piercing with descaling under the descaling conditions shown in Table 4 to produce the first hollow piece. A piercing efficiency and the miss-roll rate in this time are shown in Table 4. In addition? a substance A in Table 4 is formed of pure titanium (JIS H-4630) and a substance B is formed of a titanium alloy (Ti-6Al-4V).
It is found from the results shown in Table 4 that the slip of the solid billet due to titanium oxides left on the surface of the inclined rolls can be prevented by providing the brush on the inclined rolls and descaling the inclined rolls by blasting the high-pressure water having a water pressure of 50 kg/cm2 or more to enhance the stability of the p-iercing, by means of the inclined roll type piercer.
In addition, such the descaling treatment is effective for an increase of the stability of the operation also in the second piercing process from the first hollow plece to the second hollow piece.
Next, the reducing process using the reducer mill will be described.
Characteristics of titanium are greatly dependent upon temperature and in particular when it is subjected to the reducing under the condition that the temperature at the in-let side of the reducer mill is lower than 600 C, its deformability is worsened, so that flaws, such as skin erup-tion-like, striped, edge marks and holes due to the jamming 200t~
of the rolls, are produced. In addition, titanium alloys produce voids on the boundary surface between the a-phase and the ~-phase when they are subjected to the deformation due to a difference between the a-phase and the ~-phase in deformability. On the contrary, when they are subjected to the reducing under the condition that the temperature at the inlet side of the reducer mill exceeds 1,100 C, coarse acicular structures are produced due to the cooling after the reducing. These acicular structures have a poor room-temperature ductility and deteriorate mechanical properties of the product. Accordingly, the temperature of the hollow shell at the inlet side of the reducer is set at 600 to 1 , 1 00 C .
If the reduction of outside diameter in the reducing exceeds 80 %, outer-surface flaws, such as stripe-like and edge marks due to the jamming of the rolls, are produced and the surface properties of the product are deteriorated even though the temperature of the hollow shell at the inlet side of the reducer mill is suitably controlled. Accordingly, the reduction of outside diameter in the reducing is set at 80 % or less. In addition, the reducer mill is used as shape-regulating and correcting means at the small reduction of outside diameter according to circumstances. In this case, no evil influence occurs, so that the lower limit of the reduction of outside diameter is not specially limited.
200.'2~
A solid billet having an outside diameter of 187 mm and a length of 2,250 mm formed of industrial pure titanium having the composition shown in Table 5 (JIS H-4630-3) was subjected to the piercing by means of an inclined roll type piercer at the temperature at the inlet side of the piercer of 1,050 C to be turned into a first hollow piece having an outside diameter of 192 mm, a wall-thickness of 20.62 mm and a length of 5,470 mm and the resulting first hollow piece was subjected to the hollow piece sizing by means of a shell sizer at the temperature at the inlet side of the shell-sizer of 1,000 C to obtain a third hollow piece having an outside diameter of 168 mm, a wall-thickness of 22.0 mm and a length of 6,020 mm.
Successively, the obtained third hollow piece was sub-jected to the elongating by means of a 7-stand mandrel mill at the temperature at the inlet side of the mandrel mill of 900 C to obtain a hollow shell having an outside diameter of 140 mm, a wall-thickness of 6.0 mm and a length of 24,040 mm. In this time, an elongation ratio was set at 4.
Subsequently, the obtained hollow shell was reheated and subjected to the reducing by means of a 3-roll 24-stand reducer mill at the temperature at the inlet side of the re-ducer mill of 850 CC (constant) with varying the reduction of outside diameter. Properties of the seamless tube formed of pure titanium after the reducing and those of the seam-~ 20().~
less tube formed of pure titanium after annealing for 1 hourat 750 C are shown in Table 6. In addition, properties and characteristics of the hollow shell before the reducing and the standard values for the hollow shell formed of indus-trial pure titanium (JIS H-4630-3) of the same one grade produced by the hot extrusion and the cold drawing in com-bination are shown in Table 6 for reference.
In the case (No. 6~ where the reduction of outside dia-meter exceeded 80 %, a notable jamming of rolls and edge marks were produced while in the case where the reduction of outside diameter was 80 % or less, good surface properties were obtained and also mechanical characteristics meet all of the standard values for the hollow shell produced by the hot extrusion and the cold drawing in combination.
