Abstract:
The present invention pertains to steel with high mechanical resistance at room temperature and up to 130° C., good toughness and good corrosion resistance in the metal base as well as good resistance to cracking in the heat affected zones (HAZ) once the tubing is welded together, and more specifically to heavy gauge seamless steel tubing with high mechanical resistance, good toughness and good corrosion resistance called catenary conduit. The advantages of the present invention with respect to those of an the state of technology reside in providing a chemical composition for steel used to manufacture heavy gauge seamless steel tubing with high mechanical resistance, good toughness, good fissure resistance in the HAZ and good corrosion resistance and a process for manufacturing this product. These advantages are obtained by using a composition made up basically of Fe and a specific chemical composition.

Description:
FIELD OF THE INVENTION  
       [0001]     The present invention refers to steel with good mechanical strength, good toughness and which is corrosion resistant, more specifically to heavy gauge seamless steel tubing, with good mechanical strength, good toughness to prevent cracking in the metal base as well as in the heat affected zone, and corrosion resistant, called conduit, of catenary configuration, to be used as a conduit for fluids at high temperatures, preferably up to 130° C. and high pressure, preferably up to 680 atm and a method for manufacturing said tubing.  
       BACKGROUND OF THE INVENTION  
       [0002]     In the exploitation of deep sea oil reserves, fluid conduits called conduits of catenary configuration, commonly know in the oil industry as Steel Catenary Risers are utilized. These conduits are placed at the upper part of the underwater structure, that is, between the water surface and the first point at which the structure touches the sea bed and is only one part of the complete conduction system.  
         [0003]     This canalization system is essentially made up of conduit tubes, which serve to carry the fluids from the ocean floor to the ocean surface. At present this tubing is made of steel and is generally joined together through welding.  
         [0004]     There are several possible configurations for these conduits one of which is the asymmetric catenary configuration conduit. Its name is due to the curve which describes the conducting system which is fixed at both ends (the ocean bottom and the ocean surface) and is called a catenary curve.  
         [0005]     A conduit system such as the one described above, is exposed to the undulating movements of the waves and the ocean currents. Therefore the resistance to fatigue is a very important property in this type of tubing, making the phenomena of the welded connections of the tubing a critical one. Therefore, restricted dimensional tolerances, mechanical properties of uniform resistance and high tenacity to prevent cracking in the metal base as well as in the heat affected zone, are the principle characteristics of this kind of tubing.  
         [0006]     At the same time, the fluid which circulates within the conduit may contain H 2 S, making it also necessary for the product to be highly resistant to corrosion.  
         [0007]     Another important factor that should be taken into account is that the fluid which will be carried by the conduit is very hot, making it necessary for the tubes that make up the system to maintain their properties at high temperatures.  
         [0008]     Also, the medium in which the tubes must sometimes operate implies maintaining its operability even at very low temperatures. Many of the deposits are located at latitudes with very low temperatures, making it necessary for the tubing to maintain its mechanical properties even at these temperatures.  
         [0009]     Because of the afore described concepts and due to the exploitation of reserves at greater depths, the oil industry has found it necessary to use alloys of steel which allow for the obtaining of better properties than those used in the past.  
         [0010]     A common practice used to increase the resistance of a steel product is to add alloying elements such as C and Mn, to carry out a thermal treatment of hardening and tempering and to add elements which generate hardening through precipitation such as Nb and V. However, the type of steel products such as conduits not only require high resistance and toughness, but also other properties such as high resistance to corrosion, and high resistance to cracking in the metal base as well as in the heat affected zone once the tubing has been welded.  
         [0011]     It is a well known fact that the betterment in some of the properties of steel means determents in other properties, making the challenge to be met the obtaining of a material which provides an acceptable balance among the various properties.  
         [0012]     Conduits are tubes that, like conduit tubing, carry a liquid, a gas or both. Said tubing is manufactured under norms, standards, specifications and codes which govern the manufacturing of conduction tubes in most cases. Additionally, this tubing characterized and differentiated from the majority of standard conduction tube in terms of the range of chemical composition, the range of restricted mechanical properties (yielding, stress resistance and their relationship), low hardness, high toughness, dimensional tolerances restricted by the interior diameter and criteria of severe inspection.  
         [0013]     The design and manufacturing of steel used in heavy gauge tubing, presents problems not found in the manufacturing of tubes of lesser gauge, such as the obtaining of the correct hardening, a homogeneous mixture of the properties throughout the thickness and a homogeneous thickness throughout the tube and a reduced eccentricity.  
         [0014]     Still another more complex problem is the manufacturing of heavy gauge tubing which fulfills the correct balance of properties required for its performance as a conduit.  
         [0015]     In the state of the art, for the manufacturing of tubing to be used as conduits, we may refer to the document EP 1182268 of MIYATA Yukio and associates, which discloses an alloy of steel used for manufacturing conduction or conduit tubing.  
         [0016]     In this document the effects of the following elements are disclosed: C, Mo, Mn, N, Al, Ti, Ni, Si, V, B and Nb. Said document indicates that where the contents of carbon is greater than 0.06%, steel becomes susceptible to cracking and fissures during the tempering process.  
         [0017]     This is not necessarily valid, since even in heavy gauge tubes, and maintaining the rest of the chemical composition the same, no cracking is observed up to carbon contents of 0.13%.  
