Abstract:
The present invention relates to a stainless steel alloy, more specifically a duplex stainless steel alloy with a ferritic-austenitic matrix and high corrosion resistance in combination with good structure stability, specifically a duplex stainless steel with a ferrite content of 40-65% and a well balanced analysis and with a combination of high corrosion resistance and good mechanical properties, such as high ultimate strength and good ductility which is especially suitable for use in applications in oil and gas explorations such as wire, especially as reinforced wire in wireline applications. These purposes are achieved according to the invention by a duplex stainless steel alloy that contains (in wt %): C 0-0.03%; Si up to max 0.5%; Mn 0-3.0%; Cr 24.0-30.0%; Ni 4.9-10.0%; Mo 3.0-5.0%; N 0.28-0.5%; S up to max. 0.010%; Co 0-3.5%; W 0-3.0%; Cu 0-2%; Ru 0-0.3%; Al 0-0.03; Ca 0-0.010%; the balance being Fe and unavoidable impurities.

Description:
This application claims priority from International Application No. PCT/SE2004/000224, filed on Feb. 19, 2004; and Swedish Application No. 0300573-3, filed on Mar. 2, 2003, the subject matter of which is incorporated herein by reference. 
     The present invention relates to a stainless steel alloy, more specifically a duplex stainless steel alloy with a ferritic-austenitic matrix and with high corrosion resistance towards chloride containing environments in combination with use at high temperatures in combination with good structural stability and hot workability, with a combination of high corrosion resistance and good mechanical properties, such as high ultimate strength, good ductility and strength, that is especially suitable for use in wire applications in oil and gas exploration such as wire, rope and lines for slicklines, wire-lines and well-logging cables. 
     BACKGROUND AND PRIOR ART 
     In connection with more limited access to natural resources such as oil and gas when these resources become smaller and being of less quality efforts are being made to fund New resources or such resources that until now have not been exploited due to excessively high costs for extraction and subsequent processes such as transport and further fabrication of the raw material, maintenance of the resource and measuring operations. 
     Exploration of oil and gas from the sea bottom in deep se is an established technology. Transport of equipment and goods to and from the source and transmission of signal and energy is managed from the water surface. In very deep waters there might be transport distance that amounts up to 10,000 meters for such applications. Wire, rope or cables of stainless steel is used to a greater extent in applications for off-shore exploration of oil and gas. 
     So-called wirelines are today usually made in such manner that they contain several isolated electrical leads or cables such as fiber-optical cables which in their entirety are covered by one or several layers of helically extending steel wires. The selection of the steel grade is determined primarily by the demands for strength, ultimate strength and ductility in combination with suitable corrosion properties especially under those conditions valid for oil and gas explorations. 
     The usage is limited largely due to resistance to fatigue due to repeated use in oil and gas industry, especially when used as slick-line, wire-line or wellbore logging cable and in applications of repeated coiling and transportation over a so-called pulley-wheel. The possibility of usage of the material is limited in thus sector of the ultimate strength of the wire material being used. The degree of cold deformation is usually optimized with regard to the ductility. Specially the austenitic materials do however not satisfy the practical demands. 
     The latest years, when environments for usage of corrosion resistant metallic materials have become more demanding has caused increased requirements upon the corrosion properties of the material as well as their mechanical properties. Duplex steel alloys, established as alternative for the hitherto used steel alloys such as highly alloyed austenitic steels, nickel base alloys or other highly alloyed steels are not excluded from this development. There are high demands for corrosion resistance when the string, rope. or the line is exposed to high mechanical properties and the very corrosive environment when the surrounding isolation of a plastic material such as polyurethane is damaged and made unusable very quickly during repeated coiling. More recent developments are therefore aimed at using the reinforced wire as the outermost layer. 
     There is furthermore a desire of significantly higher strength than achieved with today&#39;s technology for a certain degree of cold deformation. 
     The disadvantage with the duplex alloys used today is the existence of hard and brittle intermetallic precipitations in the steel, such as sigma phase, especially after heat treatment during the manufacture or during subsequent working. This leads to harder material with worse workability and finally worse corrosion resistance and possibly crack propagations. 
     In order to furthermore improve the corrosion resistance of duplex stainless steels it is demanded an increase of the PRE number in both the ferrite as well as in the austenite phase without simultaneously impairing the structure stability or workability of the material. If the analysis in the two phases is not equal with regard to the active alloy constituents one phase will become susceptible for nodular or crevice corrosion. Hence, the more corrosion sensitive phase will govern the resistance of the alloy whereas the structure stability is governed by the most alloyed phase. 
     SUMMARY 
     It is an object of the invention to provide a duplex stainless steel alloy with a combination of high corrosion resistance and good mechanical properties such as high impact strength, good ductility and strength. 
     It is a further object of the invention to provide a duplex stainless steel alloy that is specifically suitable for use in wire applications in oil and gas explorations such as wires, ropes and lines for so-called slicklines, wirelines and well-logging cables. It is therefore a purpose of the invention to provide a duplex stainless steel alloy with ferritic-austenitic matrix and high corrosion resistance in chloride containing environments in combination with use under high temperatures in combination with good structure stability and hot workability. 
     The material according to the invention, with its high amounts of alloy elements, appears with good workability and will therefore be very suitable for being used for the manufacture of wires. 
     The alloy of the present invention can advantageously be used as an isolated wire in slickline applications and as so-called braided wire where several wires of same or different diameters are clogged together. 
     These objects are fulfilled with an alloy according to the invention which contains (in weight-%) 
    
    
     
       SHORT DESCRIPTION OF THE DRAWINGS 
         FIG. 1  shows CPT values from tests of heats in the modified ASTM G48C test in “green death”-solution compared with the duplex steels SAF 2507, SAF 2906. 
         FIG. 2  shows CPT-values obtained by means of the modified ASTM G48C test in “green death”-solution for then test heats compared with duplex steel SAF 2507 and SAF 2906. 
         FIG. 3  shows the average value for weight loss in mm/year in 2% HCl at a temperature of 75 degrees C. 
         FIG. 4  shows data with regard to impact strength and yield point for the ally type SAF 2205. 
         FIG. 5  shows data related to impact strength and yield point for the alloy according to the invention. 
     