The results obtained when the same one hollow shell was subjected to the reducing until an outside diameter of 63.6 mm and a wall-thickness of 5.75 mm (reduction of outside diameter: 54.6 %~ at various temperatures are shown in Table 7. In the case where the temperature at the inlet side of the mill is 500 DC (No. 1), a rough skin is produced on an inner surface of the hollow shell but in the case where the temperature at the inlet side of the mill is 600 to 1,100 C
(No. 2 to 4), both the surface properties and the mechanical characteristics are good.
Subsequently, a Ti-6Al-4V alloy having a composition 20(~
shown in Table 8 was subjected to the same test as above described. The results are shown in Tables 9, 10.
As obvious from Tables 9, 10, the reducing conditions according to the present invention in using the reducer mill are effective also for the hollow shell formed of titanium alloys.
The titanium material is anisotropic in deformation, so that its degree of polygon formation is increased in com-parison with that of plain carbon steels and also its phase characteristics are difference from those of plain carbon steels in the hollow reducing such as the reducing.
Figs. 3, 4 are graphs showing a polygon formation phase produced in the case where the reducing is conducted in a 3-grooved roll stand. Fig. 3 shows a positive phase and Fig.
4 shows a negative phase. Although it is described in de-tail later, most of plain carbon steels show the positive phase while titanium is apt to show the negative phase.
In order to suppress the polygon formation in the re-ducing, it has been known that the regulation of the projec-tion shape of the roll-contact surface hatched in Fig. 5 when projected in a direction shown by an arrow is effec-tive. In case of plain carbon steels, the roll groove is designed so that the projection shape of this roll-contact surface may be rectangular. That is to say, in the reducing of plain carbon steels, the rectangular ratio of rolls ZOO.~
(contact-length LE of an edge portion / contact-length LG of a groove portion) is brought close to 1 and a uniform out-side pressure deformation is added in a circumferential direction to make a quantity of deformation in wall-thick-ness uniform in the circumferential direction, whereby sup-pressing the polygon formation.
This design method presupposes the calculation of the contact-area on the basis of the shape of the roll grooves between the preceding stand and the present stand. Since the roll groove is not perfectly filled with the tube, the actual contact-area is smaller than that calculated by the use of the design rectangular rate. One of reasons for this is the reduction of the outside diameter by the tension of the tube between the stands.
The titanium material is anisotropic in deformation, so that it is difficult to be deformed in the circumferential direction and the reduction of outside diameter between the stand is smaller in comparison with that of steels. As a result, the actual rectangular ratio of the contact-surface of the hollow shell for the roll groove is larger in com-parison with that of the plain carbon steels. Thus, the polygon phase showing the positive phase of the plain carbon steels is apt to be turned into the negative phase in case of titanium. Accordingly, the conventional measure against the polygon formation phenomenon, in which the rectangular 20~
ratio of roll grooves is brought close to 1, brings about the opposite effect in case of titanium.
Fig. 6 is a graph showing a relation between the rec-tangular ratio of roll grooves and the degree of polygon formation when the hollow shell formed of plain carbon steels (C % = 0.2 %) and pure titanium is subjected to the reducing at the reduction of outside diameter of 55 % and t/D = 17 %. In case of the plain carbon steels, the degree of polygon formation amounts to about + 20 % at the rec-tangular rate of roll grooves of 0.8 or more and it is reduced less than 10 % at the rectangular rate of roll grooves of 1Ø On the contrary, in case of pure titanium, the negative polygon formation is brought about and its rate is increased with the approach of the rectangular ratio of roll grooves to 1.
According to the investigation by the present inven-tors, the rectangular ratio A of roll grooves effective for suppressing the polygon formation in the case where titanium material is subjected to the reducing, as shown in Fig. 7, is varied depending upon the ratio t/D, which is a ratio of the wall-thickness t to the finishing outside diameter D by the reducer mill and the following relations hold good.
When t/D < 10 %, A S 0.7;
when 10 % S t/D < 15 %, A S 0.8; and when 15 % S t/D, A S 0-9-20()~
In view of this point, in the above described preferredembodimentl the roll groove is designed so that the rec-tangular ratio of all reducing rolls excepting the inter-meshing guide rolls and finishing rolls may be 0.8, whereby the degree of polygon formation is suppressed to 15 % or less in the absolute value. In addition, in view of no problem in the properties of the inner and outer sùrfaces and the completion of the reducing, the lower limit of the rectangular ratio of roll grooves is set at O or more, pre-ferably 0.2 or more when t/D < 10 %, 0.3 or more when 10 %
t/D < 15 %, and 0.4 or more when 15 ~ t/D.