         [0018]     Furthermore, upon trying to reproduce the teachings of MIYATA and associates, it may be concluded that a material with a maximum range of carbon of 0.06% could not be used for the manufacturing of heavy gauge conduit since C is the main element which promotes the hardenability of the material and it would prove very costly to reach the high resistance required through the addition of other kinds of elements such as Molybdenum which also promotes, given a certain content, detriment in the toughness of the metal base as well as in the heat affected zone and Mn which promotes problems of segregation as we shall see in more detail later on. If the content of carbon is very low, the hardenability of the steel is affected considerably and therefore a thick heterogeneous a circular structure in the half-value layer of the tube would be produced, deteriorating the hardenability of the material as well as producing an inconsistency in the uniformity of resistance in the half-value layer of the tubing.  
         [0019]     Furthermore, in the MIYATA and associates document, it is shown that the content of Mn improves the toughness of the material, in the base material as well as in the welding heat affected zone. This affirmation is also incorrect, since Mn is an element which increases the hardenability of steel, thus promoting the formation of martensite, as well as promoting the constituent MA, which is a detriment to toughness. Mn promotes high central segregation in the steel bar from which tubing is made, even more in the presence of P. Mn is the element with the second highest index of segregation, and promotes the formation of MnS inclusions, and even when steel is treated with Ca, due to the problem of central segregation of Mn above 1.35%, said inclusions are not eliminated.  
         [0020]     With contents of over 1.35% Mn a significant negative influence is observed in the susceptibility to hydrogen induced cracking known as HIC. Therefore, Mn is the element with the second most influence on the formula CE (Carbon equivalent, formula 11W), with which the value of the content of final CE increases. High contents of CE imply welding problems with the material in terms of hardness. On the other hand, it is know that additives of up to 0.1% of V allow for the obtaining of sufficient resistance for this grade of heavy gauge tubes, although it is impossible to also obtain at the same time high toughness.  
         [0021]     One known way in which said tubes are manufactures is through the process of pilger mill lamination. If it is true that by way of this process high gauges of tubes may be obtained, it is also true that good quality in the surface finish of the tube is not obtained. This is because the tube being processed through pilger mill lamination acquires an undulated and uneven outer surface. These factors are prejudicial since they may lessen the collapse resistance which the tube must possess.  
         [0022]     On the other hand,the coating of tubes which do not have a smooth outer surface is complicated, and also the inspection for defects with ultrasound becomes inexact.  
         [0023]     Steel which may be used to manufacture tubes for conduction systems with catenary configurations, heavy gauges, high stress resistance and low hardenability, and which complies with the requirements of toughness to fissures and resistance to the propagation of fissures in the heat affected zones (HAZ), and resistance to corrosion, necessary for these types of applications has yet to be invented since without the quality of heavy gauges, the simple chemical composition and heat treatment do not allow for the obtaining of the characteristics necessary for this type of product.  
         [0024]     The precedents which have been analyzed indicate that the problem has not yet been integrally resolved, and that it is necessary to analyze other parameters and possible solutions in order to reach a complete understanding.  
       OBJECTIVE OF THE INVENTION  
       [0025]     The main objective of this invention is to provide a chemical composition for steel to be used in the manufacturing of seamless steel tube and a process for manufacturing which leads to a product with high mechanical resistance at room temperature and up to 130° C., high toughness, low hardenability, resistance to corrosion in medium&#39;s which contain H 2 S and high values of tenacity in terms of resistance to the advancing of fissures in the HAZ evaluated by the CTOD test (Crack Tip Opening Displacement).  
         [0026]     Still another objective is to make possible a product which possesses an acceptable balance of the above mentioned qualities and which complies with the requirements which a conduit for carrying fluids under high pressure, that is, above 680 atm, should have.  
         [0027]     Still another objective is to make possible a product which possesses a good degree of resistance to high temperatures. A fourth objective is to provide a heat treatment to which a seamless tube would be submitted which promotes the obtaining of the necessary mechanical properties and resistance to corrosion.  
         [0028]     Other objectives and advantages of the present invention will become apparent upon studying the following description and through the examples shown in the present description, which a-re of an illustrative but not limiting character.  
       BRIEF DESCRIPTION OF THE INVENTION  
       [0029]     Specifically, the present invention consists of, in one of its aspects, mechanical steel, highly resistant to temperatures from room -temperature to 130° C., with good toughness and low hardenability which also is highly resistant to corrosion and cracking in HAZ once the tube is welded to another tube to be used in the manufacturing of steel tubing which complies with underwater conduit systems.  
         [0030]     Another aspect of this invention is a method for manufacturing this type of tubing.  
         [0031]     With respect to the method, first an alloy is manufacture d with the desired chemical composition. This steel should contain percentages by weight of the following elements in the quantities described: C 0.06 to 0.13; Mn 1.00 to 1.30; Si 0.35 max.; P 0.015 max.; S 0.003 max.; Mo 0.10 to 0.20; Cr 0.10 to 0.30; V 0.050 to 0.10; Nb 0.020 to 0.035; Ni 0.30 to 0.45; Al 0.015 to 0.040; Ti 0.020 max.; Cu 0.2 max. and N 0.010 max.  
         [0032]     In order to guarantee a satisfactory hardenability of the material and good weldability, the aforementioned elements should satisfy the following relationships: 
 
0.5&lt;(Mo+Cr+Ni)&lt;1 
 
(Mo+Cr+V)/5+(Ni+Cu)/15≦0.14 
 
         [0033]     Steel thus obtained is solidified in blooms or bars which are then perforated and laminated into a tubular shape. The master tube is then adjusted to the final dimensions.  
         [0034]     In order to comply completely with the objectives planned for in the present invention, aside from the already defined chemical objectives, it has been determined that the gauge of the walls of the tubes should be established in the range of ≧30 mm.  
         [0035]     Next the steel tube is subjected to a thermal hardening and tempering treatment to bestow it with a microstructure and final properties.  
     