    
    
     DETAILED DESCRIPTION 
     A systematic development work has surprisingly shown that an alloy with an amount of alloying elements according to the invention satisfies these demands. 
     The importance of the alloy elements for the invention 
     Carbon has a limited solubility in both austenite and ferrite. The limited solubility causes a risk for precipitation of chromium carbides and the content thereof should therefore not exceed 0.03 wt %, preferably not exceed 0.02 wt %. 
     Silicon is used as deoxidation agent in the steel manufacture and increases flowability during manufacture and welding. However, too high amounts of Si will cause precipitation of undesirable intermetallic phase and the content thereof should therefore be limited to max 0.5 wt %, preferably max 0.3 wt %. 
     Manganese is added to increase N-solubility in the material. It has been found, however, that Mn has only a limited impact on the N-solubility in the actual type of alloy. There are instead other elements that gives higher impact on the solubility. Further, Mn in combination with high sulphur contents can give rise to manganese sulphides which act as initiation points for point corrosion. The Mn-content should therefore be limited to a value in the range 0-3.0 wt %, preferably 0.5-1.2 wt %. 
     Chromium is a very active element for increasing the resistance to most types of corrosion. A high Cr-content further leads to a very good solubility of nitrogen in the material. It is therefore desirable to keep the Cr-content as high as possible to improve the corrosion resistance. To achieve very good values of corrosion resistance the Cr-content should amount to at least 24.0 wt %, preferably 26.5-29.0 wt %. High Cr-amounts do however increase the tendency for intermetallic precipitations and the Cr-content should therefore be limited upwards to max 30.0 wt %. 
     Nickel is used as an austenite stabilizer element and should be added in suitable amounts such that desired ferrite content is achieved. In order to achieve the desired relation between the austenitic and the ferritic phases with 40-65 volume % ferrite there is required an added amount in the range 4.9-10.0 wt % nickel, preferably 4.9-9.0 wt %, and specifically 6.0-9.0 wt %. 
     Molybdenum is an active element which improves corrosion resistance in chloride environments and preferably in reducing acids. If the Mo-content is too high combined with too high Cr-content this could increase the amount of intermetallic precipitations. The Mo-content should therefore be in the range of 3.0-5.0 wt %, preferably 3.6-4.9 wt %, more specifically 4.4-4.9 wt %. 
     Nitrogen is a very active element that increases corrosion resistance, structure stability and the strength of the material. A high amount of nitrogen furthermore increases the recreation of austenite after welding which gives a good weld joint with good properties. To achieve a good effect of nitrogen its content should be at least 0.28 wt %. If the N-amount is high this could give rise to increased porosity due to exceeded solubility of N in the melt. For these reasons the N-content should be limited to max 0.5 wt %, and preferably there should be added an amount of 0.35-0.45 wt % N. 
     If the amounts of Cr and N are too high this will result in precipitation of Cr 2 N which should be avoided since this causes impairment of the properties of the material, especially during heat treatment, for instance at welding. 
     Boron is added to increase hot workability of the material. If too high boron content is present weldability and corrosion resistance could be negatively affected. The boron content should therefore exceed 0 and be present in amounts up to 0.0030 wt %. 
     Sulphur has a negative impact on corrosion resistance by formation of sulphides which are easily soluble. This causes impaired hot workability and the sulphur content should therefore be limited to max 0.010 wt %. 
     Cobalt is added primarily to improve the structure stability and the corrosion resistance. Co is an austenite stabilizer. In order to achieve its effect at least 0.5 wt %, preferably at least 1.0 wt % should be added to the alloy. Since cobalt is a relatively expensive element the added cobalt amount should be limited to max 3.5 wt %. 
     Tungsten increases the resistance against point and crevice corrosion. Adding too much tungsten combined with high Cr- and Mo-amounts will increase the risk for intermetallic precipitations. The tungsten content in the present invention should lie in the range 0-3.0 wt %, preferably between 0-1.8 wt %. 
     Copper is added to improve the general corrosion resistance in acid environments such as sulphuric acid. Cu also affects the structure stability. High amounts of Cu leads, however, to an excessive firm solubility. The Cu-content should therefore be limited to max 2 wt %, preferably between 0.1 and 1.5 wt %. 
     Ruthenium is added to the alloy in order to increase the corrosion resistance. However, since ruthenium is a very expensive element its content should be limited to max 0.3 wt %, preferably larger than=and up to 0.1 wt %. 
     Aluminum and calcium should be used as desoxidation elements during the steel production. The amount of Al should be limited to max 0.03 wt % to limit the nitride formation. Ca has a positive effect on hot ductility but the Ca-content ought to be limited to 0.01 wt % to avoid undesired amount of slag. 
     The ferrite content is important to achieve good mechanical properties and corrosion properties and good weldability. From corrosion standpoint and weldability standpoint it is desirable to have a ferrite content of 40-65% to achieve good properties. High ferrite content furthermore results in a risk of unpaired low temperature impact toughness and resistance towards hydrogen embrittlement. The ferrite content is therefore 40-65 vol %, preferably 42-65 vol %, and most preferably 45-55 vol %. 
     DESCRIPTION OF PREFERRED EMBODIMENTS 
     In the examples given below there is disclosed the analysis for a number of test charges which will illustrate the impact that various alloy elements will have upon the properties. Charge 605182 represents a reference analysis and is thus not included in the range within the scope of the invention. Also, all other charges shall not be considered as limiting the invention but rather to define examples of charges that illustrate the invention pursuant to the patent claims. The PRE-values as given are always referring to values calculated according to the PREW-formula even if not expressly defined. 
     Example 1 
     The test charges according to this example are made by laboratory casting of an ingot of 170 kg that was hot forged to a round bar. This was then hot extruded to bar shape (round bar and plate-shaped bar) where the test material was sampled out from the round bar. The plate-shaped bar was subject of heat treatment before cold rolling after which additional test material was sampled out. From a material-technical standpoint, this process is considered as representative for manufacture in a larger scale. Table 1 shows the analysis of the test charges. 
     