Although the polygon formation after the reducing does not deal the product a fatal defect, it goes without saying that the quality of the product can be still more improved by suppressing it. In addition, the degree of polygon for-mation is a value shown by the following equation.
The degree oi polygon formation =
t - t i X 100 (%) (D/2 - tmin) X 0.135 D: Nominal diameter;
timaX: Maximum wall-thickness in one side of a hexagon;
timin: Minimum wall-thickness in one side of a hexagon;
200~
~ timaX
tmax = 6 ~ ti min tmin = 6 timin = Min (timin) Next, the sizing process using the sizer mill will be described.
The temperature of the hollow shell at the inlet side of the sizer mill is set at 550 to 1,150 C due to the same reasons as those for the above described temperature at the inlet side of the reducer mill.
On the other hand, if the reduction of outside diameter in the sizing process is less than 3 %, the object of the sizing can not be achieved and the dimensional accuracy of the product is deteriorated. On the contrary, if the reduc-tion of outside diameter exceeds 15 %, surface defects, such as stripe flaws and edge marks due to the jamming of rolls, are produced to deteriorate the surface properties of the product. Accordingly, the reduction of outside diameter in the sizing is set at 3 to 15 %.
A solid billet formed of industrial pure titanium (JIS
H-4630-3) having the composition shown in Table 11 and hav-ing an outside diameter of 173 mm and a length of 2,040 mm 20().~
-was subjected to the piercing by means of an inclined type piercer at the temperature at the inlet side of the piercer of 990 to 1,250 C to be turned into a first hollow piece having an outside diameter of 178 mm, a wall-thickness of 40 mm and a length of 2,710 mm and the resulting first hollow piece was subjected to the second piercing (elongating~ by means of an elongator at the temperature at the inlet side of the elongator of 880 to 1,200 CC to be turned into a second hollow piece having an outside diameter of 190 mm, a wall-thickness of 19.5 mm and a length of 4,500 mm.
Successively, the obtained second hollow piece was sub-jected to the elongating by means of a plug mill at the tem-perature at the inlet side of the plug mill of 660 to 1,150 C to be turned into a hollow shell having an outside diameter of 183 mm, a wall-thickness of 15 mm and a length of 5,940 mm. In this time, the elongation ratio is 1.3.
Subsequently, the obtained hollow shell was reheated to various kinds of temperature and then subjected to the sizing by means of a 2-roll-7-stand sizer mill with varying the reduction of outside diameter. Properties of a seamless tube formed of pure titanium after the sizing and room-tem-perature characteristics of the seamless tube formed of pure titanium after annealing for 1 hour at 750 C are shown in Table 12. In addition, also the standard values for a seam-less tube formed of industrial pure titanium (JIS H-4630-3) 200.~
of the same one grade manufactured by the hot extrusion and the cold drawing in combination are shown in Table 12.
In No. 1, since the temperature at the inlet side of the sizer mill is low, flaws are produced on the surface of the seamless tube, whereby the seamless tube lost the pro-duct value prior to the discussion of the mechanical proper-ties. In No. 6, since the temperature at the inlet side of the sizer mill is too high, the surface properties were good but the elongation was remarkably deteriorated. In No. 8, since the temperature at the inlet side of the sizer mill is suitable but the reduction of outside diameter is insuffi-cient, the desired dimensional accuracy could not be se-cured. In No. 10, since the reduction of outside diameter is too large, the surface defects were produced and thus the seamless tube lost the product value.
On the contrary to the above described comparative examples, in Nos. 2 to 5, 7 and 9 according to the present invention, the surface properties are good and the mechan-ical characteristics meet all the standard values for the seamless tube by the hot extrusion and the cold drawing in combination.
Next, the same one test as the above described one was conducted for a Ti-6Al-4V alloy having a composition shown in Table 13. The results are shown in Table 14.
As obvious from Table 14, the sizing method according 200~
to the present invention is effective also for the produc-tion of a hollow shell formed of titanium alloys.