    
     BRIEF DESCRIPTION OF THE DRAWINGS  
       [0036]      FIG. 1  shows the Yielding Strength measured in Ksi and the transition temperature (FATT), measured in ° C., of various different steets designed by the inventor, used in the manufacturing of conduits. The chemical composition of the “BASE” alloys, “A”, “B”, “C”, “D”, “E”, and “F”, may be seen in Table 1.  
         [0037]      FIG. 2  shows the effect of different temperatures of austenticizing and tempering and the addition or not of Ti, on the Yielding Strength and the transition temperature (FATT), measured in ° C., of different alloys. The chemical composition of the different alloys that were analyzed can be seen in Table 2.  
         [0038]      FIG. 3  is a reference for a better understanding of  FIG. 2 , where the different temperatures of Austenticizing (Aust) and Tempering (Temp) used for each steel with or without the addition of Ti can be seen. 
     
    
       [0039]     Thus, the steel identified in  FIG. 2  with the number 1, possesses 0.001% Ti and has been austenticized at 920° C. and tempered at 630° C. This steel contains the chemical composition A, indicated in Table 2.  
         [0040]     Steel 17 (with chemical composition E) contains a larger amount of Ti (0.015%) and has been heat treated under the same conditions as the previously mentioned steel.  
         [0041]     In turn, the alloys A, 8, C, D, E, F and G have also been treated with other austenticizing and tempering temperatures, as indicated in  FIG. 3 .  
       DETAILED DESCRIPTION OF THE INVENTION  
       [0042]     The inventor has discovered that the combination of elements such as Nb—V—Mo—Ni—Cr among others, in predetermined amounts, leads to the obtaining of an excellent combination of stress resistance, toughness, hardenability, high levels of CTOD and good resistance to hydrogen induced cracking (HIC) in a metal base, as well as leading to the obtaining of high levels of CTOD in the heat affected zone (HAZ) of the welded joint.  
         [0043]     In turn, the inventor has discovered that this chemical composition allows for the elimination of the problems that occur in the manufacturing of high gauge conduits with the above presented characteristics.  
         [0044]     Different experiments were carried out in order to discover the best chemical composition of steel that would fulfill the above mentioned requirements. One of these consisted of the manufacturing of high gauge pieces with different alloying additives and then measuring the relation between the Yielding Strength/Ultimate Tensile Strength of each one.  
         [0045]     The results of these experiments can be seen in  FIG. 1 . As a starting point a “BASE” alloy with the chemical composition shown in Table 1 with the name “BASE” was used. It was proven that these properties could be improved through the addition of Mo and Ni to the alloy (Steel A).  
         [0046]     The next step was to reduce the content of C to 0.061% (Steel 8), observing that there was detriment to both values that were evaluated. Once again we started with Steel A, and V was eliminated from the composition (Steel C). In this case, the transition temperature improves slightly, but the Ultimate Tensile Strength of the material did not reach the minimum requirement.  
         [0047]     The next step was to experiment with the additive Cr. Cr was added to Steel A (resulting in Steel D), as well as to Steel C (resulting in Steel E). Both steels showed improvements in stress resistance as well as in the transition temperature, although Steel D better met the required standards.  
         [0048]     It was thus concluded that the best combination of resistance/transition temperature was obtained with the chemical composition of Alloy D.  
         [0049]     On successive occasions, the inventor has carried out other series of experiments to test three important factors which may affect the properties of the material used for the conduit: the content of Ti in an alloy, the effect of the size of the authentic grain and the tempering temperature during the thermal treatment of the steel.  
         [0050]     The inventor discovered that the increase in size in the dimension of the authentic grain from 12 microns to 20 microns produces an increase in the resistance of the steel, but at the same time worsens the factor of transition temperature. At the same time it as discovered that the addition of Ti to the alloy negatively affects the transition temperature.  
         [0051]     On the other hand, the inventor discovered that the variation in the tempering temperature of steel by approximately 30° C. produced no significant effect on the mechanical properties of the material, in the case of the alloy which did not contain Ti. However, in an alloy with a content of Ti of up to 0.015%, a lowering in the resistance was found when the tempering temperature was increased from 630° to 660° C.  
         [0052]     In  FIG. 2  the results of the tests may be seen. Four different casts were made with steel without Ti whose chemical composition is described in Table 2 with the letters A, B, C and D. Then three additional casts were made with chemical compositions similar to the previous ones but with the addition of Ti. The chemical composition of the casts is described in Table 2 with the letters E, F and G.  
         [0053]     It was observed that, with the addition of Ti to steels A, B, C and D, without taking into account the austenticizing and tempering temperatures to which they were subjected, there were negative results in the transition temperature, as shown in the properties of steel E, F and G which contain Ti. In the same figure it can be seen that the steel without Ti has a lower transition temperature than the steels to which Ti has been added.  
         [0054]     Following is the range of chemical compositions which were found to be optimum and which were used in the present invention  
         [0055]     C 0.06 to 0.13  
         [0056]     Carbon is the most economical element and that with the greatest impact on the mechanical resistance of steel, thus the percentage of its content cannot be too low. In order to obtain yielding strength ≧65 Ksi, it is necessary that the content of carbon be above 0.6% for heavy gauge tubes.  
         [0057]     In addition, C is the main element which promotes the hardenability of the material. It the percentage of C is too low, the hardenability of the steel is affected considerably and thus the tendency of the formation of a coarse acicular structure in the half-value layer of the tube will be characteristic. This phenomenon will lead to a less than desirable resistance for the material as well as resulting in detriment to the toughness.  