       
         
               
               
               
               
               
               
               
               
               
               
               
             
           
               
                 TABLE 1 
               
               
                   
               
               
                 Charge 
                 Mn 
                 Cr 
                 Ni 
                 Mo 
                 W 
                 Co 
                 V 
                 La 
                 Ti 
                 N 
               
               
                   
               
             
             
               
                 605193 
                 1.03 
                 27.90 
                 8.80 
                 4.00 
                 0.01 
                 0.02 
                 0.04 
                 0.01 
                 0.01 
                 0.36 
               
               
                 605195 
                 0.97 
                 27.90 
                 9.80 
                 4.00 
                 0.01 
                 0.97 
                 0.55 
                 0.01 
                 0.35 
                 0.48 
               
               
                 605197 
                 1.07 
                 28.40 
                 8.00 
                 4.00 
                 1.00 
                 1.01 
                 0.04 
                 0.01 
                 0.01 
                 0.44 
               
               
                 605178 
                 0.91 
                 27.94 
                 7.26 
                 4.01 
                 0.99 
                 0.10 
                 0.07 
                 0.01 
                 0.03 
                 0.44 
               
               
                 605183 
                 1.02 
                 28.71 
                 6.49 
                 4.03 
                 0.01 
                 1.00 
                 0.04 
                 0.01 
                 0.04 
                 0.28 
               
               
                 605184 
                 0.99 
                 28.09 
                 7.83 
                 4.01 
                 0.01 
                 0.03 
                 0.54 
                 0.01 
                 0.01 
                 0.44 
               
               
                 605187 
                 2.94 
                 27.74 
                 4.93 
                 3.98 
                 0.01 
                 0.98 
                 0.06 
                 0.01 
                 0.01 
                 0.44 
               
               
                 605153 
                 2.78 
                 27.85 
                 6.93 
                 4.03 
                 1.01 
                 0.02 
                 0.06 
                 0.02 
                 0.01 
                 0.34 
               
               
                 605182 
                 0.17 
                 23.48 
                 7.88 
                 5.75 
                 0.01 
                 0.05 
                 0.04 
                 0.01 
                 0.10 
                 0.26 
               
               
                   
               
             
          
         
       
     
     In order to investigate the structure stability specimen were taken out from every charge and heat treated at 900-1150 degrees C. with 50 degrees step and quenched in air and water respectively. At the lowest temperatures intermetallic phases were obtained. The lowest temperature where the amount of intermetallic phase was negligible was determined by means of studies in a light optical microscope. New specimen from respective charge were then heat treated at said temperature for five minutes after which the specimen was subject of cooling with a constant cooling speed of −140 degrees C. down to room temperature. 
     The point corrosion properties of all charges have been tested by ranking in the so-called “green-death”-solution which consists of 1% FeCl 3 , 1% CuCl 2 , 11% H 2 S0 4 , 1.2% HCl. This testing procedure corresponds to point corrosion testing according to ASTM G48C but is carried out in the more aggressive “green-death”-solution. Further, some charges have been tested according to ASTNIG48C (2 tests per charge). Also electrochemical testing in 3% NaCl (6 tests per charge) have been carried out. The results in the form of critical point corrosion temperature (CPT) from all tests appear from Table 2, like the PREW-value (Cr+3.3 (Mo+0.5W)+16N) for the total alloy analysis and for austenite and ferrite. The indexing alfa relates to ferrite and gamma relates to austenite. 
     
       
         
               
               
               
               
               
               
               
               
             
               
               
               
               
               
               
               
               
             
           
               
                 TABLE 2 
               
               
                   
               
               
                   
                   
                   
                   
                   
                 CPT ° C. 
                   
                   
               
               
                   
                   
                   
                   
                   
                 Modified 
                   
                 CPT ° C. 3% 
               
               
                   
                   
                   
                   
                   
                 ASTM G48C 
                 CPT ° C. ASTM 
                 NaCl (600 mv 
               
               
                 Charge 
                 PRE α 
                 PRE γ 
                 PRE γ/PRE α 
                 PRE 
                 Green Death 
                 G48C 6% FeCl 3   
                 SCE 
               
               
                   
               
             
             
               
                   
               
             
          
           
               
                 605193 
                 51.3 
                 49.0 
                 0.9552 
                 46.9 
                 93/90 
                   
                 64 
               
               
                 605195 
                 51.5 
                 48.9 
                 0.9495 
                 48.7 
                 93/90 
                   
                 95 
               
               
                 605197 
                 53.3 
                 53.7 
                 1.0075 
                 50.3 
                 93/90 
                 &gt;95 
                 &gt;95 
               
               
                 605178 
                 50.7 
                 52.5 
                 1.0355 
                 49.8 
                 75/80 
                   
                 94 
               
               
                 605183 
                 48.9 
                 48.9 
                 1.0000 
                 46.5 
                 85/85 
                 90 
                 93 
               
               
                 605184 
                 48.9 
                 51.7 
                 1.0573 
                 48.3 
                 83/80 
                   
                 72 
               
               
                 605187 
                 48.0 
                 54.4 
                 1.1333 
                 48.0 
                 73/75 
                   
                 77 
               
               
                 605153 
                 49.6 
                 51.9 
                 1.0464 
                 48.3 
                 83/85 
                 85 
                 90 
               
               
                 605182 
                 54.4 
                 46.2 
                 0.8493 
                 46.6 
                 75/70 
                 85 
                 62 
               
               
                 SAF2507 
                 39.4 
                 42.4 
                 1.0761 
                 41.1 
                 73/70 
                 80 
                 95 
               
               
                 SAF2906 
                 39.6 
                 46.4 
                 1.1717 
                 41.0 
                 60/50 
                 75 
                 75 
               
               
                   
               
             
          
         
       
     
     The strength at room temperature (RT), 100° C. and 200° C. and the impact strength at room temperature (RT) has been determined for all charges and is shown as average value out of three tests. 
     Tensile test pieces (DR-5C50) were made from extruded bars, diameter 20 mm, which were heat treated at room temperature according to Table 2 for 20 minutes followed by cooling either in air or water (605195, 605197, 605184). The results of this investigation is presented in Table 3. The results from the tensile strength testing investigation show that the contents of chromium, nitrogen and tungsten strongly affect the tensile strength in the material. All charges except 605153 satisfy the requirement of a 25% increase when subjected to tensile testing in room temperature (RT). 
     