In addition, although the hollow shell is produced by the elongating in the respective preferred examples, it is not limitative. For example, a hollow shell produced by piercing by means of the inclined roll, a hollow shell produced by the extrusion, a hollow shell produced by the simply mechanical piercing and the like can be subjected to the reducing or the sizing. Furthermore, also the reducer mill or sizer mill having a construction other than the above described ones may be used. Besides, also the sur-face-machining or cold drawing can be conducted after the reducing or the sizing.
As this invention may be embodied in several forms without departing from the spirit of essential characteris-tics thereof, the present embodiment is therefore illustra-tive and not restrictive, since the scope of the invention is defined by the appended claims rather than by the de-scription preceding them, and all changes that fall within the meets and bounds of the claims, or equivalence of such meets and bounds thereof are therefore intended to be em-braced by the claims.
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as _ -able 7 ~ ` Reducing Condition Room-temperature Tensile , Properties N~ Temperature at Inlet Reduction of Size (outside diameter mmProperty of Product Evaluation - side of Rolling Mill Outside Diameter Xwall-thickness mm) YS W mmZ) TS~kg/mm2) E ~ a , ;; (~) (%) 1 500 * 54.6 63.5 x 5.75Crack in Inner Surface 95.5 58.2 - x 2 600 54.6 63.5 x 5.75 Good 41.9 56.8 26.4 O
3 850 54.6 63.5 x5.75 Good 39.5 54.2 28.5 0 $ 4 1100 54.6 63.5 x5.75 Good 37.1 51.2 28.5 0 1150 * 54.6 63.5 X 5.75Jamming of Rolls 25.9 47.1 11.1 x JIS-H4630-3 - 49 /63 18 or more - g * Out of conditions of the invention 2~J
::
.
,~
, Table 8 ~; ~ (wt9 ,~ O F e C N H A e V
0.27 o.æ 0.07 0.006 0.002 6.03 4.10 Table 9 .
Reducing Condition Room-temperature Tensile Property ofProperties ~-~. Nl Temperature at Inlet Reduction of Size (outside diameter mm Product Evaluation :~ side of Rolling Mill Outside Diameter Xwall-thickness mm) YS(kg/mmZ) TS(kg/mm~) E e (~
C~ c) (~
' 1 850 9.2 127 x6.25 Good 92.8 100.1 17.2 0 1~
2 850 36.5 88.9 x~.o Good 93.7 l00.9 18.0 2 3 850 54.6 63.5 x 5.75 Good 94.1 101.9 17.4 0 IV
4 850 69.5 42.7 x 5.5 Good 95.1 102.3 17.3 0 850 78.5 30.0 X5.25 Good 96.9 103.1 16.8 0 . 6 850 80.5 * 27.2 x5.25 Jamming of Rolls 97.1 103.3 17.2 x Edge Mark * Out of conditions of the invention . ..
! . ' Table 10 .
~- Reducing Condition Room-temperature Tensile Properties v N~ Temperature at Inlet Reduction of Size (outside diameter mmProperty of Product Evaluation ^~, side of Rolling Mill Outside Diameter x wall-thickness mn~ YS(kg/mmZ) TS~hg/mmZ) E ~ (~S~
-,, (~) (~
!~ 1 500 * 54.6 63.5X5.75 Cracks, Voids - - - x . .
~: 2 600 54.6 63.5X5.75 Good 99.8 105.9 17.4 O
~`!
3 850 54.6 63.5X5.75 Good 94.1 101.9 17.4 O
c~ 4 1100 54.6 63.5X5.75 Good 92.3 102.3 11.9 O
: 5 1150 * 54.6 63.5X5.75 Rough Skin on Surface 90.2 100.9 3.8 x N
.~ O
¦ ~ Out of conditions of the invention ~, .
..
,. . .
, .
..
., :
, .
P' .
. Table 11 (wt9 O F e C N H
` 0.27 0.220.07 0.006 0.002 Table 12 Hollow Shell Sizin~f Condition Room-temperature Tensile P~opelly of Properties Nl Te~perature at Inlet Reduction of Product Evaluation side of SizerOutside Diameter YS(kg/mm7 TS~kg~mmZ) E ~ a i (~) (~
1 500 * 8.0 Flaws - - - x N
f 2 550 8.0 Good 44.1 59.0 29.0 0 8 3 700 8.0 Good 43.5 57.9 30-5 4 gOO 8.0 Good 43.0 58.1 30.2 0 ~P
1150 8.0 Good 42.8 57.0 28.2 0 ! 6 1200 * 8.0 Good 40.0 55.2 9.5 x 7 700 3.0 Good 41.1 53.5 32.2 0 8 700 2.5 * Insufficiency of - - - x Outside Diameter 9 900 15.0 Good 43.8 58.0 30.0 0 900 16.0 * Flaws - - - x JIS-H4630-3 - 49 / 63 18 or more * Out of conditions of the invention ..