         [0058]     The content of C should not be above 0.13% in order to avoid a high degree of high productivity and low thermal hardening in the welding in the joint between one tube and another, and to avoid that the testing values of CTOD (carried out according to the. ASTM norm E 1290) in the metal base exceed 0.8 mm at up to −40° C. and to avoid that they exceed 0.5 mm at up to 0° C. in the HAZ. Therefore, the amount of C should be between 0.06 and 0.13%.  
         [0059]     Mn 1.00 to 1.30  
         [0060]     Mn is an element which increases the hardenability of steel, promoting the formation of martensite, as well as promoting the constituent MA, which is detrimental to the toughness. Mn promotes a high central segregation in the steel bar from which the tube is laminated. Also, Mn is the element with the second highest index of segregation, promoting the formation of MnS inclusions and even when steel is treated with Ca, due to the problem of central segregation due to the amount of Mn above 1.35%, said inclusions are not eliminated.  
         [0061]     On the other hand, with amounts of Mn above 1.35% a significant negative influence is seen in the susceptibility to hydrogen induced cracking (HIC), due to the previously described formation of MnS.  
         [0062]     Mn is the second most important element influencing the formula of CE (Carbon equivalent, Formula 11W), with which the end CE value is increased.  
         [0063]     A minimum of 1.00% of Mn must be insured and a combination with C in the ranges previously mentioned will guarantee the necessary hardenability of the material in order to meet The resistant requirements.  
         [0064]     Therefore, the optimum content of Mn should be in the range of 1.00 to 1.35 and more specifically should be in the range of 1.05 to 1.30%.  
         [0065]     Si 0.35 Max.  
         [0066]     Silicon is necessary in the process of steel manufacturing as a desoxidant and is also necessary to better stress resistance in the material. This element, like manganese, promotes the segregation of P to the boundaries of the grain; therefore it proves harmful and should be kept at the lowest possible level, preferably below 0.35% by weight.  
         [0067]     P 0.015 Max.  
         [0068]     Phosphorus is an inevitable element in metallic load, and an amount above 0.015% produces segregation on the boundaries of the grain, which lowers the resistance to HIC. It is imperative to keep the levels below 0.015% in order to avoid problems of toughness as well as hydrogen induced cracking.  
         [0069]     S 0.003 Max.  
         [0070]     Sulfur, in amounts above 0.003%, promotes, together with high concentrates of Mn, the formation of elongated MnS type inclusions. This kind of sulphide is detrimental to the resistance to corrosion of the material in the presence of H 2 S.  
         [0071]     Mo 0.1 to 0.2  
         [0072]     Molybdenum allows for a rise in the tempering temperature, and also prevents the segregation of fragilizing elements on the boundaries of the authentic grain.  
         [0073]     This element is also necessary for the improvement of the tempering of the material. It was discovered that the optimum minimal amount should be 0.1%. A maximum of 0.2% is established as an upper limit since above this amount, a decrease in the toughness of the body of the tube as well as in the heat affected zone of the welding is seen.  
         [0074]     Cr 0.10 to 0.30  
         [0075]     Chromium produces hardening through solid solution and increases the hardenability of the material, thus increasing its stress resistance. Cr is an element which also is found in the chemical makeup. That is why it is necessary to have a minimum amount of 0.10%, but, parallelly, an excess can cause problems of impairment. Therefore it is recommendable to keep the maximum amount at 0.30%.  
         [0076]     V 0.050 to 0.10  
         [0077]     This element precipitates in a solid solution as carbides and thus increases the material&#39;s stress resistance, therefore the minimum amount should be 0.050%. If the amount of this element exceeds 0.10% (and even if it exceeds 0.08%) the tensile strength of the welding can be affected due to an excess of carbides or carbonitrides in the mould. Therefore, the amount should be between 0.050 and 0.10%.  
         [0078]     Nb 0.020 to 0.035  
         [0079]     This element, like V, precipitates in a solid solution in the form or carbides or nitrides thus increasing the material&#39;s resistance. Also, these carbides or nitrides deter excessive growth of the grain. An excess amount of this element has no advantages and actually could cause the precipitation of compounds which can prove harmful to the toughness. That is why the amount of Nb should be between 0.020 and 0.035.  
         [0080]     Ni 0.30 to 0.45  
         [0081]     Nickel is an element which increases the toughness of the base material and the welding, although excessive additions end up saturating this effect. Therefore the optimum range for heavy gauge tubes should be 0.30 to 0.45%. It has been found that the optimum amount of Ni is 0.40%.  
         [0082]     Cu 0.2 Max.  
         [0083]     In order to obtain a good weldability of the material and to avoid the appearance of defects which could harm the quality of the joint, the amount of Cu should be dept below 0.2%.  
         [0084]     Al 0.015 to 0.040  
         [0085]     Like Si, Aluminum acts as a deoxidant in the steel manufacturing process. It also refines the grain of the material thus allowing for higher toughness values. On the other hand, a high Al content could generate alumina inclusions, thus decreasing the toughness of the material. Therefore, the amount of Aluminum should be limited to between 0.015 and 0.040%.  
         [0086]     Ti 0.020 Max.  
         [0087]     Ti is an element which is used for deoxization and to refine grains. Amounts larger than 0.020% and in the presence of elements such as N and C may form compounds such as carbonitrides or nitrides of Ti which are detrimental to the transition temperature.  
         [0088]     As seen in  FIG. 2 , it was proven that in order to avoid a marked decrease in the transition temperature of the tube, the amount of Ti should be no greater than 0.02%.  
         [0089]     N 0.010 Max.  
         [0090]     The amount of N should be kept below 100 ppm in order to obtain steel with an amount of precipitates which do not decrease the toughness of the material.  
         [0091]     The addition of elements such as Mo, Ni and Cr allow for the development after tempering of a lower bainite microstructure polygonal ferrite with small regions of martensite high in C with retained austenite (MA constituent) dispersed in the matrix.  
         [0092]     In order to guarantee a proper hardenability of the material, and good weldability, the elements described below should keep the relationship shown here: 
 
0.5&lt;(Mo+Cr+Ni)&lt;1; 
 
(Mo+Cr+V)/5+(Ni+Cu)/15≦0.14. 
 