       
         
               
               
               
               
               
               
               
             
           
               
                 TABLE 3 
               
               
                   
               
               
                   
                   
                 R p0.2   
                 R p0.1   
                 R m   
                 A5 
                 Z 
               
               
                 Charge 
                 Temperatur 
                 (MPa) 
                 (MPa) 
                 (MPa) 
                 (%) 
                 (%) 
               
               
                   
               
             
             
               
                 605193 
                 RT 
                 652 
                 791 
                 916 
                 29.7 
                 38 
               
               
                   
                 100° C. 
                 513 
                 646 
                 818 
                 30.4 
                 36 
               
               
                   
                 200° C. 
                 511 
                 583 
                 756 
                 29.8 
                 36 
               
               
                 605195 
                 RT 
                 671 
                 773 
                 910 
                 38.0 
                 66 
               
               
                   
                 100° C. 
                 563 
                 637 
                 825 
                 39.3 
                 68 
               
               
                   
                 200° C. 
                 504 
                 563 
                 769 
                 38.1 
                 64 
               
               
                 605197 
                 RT 
                 701 
                 799 
                 939 
                 38.4 
                 66 
               
               
                   
                 100° C. 
                 564 
                 652 
                 844 
                 40.7 
                 69 
               
               
                   
                 200° C. 
                 502 
                 577 
                 802 
                 35.0 
                 65 
               
               
                 605178 
                 RT 
                 712 
                 828 
                 925 
                 27.0 
                 37 
               
               
                   
                 100° C. 
                 596 
                 677 
                 829 
                 31.9 
                 45 
               
               
                   
                 200° C. 
                 535 
                 608 
                 763 
                 27.1 
                 36 
               
               
                 605183 
                 RT 
                 677 
                 775 
                 882 
                 32.4 
                 67 
               
               
                   
                 100° C. 
                 560 
                 642 
                 788 
                 33.0 
                 59 
               
               
                   
                 200° C. 
                 499 
                 578 
                 737 
                 29.9 
                 52 
               
               
                 605184 
                 RT 
                 702 
                 793 
                 915 
                 32.5 
                 60 
               
               
                   
                 100° C. 
                 569 
                 657 
                 821 
                 34.5 
                 61 
               
               
                   
                 200° C. 
                 526 
                 581 
                 774 
                 31.6 
                 56 
               
               
                 605187 
                 RT 
                 679 
                 777 
                 893 
                 35.7 
                 61 
               
               
                   
                 100° C. 
                 513 
                 628 
                 799 
                 38.9 
                 64 
               
               
                   
                 200° C. 
                 505 
                 558 
                 743 
                 35.8 
                 58 
               
               
                 605153 
                 RT 
                 715 
                 845 
                 917 
                 20.7 
                 24 
               
               
                   
                 100° C. 
                 572 
                 692 
                 817 
                 29.3 
                 27 
               
               
                   
                 200° C. 
                 532 
                 611 
                 749 
                 23.7 
                 31 
               
               
                 605182 
                 RT 
                 627 
                 754 
                 903 
                 28.4 
                 43 
               
               
                   
                 100° C. 
                 493 
                 621 
                 802 
                 31.8 
                 42 
               
               
                   
               
             
          
         
       
     
     Example 2 
     In the following example the analysis is given for yet another number of test charges made for the purpose to find the optimal analysis. These charges are modified outgoing from the properties of those charges with good structure stability and high corrosion resistance from the results shown in Example 1. All the charges in table 4 are included by the analysis according to the present invention where charge 1-8 are part of a statistic test plan whereas charge e to n are further test alloys within the scope of the present invention. 
     A number of test charges were made by casting 270 kg ingots that were hot forged into cylindrical rods. These were subject of extrusion to bars out of which test pieces were taken. These were then subject of heating before fold rolling of plate shaped bar after which further test piece were taken out. Table 4 shows the analysis for these test charges. 
     
       
         
               
               
               
               
               
               
               
               
               
               
               
               
             
               
               
               
               
               
               
               
               
               
               
               
               
             
           
               
                 TABLE 4 
               
               
                   
               
               
                   
                 Charge 
                 Mn 
                 Cr 
                 Ni 
                 Mo 
                 W 
                 Co 
                 Cu 
                 Ru 
                 B 
                 N 
               
               
                   
               
             
             
               
                   
               
             
          
           
               
                 1 
                 605258 
                 1.1 
                 29.0 
                 6.5 
                 4.23 
                   
                 1.5 
                   
                   
                 0.0018 
                 0.46 
               
               
                 2 
                 605249 
                 1.0 
                 28.8 
                 7.0 
                 4.23 
                   
                 1.5 
                   
                   
                 0.0026 
                 0.38 
               
               
                 3 
                 605259 
                 1.1 
                 29.0 
                 6.8 
                 4.23 
                   
                 0.6 
                   
                   
                 0.0019 
                 0.45 
               
               
                 4 
                 605260 
                 1.1 
                 27.5 
                 5.9 
                 4.22 
                   
                 1.5 
                   
                   
                 0.0020 
                 0.44 
               
               
                 5 
                 605250 
                 1.1 
                 28.8 
                 7.6 
                 4.24 
                   
                 0.6 
                   
                   
                 0.0019 
                 0.40 
               
               
                 6 
                 605251 
                 1.0 
                 28.1 
                 6.5 
                 4.24 
                   
                 1.5 
                   
                   
                 0.0021 
                 0.38 
               
               
                 7 
                 605261 
                 1.0 
                 27.8 
                 6.1 
                 4.22 
                   