`~ Table 13 ` (wt9 O F e C N H A ~ V
0.27 o.æ 0.07 0.006 0.002 6.03 4.10 Table 14 Hollow Shell Sizing Condition Room-temperature Tensile Property of Properties Nl Temperature at Inlet Reduction of Product Evaluation side of Sizer Outside Diameter YS(kg/mm2) TS(kg/mm2) E ~ (9~
Il 500 ~ 6.0 Flaws - - - x 12 550 6.0 Good 95.8 105.0 20.3 13 600 6.0 Good 95.2 104.8 20.5 O
14 900 6.0 Good 95.0 104.2 21.0 O iP
1150 6.0 Good 93.1 102.3 21.2 O
16 1200 * 6.0 Good 92.0 101.0 3.8 x 7` 17 700 3.0 Good 94.9 104.1 20.6 O
.
18 700 2.5 * Insufficiency of - - - x .. Outside Diameter 19 900 15.0 Good 95.3 105.0 20.0 O
` 20 900 16.0 * Flaws - - - x * Out of conditions of the invention
! . ' Table 10 .
~- Reducing Condition Room-temperature Tensile Properties v N~ Temperature at Inlet Reduction of Size (outside diameter mmProperty of Product Evaluation ^~, side of Rolling Mill Outside Diameter x wall-thickness mn~ YS(kg/mmZ) TS~hg/mmZ) E ~ (~S~
-,, (~) (~
!~ 1 500 * 54.6 63.5X5.75 Cracks, Voids - - - x . .
~: 2 600 54.6 63.5X5.75 Good 99.8 105.9 17.4 O
~`!
3 850 54.6 63.5X5.75 Good 94.1 101.9 17.4 O
c~ 4 1100 54.6 63.5X5.75 Good 92.3 102.3 11.9 O
: 5 1150 * 54.6 63.5X5.75 Rough Skin on Surface 90.2 100.9 3.8 x N
.~ O
¦ ~ Out of conditions of the invention ~, .
..
,. . .
, .
..
., :
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. Table 11 (wt9 O F e C N H
` 0.27 0.220.07 0.006 0.002 Table 12 Hollow Shell Sizin~f Condition Room-temperature Tensile P~opelly of Properties Nl Te~perature at Inlet Reduction of Product Evaluation side of SizerOutside Diameter YS(kg/mm7 TS~kg~mmZ) E ~ a i (~) (~
1 500 * 8.0 Flaws - - - x N
f 2 550 8.0 Good 44.1 59.0 29.0 0 8 3 700 8.0 Good 43.5 57.9 30-5 4 gOO 8.0 Good 43.0 58.1 30.2 0 ~P
1150 8.0 Good 42.8 57.0 28.2 0 ! 6 1200 * 8.0 Good 40.0 55.2 9.5 x 7 700 3.0 Good 41.1 53.5 32.2 0 8 700 2.5 * Insufficiency of - - - x Outside Diameter 9 900 15.0 Good 43.8 58.0 30.0 0 900 16.0 * Flaws - - - x JIS-H4630-3 - 49 / 63 18 or more * Out of conditions of the invention ..
`~ Table 13 ` (wt9 O F e C N H A ~ V
0.27 o.æ 0.07 0.006 0.002 6.03 4.10 Table 14 Hollow Shell Sizing Condition Room-temperature Tensile Property of Properties Nl Temperature at Inlet Reduction of Product Evaluation side of Sizer Outside Diameter YS(kg/mm2) TS(kg/mm2) E ~ (9~
Il 500 ~ 6.0 Flaws - - - x 12 550 6.0 Good 95.8 105.0 20.3 13 600 6.0 Good 95.2 104.8 20.5 O
14 900 6.0 Good 95.0 104.2 21.0 O iP
1150 6.0 Good 93.1 102.3 21.2 O
16 1200 * 6.0 Good 92.0 101.0 3.8 x 7` 17 700 3.0 Good 94.9 104.1 20.6 O
.