         [0093]     It was also found that the size of the optimum authentic grain is form 9 to 10 according to ASTM.  
         [0094]     The inventor discovered that the chemical composition described lead to the obtaining of an adequate balance of mechanical properties and corrosion resistance, which allowed the conduit to meet the functional requirements.  
         [0095]     Since an improvement of certain properties in steel implies a detriment to others, it was necessary to design a material which at the same time allowed for compliance with high stress resistance, good toughness, high CTOD values and high resistance to corrosion in the metal base and high resistance to the advancement of cracking in the zone affected by heat (HAZ).  
         [0096]     Preferably, the heavy gauge seamless steel tube containing the detailed chemical composition should have the following balance of characteristic values: 
        Yielding Strength (YS) at room temperature≧65 Ksi     Yielding Strength (YS) at 130° C.≧65 Ksi     Ultimate Tensile Strength (UTS) at room temperature≧77 Ksi     Ultimate Tensile Strength (UTS) at 130° C.≧77 Ksi     Elongation of 2″≧20% minimum     Relation YS/UTS≦0.89 maximum     Energy absorbed measured at a temperature of −10° C.≧100 Joules minimum     Shear Area (−10° C.)=100%     Hardness≦240 HV10 maximum     CTOD in the metal base (tested at a temperature of up to −40° C.)≧0.8 mm minimum     CTOD in the heat affected zone (HAZ) (tested at a temperature of 0° C.)≧0.50 mm     Corrosion test HIC, according to NACE TM0284, with solution A: CTR 1.5% Max.; CLR 5.0% Max.        
 
         [0109]     Another aspect of the present invention is that of disclosing the heat treatment suitable for use on a heavy gauge tube with the chemical composition indicated above, in order to obtain the mechanical properties and resistance to corrosion which are required.  
         [0110]     The manufacturing process and specifically the parameters of the heat treatment together with the chemical composition described, have been developed by the inventor in order to obtain a suitable relationship of mechanical properties and corrosion resistance, at the same time obtaining high mechanical resistance of the material at 130° C.  
         [0111]     The following steps constitute the process for manufacturing the product:  
         [0112]     First an alloy with the indicated chemical composition is manufactured. This steel, as has already been mentioned, should contain a percentage by weight of the following elements in the amounts described: C 0.06 to 0.13; Mn 1.00 to 1.30; Si 0.35 Max.; P 0.015 Max.; S 0.003 Max.; Mo 0.10 to 0.20; Cr 0.10 to 0.30; V 0.050 to 0.10; Nb 0.020 to 0.035; Ni 0.30 to 0.45; Al 0.015 to 0.040; Ti 0.020 Max.; Cu 0.2 Max. and N 0.010 Max.  
         [0113]     Additionally, the amount of these elements should be such that they meet the following relationship: 
 
0.5&lt;(Mo+Cr+Ni)&lt;1; 
 
(Mo+Cr+V)/5+(Ni+Cu)/15≦0.14. 
 
         [0114]     This steel is shaped into solid bars obtained through curved or vertical continuous casting. Next the perforation of the bar and its posterior lamination takes place ending with the product in its final dimensions.  
         [0115]     In order to obtain good eccentricity, satisfactory quality in the surface of the outside wall of the tube and good dimensional tolerances, the preferred lamination process should be by still mandrel.  
         [0116]     Once the tube is conformed, it is subjected to heat treatment. 1 5 During this treatment the tube is first heated in an authentic furnace to a temperature above Ac3. The inventor has found that for the chemical composition described above, an authentic temperature of between 900 and 930° C. is necessary. This range has been developed to be sufficiently high as to obtain the correct dissolution of carbides in the matrix and at the same time not so high as to inhibit the excessive growth of the grain, which would later be detrimental to the transition temperature of the tube.  
         [0117]     On the other hand, high authentic temperatures above 930° C. could cause the partial dissolution of the precipitates of Nb (C, N) effective in the inhibition of the excessive growth of the size of the grain and detrimental to the transition temperature of the tube.  
         [0118]     Once the tube exits the authentic furnace, it is immediately subjected to exterior-interior tempering in a tub where the tempering agent is water. The tempering should-take place in a tub which allows for the rotation of the tube while it is immersed in water, in order to obtain a homogeneous structure throughout the body of the tube preferentially. At the same time, an automatic alignment of the tube with respect to the injection nozzle of water, also allows for better compliance with the planned objectives.  
         [0119]     The next step is the tempering treatment of the tube, a process which assures the end microstructure. Said microstructure will give the product its mechanical and corrosion characteristics.  
         [0120]     It has been found that this heat treatment together with the chemical composition revealed above provide for a matrix of refined bainite with a low C content with small areas, if they are still present, of well dispersed MA constituents, this being advantageous for obtaining the properties that steel for conduit requires. The inventor has found that, to the contrary, the presence of MA constituents in large numbers and of precipitates in the matrix and the boundaries of the grain, is detrimental to the transition temperature.  
         [0121]     A high tempering temperature is effective in increasing the toughness of the material since it releases a significant amount of residual forces and places some constituents in the solution.  
         [0122]     Therefore, in order to obtain the yielding strength required for this material after the tempering, it is necessary to maintain the fraction de polygonal ferrite low, preferably below 30% and to mainly promote the presence of inferior bainite.  
         [0123]     In compliance with the above and in order to reach the necessary balance in the properties of the steel, the tempering temperature should be between 630° C. and 690° C.  
         [0124]     It is known that, depending on the chemical composition that the steel possesses, the parameters for the thermal treatment and fundamentally the authentic and tempering temperatures should be determined. Consequently, the inventor found a relationship which makes it possible to determine the optimal tempering temperature, depending on the chemical composition of the steel. This temperature is established according to the following relationship: 
 