                 0.6 
                   
                   
                 0.0021 
                 0.43 
               
               
                 8 
                 605252 
                 1.1 
                 28.4 
                 6.9 
                 4.23 
                   
                 0.5 
                   
                   
                 0.0018 
                 0.37 
               
               
                 e 
                 605254 
                 1.1 
                 26.9 
                 6.5 
                 4.8 
                   
                 1.0 
                   
                   
                 0.0021 
                 0.38 
               
               
                 f 
                 605255 
                 1.0 
                 28.6 
                 6.5 
                 4.0 
                   
                 3.0 
                   
                   
                 0.0020 
                 0.31 
               
               
                 g 
                 605262 
                 2.7 
                 27.6 
                 6.9 
                 3.9 
                 1.0 
                 1.0 
                   
                   
                 0.0019 
                 0.36 
               
               
                 h 
                 605263 
                 1.0 
                 28.7 
                 6.6 
                 4.0 
                 1.0 
                 1.0 
                   
                   
                 0.0020 
                 0.40 
               
               
                 i 
                 605253 
                 1.0 
                 28.8 
                 7.0 
                 4.16 
                   
                 1.5 
                   
                   
                 0.0019 
                 0.37 
               
               
                 j 
                 605266 
                 1.1 
                 30.0 
                 7.1 
                 4.02 
                   
                   
                   
                   
                 0.0018 
                 0.38 
               
               
                 k 
                 605269 
                 1.0 
                 28.5 
                 7.0 
                 3.97 
                 1.0 
                 1.0 
                   
                   
                 0.0020 
                 0.45 
               
               
                 l 
                 605268 
                 1.1 
                 28.2 
                 6.6 
                 4.0 
                 1.0 
                 1.0 
                 1.0 
                   
                 0.0021 
                 0.43 
               
               
                 m 
                 605270 
                 1.0 
                 28.8 
                 7.0 
                 4.2 
                   
                 1.5 
                   
                 0.1 
                 0.0021 
                 0.41 
               
               
                 n 
                 605267 
                 1.1 
                 29.3 
                 6.5 
                 4.23 
                   
                   
                 1.5 
                   
                 0.0019 
                 0.38 
               
               
                   
               
             
          
         
       
     
     The distribution of the alloy elements in the ferrite and austenite phase was investigated by microsound analysis, the results of which appear from Table 5. 
     
       
         
               
               
               
               
               
               
               
               
               
               
             
               
               
               
               
               
               
               
               
               
               
             
           
               
                 TABLE 5 
               
               
                   
               
               
                 Charge 
                 Phase 
                 Cr 
                 Mn 
                 Ni 
                 Mo 
                 W 
                 Co 
                 Cu 
                 N 
               
               
                   
               
             
             
               
                   
               
             
          
           
               
                 605258 
                 Ferrite 
                 29.8 
                 1.3 
                 4.8 
                 5.0 
                   
                 1.4 
                   
                 0.11 
               
               
                   
                 Austenit 
                 28.3 
                 1.4 
                 7.3 
                 3.4 
                   
                 1.5 
                   
                 0.60 
               
               
                 605249 
                 Ferrit 
                 29.8 
                 1.1 
                 5.4 
                 5.1 
                   
                 1.3 
                   
                 0.10 
               
               
                   
                 Austenite 
                 27.3 
                 1.2 
                 7.9 
                 3.3 
                   
                 1.6 
                   
                 0.53 
               
               
                 605259 
                 Ferrite 
                 29.7 
                 1.3 
                 5.3 
                 5.3 
                   
                 0.5 
                   
                 0.10 
               
               
                   
                 Austenite 
                 28.1 
                 1.4 
                 7.8 
                 3.3 
                   
                 0.58 
                   
                 0.59 
               
               
                 605260 
                 Ferrite 
                 28.4 
                 1.3 
                 4.4 
                 5.0 
                   
                 1.4 
                   
                 0.08 
               
               
                   
                 Austenite 
                 26.5 
                 1.4 
                 6.3 
                 3.6 
                   
                 1.5 
                   
                 0.54 
               
               
                 605250 
                 Ferrite 
                 30.1 
                 1.3 
                 5.6 
                 5.1 
                   
                 0.46 
                   
                 0.07 
               
               
                   
                 Austenite 
                 27.3 
                 1.4 
                 8.8 
                 3.4 
                   
                 0.53 
                   
                 0.52 
               
               
                 605251 
                 Ferrite 
                 29.6 
                 1.2 
                 5.0 
                 5.2 
                   
                 1.3 
                   
                 0.08 
               
               
                   
                 Austenite 
                 26.9 
                 1.3 
                 7.6 
                 3.5 
                   
                 1.5 
                   
                 0.53 
               
               
                 605261 
                 Ferrite 
                 28.0 
                 1.2 
                 4.5 
                 4.9 
                   
                 0.45 
                   
                 0.07 
               
               
                   
                 Austenite 
                 26.5 
                 1.4 
                 6.9 
                 3.3 
                   
                 0.56 
                   
                 0.56 
               
               
                 605252 
                 Ferrite 
                 29.6 
                 1.3 
                 5.3 
                 5.2 
                   
                 0.42 
                   
                 0.09 
               
               
                   
                 Austenite 
                 27.1 
                 1.4 
                 8.2 
                 3.3 
                   
                 0.51 
                   
                 0.48 
               
               
                 605254 
                 Ferrite 
                 28.1 
                 1.3 
                 4.9 
                 5.8 
                   
                 0.89 
                   
                 0.08 
               
               
                   
                 Austenite 
                 26.0 
                 1.4 
                 7.6 
                 3.8 
                   
                 1.0 
                   
                 0.48 
               
               
                 605255 
                 Ferrite 
                 30.1 
                 1.3 
                 5.0 
                 4.7 
                   
                 2.7 
                   
                 0.08 
               
               
                   
                 Austenite 
                 27.0 
                 1.3 
                 7.7 
                 3.0 
                   