18 700 2.5 * Insufficiency of - - - x .. Outside Diameter 19 900 15.0 Good 95.3 105.0 20.0 O
` 20 900 16.0 * Flaws - - - x * Out of conditions of the invention
Claims (21)
1. A method of manufacturing a seamless tube formed of a titanium material by the use of the Mannesmann's method com-prising a first process, in which an ingot formed of pure titanium or titanium alloy is heated to be turned into a solid billet; a second process, in which the resulting solid billet is subjected to a piercing to be turned into a hollow piece; a third process, in which the resulting hollow piece is subjected to an elongating to be turned into a hollow shell; and a fourth process, in which the resulting hollow shell is subjected to a sizing or a reducing;
characterized in that in said first process said ingot is heated within a temperature range of 850 to 1,250 °C, the final temperature being set within a range of 600 to 1,100 °C, and a working degree being set at 50 % or more, and, in said second process said solid billet is subjected to the piercing within a temperature range of .beta. transus - 100 to 1,250 °C.
characterized in that in said first process said ingot is heated within a temperature range of 850 to 1,250 °C, the final temperature being set within a range of 600 to 1,100 °C, and a working degree being set at 50 % or more, and, in said second process said solid billet is subjected to the piercing within a temperature range of .beta. transus - 100 to 1,250 °C.
2. A method of manufacturing a seamless tube formed of a titanium material as set forth in Claim 1, wherein said titanium alloy is an .alpha.-type titanium alloy.
3. A method of manufacturing a seamless tube formed of a titanium material as set forth in Claim 2, wherein said .alpha.-type titanium alloy is one selected from the group consist-ing of Ti-0.15Pd, Ti-0.8Ni-0.3Mo and Ti-5Al-2.5Sn.
4. A method of manufacturing a seamless tube formed of a titanium material as set forth in Claim 1, wherein said titanium alloy is an .alpha. + .beta.-type titanium alloy.
5. A method of manufacturing a seamless tube formed of a titanium material as set forth in Claim 4, wherein said .alpha. + .beta.-type titanium alloy is one selected from the group consisting of Ti-8Al-1Mo-1V, Ti-3Al-2.5V, Ti-6Al-4V, Ti-6Al-6V-2Sn, Ti-6Al-2Sn-4Zr-6Mo and Ti-6Al-2Sn-4Zr-2Mo.
6. A method of manufacturing a seamless tube formed of a titanium material as set forth in Claim 1, wherein said titanium alloy is a .beta.-type titanium alloy.
7. A method of manufacturing a seamless tube formed of a titanium material as set forth in Claim 1, further compris-ing, between said second process and said third process, an elongating process or a hollow piece sizing process for regulating a size of said hollow piece.
8. A method of manufacturing a seamless tube formed of a titanium material by the use of the Mannesmann's method comprising a first process, in which an ingot formed of pure titanium or titanium alloy is heated to be turned into a solid billet; a second process, in which the resulting solid billet is subjected to a piercing by means of a piercer having inclined rolls to be turned into a hollow piece; a third process, in which the resulting hollow piece is sub-jected to an elongating to be turned into a hollow shell;
and a fourth process, in which the resulting hollow shell is subjected to a sizing or a reducing;
characterized in that said inclined rolls are provided with a nozzle for blasting a high-pressure water of 50 kg/cm2 or more and a brush for cleaning said inclined rolls and in said second process said solid billet is subjected to the piercing with descaling.
and a fourth process, in which the resulting hollow shell is subjected to a sizing or a reducing;
characterized in that said inclined rolls are provided with a nozzle for blasting a high-pressure water of 50 kg/cm2 or more and a brush for cleaning said inclined rolls and in said second process said solid billet is subjected to the piercing with descaling.
9. A method of manufacturing a seamless tube formed of a titanium material as set forth in Claim 8, wherein said ingot is heated within a temperature range of 850 to 1,250 °C, the final temperature being set within a range of 600 to 1,100 °C, a working degree being set at 50 % or more to obtain said solid billet, and the resulting solid billet being subjected to the piercing within a temperature range of .beta. transus - 100 to 1,250 °C to be turned into said hollow piece.