T temp  (° C.)=[−273+1000/(1.17−0.2 C−0.3 Mo−0.4 V)]±5 
 
         [0125]     Following is a description of the best method for carrying out the invention.  
         [0126]     The metallic load is prepared according to the concepts described and is cast in an electric arc furnace. During the fusion stage of the load at up to 1550° C. dephosphorization of the steel takes place, next it is descaled and new scale is formed in order to somewhat reduce the sulfur content. Finally it is decaburized to the desired levels and the liquid steel is emptied into the crevet.  
         [0127]     During the casting stage, aluminum is added in order to de-oxidize the steel and also an estimated amount of ferro-alloys are added until it reaches 80% of the end composition. Next de-sulfurization takes place; the casting is adjusted in composition as well as temperature; and the steel is sent to the vacuum degassing station where reduction of gases (H, N, O and S) takes place; and finally the treatment ends with the addition of CaSi to make inclusions float.  
         [0128]     Once the casting material is prepared in composition and temperature, it is sent to the continuous casting machine or the ingot casting where the transformation from liquid steel to solid bars of the desired diameter takes place. The product obtained on completion of this process is ingots, bars or blossoms having the chemical composition described above.  
         [0129]     The next step is the reheating of the steel blossoms to the temperature necessary for perforation and later lamination. The master tube thus obtained is then adjusted to the final desired dimensions.  
         [0130]     Next the steel tube is subjected to a hardening and tempering heat treatment in accordance with the parameters described in detail above.  
       EXAMPLES  
       [0131]     Following are examples of the application of the present invention in table form.  
         [0132]     Table 3 presents the different chemical compositions on which the tests used to consolidate this invention were based. Table 4 establishes the effect of this composition, with the heat treatments indicated, on the mechanical and anti-corrosion properties of the product. For example, the conduit identified with the number 1 has the chemical composition described in Table 3, that is: C, 0.09; Mn, 1.16; Si, 0.28; P. 0.01; S, 0.0012; Mo, 0.133; Cr, 0.20; V, 0.061; Nb, 0.025; Ni, 0.35; Al, 0.021; Ti, 0.013; N, 0.0051: Mo +Cr +Ni 0.68 and (Mo+Cr+V)/5+(Ni+Cu)/15=0.10.  
         [0133]     At a given moment, this same material is subjected to a heat treatment as indicated in columns “T.Aust.” Y “T. Temp” in Table 4, that is, an authentic Temperature: T. Aust=900° C. and a Tempering Temperature: T. Temp.=650° C.  
         [0134]     This same tube possesses the properties indicated in the following columns for the same steel number as in Table 4, that is, a thickness of 35 mm, a yielding strength (YS) of 75 Ksi, an ultimate tensile strength (UTS) of 89 Ksi, a relation between the yielding strength and the ultimate tensile strength (YS/UTS) of 0.84, a yielding strength measured at 130° C. of 69 Ksi, an ultimate tensile strength measured at 130° C. of 82 Ksi, a relationship between the yielding strength and the ultimate tensile strength measured at 130° C. of 0.84, a resistance to cracking measured by the CTOD test at −10° C. of 1.37 mm, a measurement of absorbed energy measured by the Charpy test at −10° C. of 440 Joules, a ductile/brittle area of 100%, a hardness of 215 HV10 and corrosion resistance measured by the HIC test in accordance with the NACE TM0284, with solution A of Norm NACE TM0177 1.5% being the maximum for CTR and 5.0% being the maximum for CLR.  
                                                                             TABLE 1                           Chemical composition of the steels shown in  FIG. 1              Steel   C   Si   Mn   P   S   Al   N   Nb   V   Ti   Cr   Ni   Cu   Mo               Base   0.089   0.230   1.29   0.007   0.0014   0.022   0.0030   0.028   0.050   0.0012   0.070   0.010   0.12   0.002       A   0.083   0.230   1.28   0.007   0.0013   0.025   0.0031   0.027   0.050   0.0012   0.070   0.380   0.12   0.150       B   0.061   0.230   1.28   0.007   0.0011   0.025   0.0032   0.027   0.050   0.0013   0.070   0.380   0.12   0.150       C   0.092   0.230   1.29   0.007   0.0015   0.025   0.0029   0.027   0.002   0.0013   0.067   0.384   0.12   0.150       D   0.089   0.229   1.27   0.007   0.0011   0.026   0.0028   0.027   0.002   0.0020   0.223   0.379   0.12   0.153       E   0.091   0.225   1.27   0.007   0.0012   0.023   0.0035   0.027   0.050   0.0013   0.220   0.380   0.11   0.150       F   0.130   0.230   1.28   0.007   0.0014   0.025   0.0031   0.027   0.050   0.0013   0.067   0.383   0.11   0.153                  
 
         [0135]    
       
         
               
             
               
               
               
               
               
               
               
               
               
               
               
               
               
               
               
             
           
               
                 TABLE 2 
               
             
             
               
                   
               
               
                   
               
               
                 Chemical composition of steels shown in  FIG. 2 . 
               