                 3.3 
                   
                 0.45 
               
               
                 605262 
                 Ferrite 
                 28.8 
                 3.0 
                 5.3 
                 4.8 
                 1.4 
                 0.9 
                   
                 0.08 
               
               
                   
                 Austenite 
                 26.3 
                 3.2 
                 8.1 
                 3.0 
                 0.85 
                 1.1 
                   
                 0.46 
               
               
                 605263 
                 Ferrite 
                 29.7 
                 1.3 
                 5.1 
                 5.1 
                 1.3 
                 0.91 
                   
                 0.07 
               
               
                   
                 Austenite 
                 27.8 
                 1.4 
                 7.7 
                 3.2 
                 0.79 
                 1.1 
                   
                 0.51 
               
               
                 605253 
                 Ferrite 
                 30.2 
                 1.3 
                 5.4 
                 5.0 
                   
                 1.3 
                   
                 0.09 
               
               
                   
                 Austenite 
                 27.5 
                 1.4 
                 8.4 
                 3.1 
                   
                 1.5 
                   
                 0.48 
               
               
                 605266 
                 Ferrite 
                 31.0 
                 1.4 
                 5.7 
                 4.8 
                   
                   
                   
                 0.09 
               
               
                   
                 Austenite 
                 29.0 
                 1.5 
                 8.4 
                 3.1 
                   
                   
                   
                 0.52 
               
               
                 605269 
                 Ferrite 
                 28.7 
                 1.3 
                 5.2 
                 5.1 
                 1.4 
                 0.9 
                   
                 0.11 
               
               
                   
                 Austenite 
                 26.6 
                 1.4 
                 7.8 
                 3.2 
                 0.87 
                 1.1 
                   
                 0.52 
               
               
                 605268 
                 Ferrite 
                 29.1 
                 1.3 
                 5.0 
                 4.7 
                 1.3 
                 0.91 
                 0.84 
                 0.12 
               
               
                   
                 Austenite 
                 26.7 
                 1.4 
                 7.5 
                 3.2 
                 0.97 
                 1.0 
                 1.2 
                 0.51 
               
               
                 605270 
                 Ferrite 
                 30.2 
                 1.2 
                 5.3 
                 5.0 
                   
                 1.3 
                   
                 0.11 
               
               
                   
                 Austenite 
                 27.7 
                 1.3 
                 8.0 
                 3.2 
                   
                 1.4 
                   
                 0.47 
               
               
                 605267 
                 Ferrite 
                 30.1 
                 1.3 
                 5.1 
                 4.9 
                   
                   
                 1.3 
                 0.08 
               
               
                   
                 Austenite 
                 27.8 
                 1.4 
                 7.6 
                 3.1 
                   
                   
                 1.8 
                 0.46 
               
               
                   
               
             
          
         
       
     
     The point corrosion properties of all the charges have been tested by the “green death” solution (1% FeCl 3 , 1% CuCl 2 , 11% H 2 SO 4 , 1.2% HCl) for ranking. 
     The test procedure is the same as for point corrosion testing according to ASTM G48C except for the used solution that is more aggressive than 6% FeCl 3 , the so-called “green death”-solution. Also general corrosion testing in 2% HCl (2 tests per charge) has been carried out for ranking before dew point testing. The results from all tests appear from Table 6,  FIG. 2  and  FIG. 3 . All the tested charges perform better than SAF 2507 in the green death solution. All the charges lie in the defined interval of 0.9-1.15, preferably 0.9-1.05 as regards the ratio PRE austenite/PRE ferrite at the same time as PRE for both austenite and ferrite exceeds 44 and for most charges also essentially exceeds 44. Some of the charges are even extending to the limit value totally PRE50. It is very interesting to observe that charge 605251 alloyed with 1.5% cobalt performs almost equally as good as charge 605250 alloyed with 0.6% cobalt in the “green death” solution in spite of the lower chromium content in charge 605251. This is of special surprise and interest since charge 605251 has a PRE-value of approximately 48 which is higher than for a commercial superduplex alloy at the same time as T-max sigma value under 1010° C. indicates good structure stability based on the values in Table 2 in example 1. 
     
       
         
               
               
               
               
               
               
               
             
           
               
                 TABLE 6 
               
               
                   
               
               
                   
                   
                   
                   
                   
                   
                 CPT ° C. 
               
               
                   
                   
                 PREW 
                   
                   
                 PREγ/ 
                 the Green 
               
               
                 Charge 
                 α content 
                 Total 
                 PRE α 
                 PRE γ 
                 PREα 
                 Death 
               
               
                   
               
             
             
               
                 605258 
                 48.2 
                 50.3 
                 48.1 
                 49.1 
                 1.021 
                 65/70 
               
               
                 605249 
                 59.2 
                 48.9 
                 48.3 
                 46.6 
                 0.967 
                 75/80 
               
               
                 605259 
                 49.2 
                 50.2 
                 48.8 
                 48.4 
                 0.991 
                 75/75 
               
               
                 605260 
                 53.4 
                 48.5 
                 46.1 
                 47.0 
                 1.019 
                 75/80 
               
               
                 605250 
                 53.6 
                 49.2 
                 48.1 
                 46.8 
                 0.974 
                 95/80 
               
               
                 605251 
                 54.2 
                 48.2 
                 48.1 
                 46.9 
                 0.976 
                 90/80 
               
               
                 605261 
                 50.8 
                 48.6 
                 45.2 
                 46.3 
                 1.024 
                 80/70 
               
               
                 605252 
                 56.6 
                 48.2 
                 48.2 
                 45.6 
                 0.946 
                 80/75 
               
               
                 605254 
                 53.2 
                 48.8 
                 48.5 
                 46.2 
                 0.953 
                 90/75 
               
               
                 605255 
                 57.4 
                 46.9 
                 46.9 
                 44.1 
                 0.940 
                 90/80 
               
               
                 605262 
                 57.2 
                 47.9 
                 48.3 
                 45.0 
                 0.931 
                 70/85 
               
               
                 605263 
                 53.6 
                 49.7 
                 49.8 
                 47.8 
                 0.959 
                 80/75 
               