10. A method of manufacturing a seamless tube formed of a titanium material by the use of the Mannesmann's method comprising a first process, in which an ingot formed of pure titanium or titanium alloy is heated to be turned into a solid billet; a second process, in which the resulting solid billet is subjected to a piercing to be turned into a hollow piece; a third process, in which the resulting hollow piece is subjected to an elongating to be turned into a hollow shell; and a fourth process, in which the resulting hollow shell is subjected to a reducing;
characterized in that in said fourth process said hol-low shell is subjected to the reducing by means of a reducer mill, a temperature of said hollow shell at an inlet side of said reducer mill being set at 600 to 1,100 °C, and a reduction of outside diameter being set at 80 % or less.
characterized in that in said fourth process said hol-low shell is subjected to the reducing by means of a reducer mill, a temperature of said hollow shell at an inlet side of said reducer mill being set at 600 to 1,100 °C, and a reduction of outside diameter being set at 80 % or less.
11. A method of manufacturing a seamless tube formed of a titanium materiel as set forth in Claim 10, further compris-ing, between said second process and said third process, an elongating process or a hollow piece sizing process for regulating a size of said hollow piece.
12. A method of manufacturing a seamless tube formed of a titanium material as set forth in Claim 10, wherein a rec-tangular ratio (.lambda.) of roll grooves in said reducer mill is set as below according to a wall-thickness (t) and an out-side diameter (D) of the seamless tube to be manufactured, When t/D is less than 10 %, .lambda. ? 0.7;
when 10 % ? t/D < 15 %, .lambda. ? 0.8; and when t/D is 15 % or more, .lambda. ? 0.9.
when 10 % ? t/D < 15 %, .lambda. ? 0.8; and when t/D is 15 % or more, .lambda. ? 0.9.
13. A method of manufacturing a seamless tube formed of a titanium material as set forth in Claim 10, wherein in said third process said hollow piece is subjected to the elon-gating by means of a mandrel mill.
14. A method of manufacturing a seamless tube formed of a titanium material as set forth in Claim 10, wherein said ingot is heated within a temperature range of 850 to 1,250 °C, the final temperature being set within a range of 600 to 1,100 °C, a working degree being set at 50 % or more to obtain said solid billet, and the resulting solid billet being subjected to the piercing within a temperature range of .beta. transus - 100 to 1,250 °C to be turned into said hollow piece.
15. A method of manufacturing a seamless tube formed of a titanium material by the use of the Mannesmann's method com-prising a first process, in which an ingot formed of pure titanium or titanium alloy is heated to be turned into a solid billet; a second process, in which the resulting solid billet is subjected to a piercing to be turned into a hollow piece; a third process, in which the resulting hollow piece is subjected to an elongating to be turned into a hollow shell; and a fourth process, in which the resulting hollow shell is subjected to a sizing;
characterized in that in said fourth process said hol-low shell is subjected to the sizing by means of a sizer mill, a temperature of said hollow shell at an inlet side of said sizer mill being set at 550 to 1,150 °C, and a re-duction of outside diameter being set at 3 to 15 %.
characterized in that in said fourth process said hol-low shell is subjected to the sizing by means of a sizer mill, a temperature of said hollow shell at an inlet side of said sizer mill being set at 550 to 1,150 °C, and a re-duction of outside diameter being set at 3 to 15 %.
16. A method of manufacturing a seamless tube formed of a titanium material as set forth in Claim 15, further compris-ing, between said second process and said third process, an elongating process or a hollow piece sizing process for regulating a size of said hollow piece.
17. A method of manufacturing a seamless tube formed of a titanium material as set forth in Claim 15, wherein in said third process said hollow piece is subjected to the elongat-ing by means of a plug mill.
18. A method of manufacturing a seamless tube formed of a titanium material as set forth in Claim 15, wherein said ingot is heated within a temperature range of 850 to 1,250 °C, the final temperature being set within a range of 600 to 1,100 °C, a working degree being set at 50 % or more to obtain said solid billet, and the resulting solid billet being subjected to the piercing within a temperature range of .beta. transus - 100 to 1,250 °C to be turned into said hollow piece.