             
          
           
               
                 Steel 
                 C 
                 Si 
                 Mn 
                 P 
                 S 
                 Al 
                 N 
                 Nb 
                 V 
                 Ti 
                 Cr 
                 Ni 
                 Cu 
                 Mo 
               
               
                   
               
               
                 A 
                 0.09 
                 0.23 
                 1.3 
                 0.01 
                 0.001 
                 0.023 
                 0.003 
                 0.03 
                 0.05 
                 0.001 
                 0.068 
                 0.01 
                 0.11 
                 0.15 
               
               
                 B 
                 0.08 
                 0.23 
                 1.3 
                 0.01 
                 0.001 
                 0.025 
                 0.003 
                 0.03 
                 0.05 
                 0.001 
                 0.070 
                 0.38 
                 0.12 
                 0.15 
               
               
                 C 
                 0.09 
                 0.23 
                 1.3 
                 0.01 
                 0.001 
                 0.023 
                 0.004 
                 0.03 
                 0.05 
                 0.001 
                 0.220 
                 0.38 
                 0.11 
                 0.15 
               
               
                 D 
                 0.09 
                 0.23 
                 1.3 
                 0.01 
                 0.001 
                 0.026 
                 0.003 
                 0.03 
                 0.05 
                 0.002 
                 0.223 
                 0.38 
                 0.12 
                 0.15 
               
               
                 E 
                 0.09 
                 0.22 
                 1.3 
                 0.01 
                 0.001 
                 0.024 
                 0.005 
                 0.03 
                 0.05 
                 0.015 
                 0.065 
                 0.01 
                 0.11 
                 0.15 
               
               
                 F 
                 0.09 
                 0.22 
                 1.3 
                 0.01 
                 0.001 
                 0.022 
                 0.005 
                 0.03 
                 0.05 
                 0.014 
                 0.065 
                 0.38 
                 0.11 
                 0.15 
               
               
                 G 
                 0.09 
                 0.22 
                 1.3 
                 0.01 
                 0.001 
                 0.022 
                 0.005 
                 0.03 
                 0.05 
                 0.015 
                 0.220 
                 0.37 
                 0.12 
                 0.15 
               
               
                   
               
             
          
         
       
     
         [0136]    
       
         
               
             
               
               
               
               
               
               
               
               
               
               
               
               
               
               
               
               
             
               
               
               
               
               
               
               
               
               
               
               
               
               
               
               
               
             
           
               
                 TABLE 3 
               
             
             
               
                   
               
               
                   
               
               
                 Examples of chemical composition of the present invention 
               
             
          
           
               
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
                 Mo + 
                 (Mo + Cr + 
               
               
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
                 Cr + 
                 V)/5 + (Ni + 
               
               
                 Steel 
                 C 
                 Mn 
                 Si 
                 P 
                 S 
                 Mo 
                 Cr 
                 V 
                 Nb 
                 Ni 
                 Al 
                 Ti 
                 N 
                 Ni 
                 Cu)/15 
               
               
                   
               
             
          
           
               
                 1 
                 0.09 
                 1.16 
                 0.28 
                 0.01 
                 0.001 
                 0.13 
                 0.20 
                 0.061 
                 0.025 
                 0.35 
                 0.021 
                 0.0130 
                 0.0051 
                 0.68 
                 0.10 
               
               
                 2 
                 0.11 
                 1.12 
                 0.30 
                 0.011 
                 0.003 
                 0.14 
                 0.14 
                 0.054 
                 0.023 
                 0.41 
                 0.025 
                 0.0030 
                 0.0056 
                 0.69 
                 0.09 
               
               
                 3 
                 0.10 
                 1.13 
                 0.30 
                 0.010 
                 0.002 
                 0.14 
                 0.14 
                 0.056 
                 0.024 
                 0.42 
                 0.026 
                 0.0030 
                 0.0043 
                 0.70 
                 0.10 
               
               
                 4 
                 0.11 
                 1.13 
                 0.29 
                 0.013 
                 0.002 
                 0.14 
                 0.11 
                 0.063 
                 0.030 
                 0.42 
                 0.026 
                 0.0020 
                 0.0060 
                 0.67 
                 0.09 
               
               
                 5 
                 0.10 
                 1.12 
                 0.29 
                 0.012 
                 0.003 
                 0.14 
                 0.12 
                 0.066 
                 0.032 
                 0.43 
                 0.026 
                 0.0020 
                 0.0060 
                 0.69 
                 0.09 
               
               
                 6 
                 0.11 
                 1.11 
                 0.30 
                 0.011 
                 0.002 
                 0.14 
                 0.14 
                 0.055 
                 0.023 
                 0.41 
                 0.026 
                 0.0030 
                 0.0058 
                 0.69 
                 0.09 
               
               
                 7 
                 0.10 
                 1.14 
                 0.29 
                 0.012 
                 0.003 
                 0.14 
                 0.11 
                 0.063 
                 0.030 
                 0.42 
                 0.025 
                 0.0020 
                 0.0057 
                 0.67 
                 0.09 
               
               
                 8 
                 0.09 
                 1.13 
                 0.30 
                 0.010 
                 0.002 
                 0.14 
                 0.13 
                 0.056 
                 0.024 
                 0.42 
                 0.026 
                 0.0030 
                 0.0053 
                 0.69 
                 0.09 
               
               
                 9 
                 0.11 
                 1.21 
                 0.29 
                 0.013 
                 0.003 
                 0.15 
                 0.19 
                 0.054 
                 0.023 
                 0.39 
                 0.027 
                 0.0030 
                 0.0058 
                 0.73 
                 0.10 
               
               
                 10 
                 0.11 
                 1.21 
                 0.29 
                 0.014 
                 0.002 
                 0.14 
                 0.18 
                 0.054 
                 0.028 
                 0.39 
                 0.026 
                 0.0030 
                 0.0053 
                 0.71 
                 0.10 
               