               
                 605253 
                 52.6 
                 48.4 
                 48.2 
                 45.4 
                 0.942 
                 85/75 
               
               
                 605266 
                 62.6 
                 49.4 
                 48.3 
                 47.6 
                 0.986 
                 70/65 
               
               
                 605269 
                 52.8 
                 50.5 
                 49.6 
                 46.9 
                 0.945 
                 80/90 
               
               
                 605268 
                 52.0 
                 49.9 
                 48.7 
                 47.0 
                 0.965 
                 85/75 
               
               
                 605270 
                 57.0 
                 49.2 
                 48.5 
                 45.7 
                 0.944 
                 80/85 
               
               
                 605267 
                 59.8 
                 49.3 
                 47.6 
                 45.4 
                 0.953 
                 60/65 
               
               
                   
               
             
          
         
       
     
     
       
         
               
               
               
               
               
               
               
             
           
               
                 TABLE 7 
               
               
                   
               
               
                   
                 CPT 
                   
                   
                   
                   
                   
               
               
                 Charge 
                 Average 
                 CCT Average 
                 RPO,12 RT 
                 Rm RT 
                 A RT 
                 Z RT 
               
               
                   
               
             
             
               
                 605258 
                 84 
                 68 
                 725 
                 929 
                 40 
                 73 
               
               
                 605249 
                 74 
                 78 
                 706 
                 922 
                 38 
                 74 
               
               
                 605259 
                 90 
                 85 
                 722 
                 928 
                 39 
                 73 
               
               
                 605260 
                 93 
                 70 
                 709 
                 917 
                 40 
                 73 
               
               
                 605250 
                 89 
                 83 
                 698 
                 923 
                 38 
                 75 
               
               
                 605251 
                 95 
                 65 
                 700 
                 909 
                 37 
                 74 
               
               
                 605261 
                 93 
                 78 
                 718 
                 918 
                 40 
                 73 
               
               
                 605252 
                 87 
                 70 
                 704 
                 909 
                 38 
                 74 
               
               
                 605254 
                 93 
                 80 
                 695 
                 909 
                 39 
                 73 
               
               
                 605255 
                 84 
                 65 
                 698 
                 896 
                 37 
                 74 
               
               
                 605262 
                 80 
                 83 
                 721 
                 919 
                 36 
                 75 
               
               
                 605263 
                 83 
                 75 
                 731 
                 924 
                 37 
                 73 
               
               
                 605253 
                 96 
                 75 
                 707 
                 908 
                 38 
                 73 
               
               
                 605266 
                 63 
                 78 
                 742 
                 916 
                 34 
                 71 
               
               
                 605269 
                 95 
                 90 
                 732 
                 932 
                 39 
                 73 
               
               
                 605268 
                 75 
                 85 
                 708 
                 926 
                 38 
                 73 
               
               
                 605270 
                 95 
                 80 
                 711 
                 916 
                 38 
                 74 
               
               
                 605267 
                 58 
                 73 
                 759 
                 943 
                 34 
                 71 
               
               
                   
               
             
          
         
       
     
     In order to investigate more in detail the structure stability the test pieces were annealed for 20 minutes at 1080° C., 1100° C., and 1150° C. after which they were quenched in water. 
     The temperature at which the amount of intermetallic phase became negligible was determined by means of investigations in light optical microscope. A comparison of the structure of the charges after annealing at 1080° C. followed by water quenching indicates which charges that are more likely to contain undesired sigma phase. The results appear from Table 8. Structure control shows that the charges 605249, 605251, 605252, 605253, 605254, 605255, 605259, 605260, 605266 and 605267 are free from undesired sigmaphase. Further, charge 605249 alloyed with 1.5% cobalt is free from sigmaphase whereas charge 605250 alloyed with 0.6% cobalt contains some sigmaphase. Both charges are alloyed with high chromium content close to 29 wt % and molybdenum content of close to 4.25 wt %. If we compare the analysis for charges 605249, 605250, 605251 and 605252 with regard to sigma phase content it is very clear that the interval of the analysis for the optimal material with regard to in this case structure stability is very tight. Further, it appears that charge 605268 contains only minor sigmaphase compared with the charge 605263 which contains large amount of sigmaphase. The essential difference between these two charges is the added copper amount into charge 605268. In charge 605266 and 605267 the sigmaphase is free from high chromium content whereby the latter charge is alloyed with copper. Further the charges 605262 and 605263 containing 1.0 wt % tungsten appear with a structure having high amount of sigmaphase whereas it is of interest to observe that charge 605269 also containing 1.0 wt % tungsten but with higher nitrogen content that 605262 and 605263 appear with a substantially smaller amount of sigmaphase. Hence, it is required carefully balanced amounts between the various alloy elements at these high amounts of elements as regards for example chromium and molybdenum for achieving good structure properties. 
     
       
         
               
               
               
               
               
               
               
               
               
             
           
               
                 TABLE 8 
               
               
                   
               
               
                 Charge 
                 Sigma phase 
                 Cr 
                 Mo 
                 W 
                 Co 
                 Cu 
                 N 
                 Ru 
               
               
                   
               
             
             
               
                 605249 
                 1 
                 28.8 
                 4.23 
                   
                 1.5 
                   
                 0.38 
                   
               
               
                 605250 
                 2 
                 28.8 
                 4.24 
                   
                 0.6 
                   
                 0.40 
                   
               
               
                 605251 
                 1 
                 28.1 
                 4.24 
                   
                 1.5 
                   
                 0.38 
                   
               
               
                 605252 
                 1 
                 28.4 
                 4.23 
                   
                 0.5 
                   
                 0.37 
                   
               
               
                 605253 
                 1 
                 28.8 
                 4.16 
                   
                 1.5 
                   
                 0.37 
                   
               
               
                 605254 
                 1 
                 26.9 
                 4.80 
                   
                 1.0 
                   
                 0.38 
                   
               
               
                 605255 
                 1 
                 28.6 
                 4.04 
                   
                 3.0 
                   
                 0.31 
                   
               
               