19. A method of manufacturing a seamless tube formed of a titanium material by the use of the Mannesmann's method comprising a first process, in which an ingot formed of pure titanium or titanium alloy is heated to be turned into a solid billet; a second process, in which the resulting solid billet is subjected to a piercing to be turned into a first hollow piece; a third process, in which the resulting first hollow piece is subjected to an elongating to be turned into a second hollow piece; a fourth process, in which the re-sulting second hollow piece is subjected to an elongating to be turned into a hollow shell; and a fifth process, in which the resulting hollow shell is subjected to a sizing;
characterized in that in said first process said ingot is heated within a temperature range of 850 to 1,250 °C, the final temperature being set within a range of 600 to 1,100 °C, and a working degree being set at 50 % or more, and, in said second process said solid billet is subjected to the piercing within a temperature range of .beta. transus - 100 to 1,250 °C.
characterized in that in said first process said ingot is heated within a temperature range of 850 to 1,250 °C, the final temperature being set within a range of 600 to 1,100 °C, and a working degree being set at 50 % or more, and, in said second process said solid billet is subjected to the piercing within a temperature range of .beta. transus - 100 to 1,250 °C.
20. A method of manufacturing a seamless tube formed of a titanium material by the use of the Mannesmann's method com-prising a first process, in which an ingot formed of pure titanium or titanium alloy is heated to be turned into a solid billet; a second process, in which the resulting solid billet is subjected to a piercing by means of a piercer hav-ing inclined rolls to be turned into a first hollow piece; a third process, in which the resulting first hollow piece is subjected to an elongating by means of an elongator having inclined rolls to be turned into a second hollow piece; a fourth process, in which the resulting second hollow piece is subjected to an elongating to be turned into a hollow shell; and a fifth process, in which the resulting hollow shell is subjected to a sizing or a reducing;
characterized in that said inclined rolls of said piercer and/or said elongator are provided with a nozzle for blasting a high-pressure water of 50 kg/cm2 or more and a brush for cleaning the inclined rolls and in said second and/or third process said solid billet is subjected to the piercing and/or said first hollow piece is subjected to the elongating with descaling.
characterized in that said inclined rolls of said piercer and/or said elongator are provided with a nozzle for blasting a high-pressure water of 50 kg/cm2 or more and a brush for cleaning the inclined rolls and in said second and/or third process said solid billet is subjected to the piercing and/or said first hollow piece is subjected to the elongating with descaling.
21. A method of manufacturing a seamless tube formed of a titanium material as set forth in Claim 20, wherein said ingot is heated within a temperature range of 850 to 1,250 °C, the final temperature being set within a range of 600 to 1,100 °C, a working degree being set at 50 % or more to obtain said solid billet, and the resulting solid billet being subjected to the piercing within a temperature range of .beta. transus - 100 to 1,250 °C to be turned into said hollow piece.
Applications Claiming Priority (6)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP29302788A JPH02137604A (en) | 1988-11-18 | 1988-11-18 | Manufacture of seamless tube of alpha+beta type titanium alloy |
| JP63-293027 | 1988-11-18 | ||
| JP31722788A JPH02160102A (en) | 1988-12-14 | 1988-12-14 | Method for reducing rolling titanium stock |
| JP63-317226 | 1988-12-14 | ||
| JP63-317227 | 1988-12-14 | ||
| JP31722688A JPH02160103A (en) | 1988-12-14 | 1988-12-14 | Method for sizing rolling titanium stock |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CA2003244A1 CA2003244A1 (en) | 1990-05-18 |
| CA2003244C true CA2003244C (en) | 1994-08-02 |
Family
ID=27337788
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA 2003244 Expired - Lifetime CA2003244C (en) | 1988-11-18 | 1989-11-17 | Method of manufacturing seamless tube formed of titanium material |
Country Status (1)
| Country | Link |
|---|---|
| CA (1) | CA2003244C (en) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112044979A (en) * | 2019-12-30 | 2020-12-08 | 宁夏中色金航钛业有限公司 | Low-bursting-rate pure titanium seamless tube for metal corrugated tube and production process thereof |
| CN114799738B (en) * | 2022-03-24 | 2023-12-22 | 新疆湘润新材料科技有限公司 | Preparation method of TC4 titanium alloy thin-wall ring material |
| CN114653793B (en) * | 2022-03-30 | 2023-08-04 | 西部金属材料股份有限公司 | Preparation method of titanium alloy forming part and preparation method of titanium alloy thin-wall section bar |
-
1989
- 1989-11-17 CA CA 2003244 patent/CA2003244C/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| CA2003244A1 (en) | 1990-05-18 |
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