               
                 11 
                 0.12 
                 1.21 
                 0.28 
                 0.013 
                 0.002 
                 0.14 
                 0.18 
                 0.051 
                 0.024 
                 0.38 
                 0.023 
                 0.0020 
                 0.0065 
                 0.70 
                 0.10 
               
               
                 12 
                 0.12 
                 1.20 
                 0.28 
                 0.013 
                 0.003 
                 0.13 
                 0.19 
                 0.052 
                 0.022 
                 0.38 
                 0.029 
                 0.0020 
                 0.0067 
                 0.70 
                 0.10 
               
               
                   
               
             
          
         
       
     
         [0137]    
       
         
               
             
               
               
               
               
               
               
               
               
             
               
               
               
               
               
               
               
               
               
               
               
               
               
               
               
             
               
               
               
               
               
               
               
               
               
               
               
               
               
               
               
               
             
               
               
               
               
               
               
               
               
               
               
               
               
               
               
               
               
             
           
               
                 TABLE 4 
               
             
             
               
                   
               
               
                   
               
               
                 Examples of the balance of properties of the present invention 
               
             
          
           
               
                   
                   
                   
                   
                   
                   
                 Energy 
                   
               
               
                   
                   
                   
                 Room 
                   
                   
                 absorbed 
               
               
                   
                 Rev. 
                   
                 Temperature 
                 130° C. 
                 CTOD 
                 at −10° C. 
               
             
          
           
               
                   
                 Aust. 
                 T. 
                   
                   
                   
                 YS/ 
                   
                   
                 YS/ 
                 at 
                 in base 
                 Shear 
                   
                   
               
               
                   
                 T. 
                 (*) 
                 Thickness 
                 YS 
                 UTS 
                 UTS 
                 YS 
                 UTS 
                 UTS 
                 −10° C. 
                 metel 
                 Area 
                 Hardness 
                 HIC Test 
               
             
          
           
               
                 Steel 
                 ° C. 
                 ° C. 
                 (mm) 
                 Ksi 
                 Ksi 
                 — 
                 Ksi 
                 Ksi 
                 — 
                 (mm) 
                 (Joules) 
                 % 
                 HV10 
                 CTR 
                 CLR 
               
               
                   
               
             
          
           
               
                 1 
                 900 
                 646 
                 35 
                 75 
                 89 
                 0.84 
                 69 
                 82 
                 0.84 
                 1.37 
                 440 
                 100 
                 215 
                 0 
                 0 
               
               
                 2 
                 900 
                 649 
                 30 
                 81 
                 91 
                 0.89 
                 70 
                 83 
                 0.84 
                 1.39 
                 410 
                 100 
                 202 
                 0 
                 0 
               
               
                 3 
                 900 
                 648 
                 30 
                 81 
                 91 
                 0.89 
                 69 
                 82 
                 0.84 
                 1.35 
                 405 
                 100 
                 214 
                 0 
                 0 
               
               
                 4 
                 900 
                 652 
                 35 
                 77 
                 89 
                 0.86 
                 69 
                 82 
                 0.84 
                 1.38 
                 390 
                 100 
                 201 
                 0 
                 0 
               
               
                 5 
                 900 
                 652 
                 35 
                 82 
                 92 
                 0.89 
                 76 
                 89 
                 0.85 
                 1.38 
                 380 
                 100 
                 208 
                 0 
                 0 
               
               
                 6 
                 900 
                 650 
                 38 
                 78 
                 92 
                 0.85 
                 72 
                 82 
                 0.88 
                 1.36 
                 400 
                 100 
                 218 
                 0 
                 0 
               
               
                 7 
                 900 
                 651 
                 38 
                 80 
                 90 
                 0.89 
                 71 
                 83 
                 0.85 
                 1.39 
                 410 
                 100 
                 217 
                 0 
                 0 
               
               
                 8 
                 900 
                 646 
                 40 
                 80 
                 90 
                 0.88 
                 77 
                 88 
                 0.87 
                 1.39 
                 407 
                 100 
                 203 
                 0 
                 0 
               
               
                 9 
                 900 
                 652 
                 40 
                 79 
                 89 
                 0.88 
                 74 
                 83 
                 0.89 
                 1.37 
                 425 
                 100 
                 202 
                 0 
                 0 
               
               
                 10 
                 900 
                 649 
                 40 
                 76 
                 87 
                 0.87 
                 74 
                 85 
                 0.87 
                 1.38 
                 419 
                 100 
                 202 
                 0 
                 0 
               
               
                 11 
                 900 
                 650 
                 40 
                 81 
                 91 
                 0.89 
                 69 
                 81 
                 0.85 
                 1.34 
                 423 
                 100 
                 203 
                 0 
                 0 
               
               
                 12 
                 900 
                 648 
                 40 
                 80 
                 91 
                 0.88 
                 70 
                 83 
                 0.84 
                 1.36 
                 393 
                 100 
                 214 
                 0 
                 0 
               
               
                   
               
               
                   (*) Defined according to the formula: T temp  (° C.) = [−273 + 1000/(1.17 − 0.2 C − 0.3 Mo − 0.4 V)] +/− 5    
               
             
          
         
       
     
         [0138]     The invention has been sufficiently described so that anyone with knowledge in the field can reproduce and obtain the results that we mention in the present invention. However, any person skilled in the art of the present invention is able to carry out modifications not described in the present application, but as for the application of these modifications in a determined material or manufacturing process of said, the material claimed in the following Claims is required, said material and said processes are deemed to fall within the broad scope and ambit of the invention as is herein set forth.