                 605258 
                 2 
                 29.0 
                 4.23 
                   
                 1.5 
                   
                 0.46 
                   
               
               
                 605259 
                 1 
                 29.0 
                 4.23 
                   
                 0.6 
                   
                 0.45 
                   
               
               
                 605260 
                 1 
                 27.5 
                 4.22 
                   
                 1.5 
                   
                 0.44 
                   
               
               
                 605261 
                 2 
                 27.8 
                 4.22 
                   
                 0.6 
                   
                 0.43 
                   
               
               
                 605262 
                 4 
                 27.6 
                 3.93 
                 1.0 
                 1.0 
                   
                 0.36 
                   
               
               
                 605263 
                 5 
                 28.7 
                 3.96 
                 1.0 
                 1.0 
                   
                 0.40 
                   
               
               
                 605266 
                 1 
                 30.0 
                 4.02 
                   
                   
                   
                 0.38 
                   
               
               
                 605267 
                 1 
                 29.3 
                 4.23 
                   
                   
                 1.5 
                 0.38 
                   
               
               
                 605268 
                 2 
                 28.2 
                 3.98 
                 1.0 
                 1.0 
                 1.0 
                 0.43 
                   
               
               
                 605269 
                 3 
                 28.5 
                 3.97 
                 1.0 
                 1.0 
                   
                 0.45 
                   
               
               
                 605270 
                 3 
                 28.8 
                 4.19 
                   
                 1.5 
                   
                 0.41 
                 0.1 
               
               
                   
               
             
          
         
       
     
     In Table 8, numeral 1 for sigma phase is equivalent to free from undesired sigma phase. 
     Example 3 
     The stress picture for a wire in a wireline application is mainly composed of three components as appears from Table 9: the wire&#39;s dead load pursuant to equation (1), the impacted load according to equation (2) and the stress induced by the various support wheels of the feeding equipment according to equation (3) and the total tension expressed as the sure of partial tensions according to equation (4). As appears from the expressions for the various tensions; described below, a higher tension/ultimate strength enables use of smaller feeding wheels as well as larger added load per area unit. 
     
       
         
               
               
             
               
               
               
             
           
               
                 TABLE 9 
               
               
                   
               
               
                   
                 Expression for induced tension 
               
               
                   
               
             
             
               
                   
               
             
          
           
               
                   
                 (1) Wire dead load 
                 σ 1  = ρgl/2; ρ = material density 
               
               
                   
                   
                 g = acceleration of gravity, l = the free 
               
               
                   
                   
                 length of the wire in the drill hole 
               
               
                   
                 (2) Added load 
                 σ 2  = F/A; F = added load, A = wire 
               
               
                   
                 (3) Support wheel 
                 σ 3  = dE/R; d = wirediameter, E = E-modulus 
               
               
                   
                   
                 R = support wheel radius 
               
               
                   
                 (4) Total 
                 σ = σ 1  + σ 2  + σ 3   
               
               
                   
               
             
          
         
       
     
     A long wire can in the intended application as slickline amount to 30,000 feet length and will appear with a remarkable dead load which will load upon the wire. Thus dead load is usually carried by a wheel of varying curvature which will add to the load impact upon the wire. The smaller radius of curvature used for the wheel the higher will the bending load be that is implied upon the wire. At the same time, a smaller wire diameter will sustain larger amounts of winding. The alloy of the invention appears surprisingly to have a very high corrosions resistance in an environment relevant for the application of wirelines. 
     A higher strength of the alloy can be achieved for a given reduction according to the invention as compared with conventional alloys. Hence, a produced amount of goods with dimension 2.08 mm (0.082″) is obtained with the following data: 
     Charge: 456904 
     Final dimension: 2.08 mm 
     E-modulus: 195266 N/mm2 
     Rm: 1858 N/mm2 Breaking load: 6344 N=1426 lbf 
     No presence of sigmaphase 
     Ductility: Acceptable 
     Table 10 shows strength and break load for the alloy of the invention as compared with hitherto used alloys: 
     
       
         
               
               
               
             
               
               
               
               
               
               
               
               
               
               
               
             
               
               
               
               
               
               
               
               
               
               
               
             
           
               
                 TABLE 10 
               
             
             
               
                   
               
               
                   
                 Tensile 
                   
               
               
                   
                 Str 
                 Break load(lbf)per size(inch) 
               
             
          
           
               
                 Alloy 
                 PRE 
                 ksi 
                 MPa 
                 .072″ 
                 .082″ 
                 .092″ 
                 .108″ 
                 .125″ 
                 .14″ 
                 .15″ 
               
               
                   
               
             
          
           
               
                 GD22 
                   
                 225 
                 1550 
                 916 
                   
                 1495 
                 2061 
                 2761 
                   
                   
               
               
                 GD31Mo 
                   
                   
                   
                   
                   
                   
                   
                 2822 
                   
                   
               
               
                 High Strength 
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
               
               
                 Bridon SUPA 
                   
                   
                   
                   
                 1240 
                 1550 
                 2030 
                 2560 
                   
                   
               
               
                 75 
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
               
               
                 Sandvik SAF 
                 35 
                 250 
                 1700 
                 1010 
                 1310 
                 1650 
                 2275 
                 3045 
                 3795 
                 4356 
               
               
                 2205 
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
               
               
                 Sandvik SAF 
                 43 
                 255 
                 1750 
                 1035 
                 1345 
                 1690 
                 2330 
                 3120 
                   
                   
               
               
                 2507 
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
               
               
                 Alloy 
                 46 
                   
                 1858 
                   
                 1426 
                   
                   
                   
                   
                   
               
               
                 according to 
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
               
               
                 the invention 
               
               
                   
               
             
          
         
       
     
     These properties will make an alloy of the invention very suitable for use within O &amp; G-industry such as in applications for wirelines, slicklines or control cables. 
     SUMMARY 
     The present invention has a unique combination of
         High corrosion resistance   High strength both in hot worked status as well as after cold working   Good ductility   Good structure stability, minimal risk of precipitation of intermetallic phases provided that controlled temperature conditions are maintained   Good hot workability