CEMENTED CARBIDE

Abstract: In material applications in which besides a high wear resistance also excellent corrosion resistance, strength and toughness are required, conventional hard metal alloys have appeared inadequate. According to the invention a hard metal alloy now exists which fulfils these requirements. It is based on WC-Ni, and the binder phase of nickel is alloyed with low, well adjusted concentrations of above all Cr and Mo.

Description: CEMENTED CARBIDE The present invention relates to a new type of hard metal with excellent properties especially when used for construc¬ tion parts and wear parts but also as cutting tools and in rock drilling. More exactly the invention relates to a sintered hard metal alloy, in which the hard material prin¬ cipally is tungsten carbide (WC), and the binder phase is based on Ni with opti ixed additives of above all the ele¬ ments Cr and Mo. Since a long time hard metal, in which the hard material consists mainly of WC and the binder phase of Co, dominates when used in said applications. Principally in applications for high temperatures it has been favourable substituting WC for one or more of the carbides where Ti, V, Cr,- Nb, Hf, Mo and Ta are the metal components. When high oxidation resistance or high corrosion resistance is demanded, hard metal with TiC or Cr,C 2 as main component of the hard mate¬ rial and with a binder phase having Ni as main component, has been commercially used in rare applications. This in spite of the fact that the latter types of hard metal from a general point of view have got unfavourable properties of toughness. Hard metal of the type in which WC is the hard material but the binder phase consists of Ni has hitherto had only a li¬ mited use. Principally it is used in certain applications in the nuclear power industry where WC-Co cannot be used because of Co-isotopes of long half-lives. However, metallic Ni has several advantages, with respect to properties, over metallic Co. Thus, both the oxidation resistance and the corrosion resistance are better because of the higher electropotential of Ni than of Co in most reagences. Furthermore, Co is around 10 times more expensi¬ ve than Ni (Nov. 78) and the mean occurrenceof Ni in the earth crust is around- •_ times larger than the occurrence of Co. Ni is used as an alloying material in Co-alloys because of the higher corrosion resistance and oxidation resis¬ tance of Ni. This indicates especially favourable pro¬ perties of Ni-bound hard metal. This is especially valid in applications in critical working environments under reducing or oxidation conditions. Furthermore, a long life, often for years, is a necessary demand for an eco¬ nomically favourable use of an expensive hard metal part compared with for example a steel part, which is much cheaper. The physical and mechanical properties of hard metal where WC is the main component of the hard materials, are cha¬ racterized mainly by the mean grain size of WC, by the con¬ centration of binder phase and the composition of the binder phase. For hard metals the highest E-module, the lowest coefficient of thermal expansion and the highest thermal conductivity have hitherto been obtained when WC is the hard material. Furthermore, the highest toughness and a very favourable strength have been obtained for pure WC-Co hard metal. Generally the elasticity module of hard metal is influenced mainly by the composition and amount of the hard material and for comparable elasticity modules the transverse rupture strength is a good measure of the general properties of toughness of the hard metal. The hardness, the resistance of the material to plastic deformation, is a measure of strength. It is earlier known that for additives of Cr and Ni, respec¬ tively, to the binder phase of Wc-Co hard metal, which gives improved oxidation and corrosion resistances, a decrease of especially the toughness is obtained for Cr additives, whereas additives of Ni result in decrease of both tough¬ ness and strength. Additives of Cr in greater concentra¬ tions can furthermore lead to difficulties in controlling the carbon balance in sintered hard metal and to the for- mation of brittle double carbides in which the binder phase metals are components, which will result in drasticly de- • creased toughness. Additives of Fe cause still lower tough¬ ness than additives of Ni. Thus, it is well known that for hard metal with WC as main component of the hard material the alternative with Co in the binder phase is favourable principally from a tough¬ ness point of view. Especially for construction parts and wear parts the toughness properties of WC-Co hard metal are the fundamental properties which besides a good wear resistance have led to that hard metal has successfully been able to compete with materials as hard as hard metal and in certain cases very much cheaper materials, such as ceramic. However, the stated type of hard metal has got relatively limited corrosion resistance. The most common type of corro¬ sion damages on WC-Co hard metal involves a general corro¬ sion of the ductile binder phase, which is dissolved, and only a brittle WC-skeleton remains in the attacked area. This type of damage means that a dangerous indication of fracture has been created involving a catastrophic decrease of the real toughness of the detail. When increased corro¬ sion resistance or oxidation resistance is demanded, hard metal of a different type than WC-Co is therefore used in certain cases, but because of the inferior properties of toughness and wear resistance of these types the advantage of using hard metal compared to cheaper materials decreases. A hard metal type of improved corrosion resistance and oxi¬ dation resistance which has also got a good toughness is up to now missing. When high toughness of the hard metal is needed and at the same time a high corrosion resistance is demanded for a cer¬ tain application, constructions, where corrosion preventing water which is lead past the detail is protecting the detail of the corrosive medium, are utilized in exceptional cases. . In certain other cases- sacrificial anodes have been placed near the hard metal detail and protect the latter one of corro¬ sion by consuming themselves. The material of the anode is chosen to have a lower electro^potential than the hard metal in the present environment. In closed systems corrosion inhibitors can in certain cases be added to the system and inhibit the corrosion. All these up to now available ways of meeting high demands of toughness and corrosion resistan¬ ce of the hard metal require adjustments of the construc¬ tion to each specific working environment and will conse¬ quently be expensive. Also the constructions will be com¬ plicated when for instance pure corrosion preventing water must be supplied by a special system of pumps and systems for supervision are necessary. Small changes of the working environment which often occur in practical working, such as acidifying of process media, can destroy the function of the construction. This can cause a drastic increase of. the speed of consumption of the anode material or that added inhibitors will be without effect. According to the present invention a new type of hard metal now exists, which besides a very high wear resistance has got at least the good properties of toughness and strength of the WC-Co hard metal grades and which furthermore has got very good corrosion and oxidation resistances. This new hard metal type has properties to fill the hitherto lack of grades when both high toughness and high corrosion and oxidation resistances are required. This is valid with¬ out developing special constructions for the protection of the construction part or wear part. The hard metal type, whose content of alloying elements and structural consti¬ tuents is near a well known range, per se, obtains its sur¬ prisingly good properties by balanced proportions of alloying elements and, by extremely controlled production, optimized structural constituents. The alloy consists of 55 - 95 vol- hard material which essen¬ tially is WC, more than 90 vol# and preferably more than 95 vol , but also carbides in which the metal content is Ti, Zr, Hf, V, Nb and Ta, can be included in an amount of at most 10 vol-jt. The hard material is preferably composed of WC to minimum 98 vol-#. Thus, the binder phase, which com¬ prises the remaining structuralconstituent, comprises 5 - ' ^5 _. vol- of the hard metal. The binder phase comprises suitably between 8 - 40 vol-# of the hard metal. The main constituent of the binder phase is Ni, which comprises minimum 50 vol- , suitably more than 6θ vol-#. The binder phase contains dif¬ ferent alloying elements in solution and consists, besides of Ni, of 2 - 25 Cr, 1 - 15 % Mo, max. 10 Mn, max. 5 % Al, max. 5 Si,, max. 10 Cu, max. JO Co, max. 20 Fe and max. 13 W. (All the figures relate to vol-# of the bin¬ der phase.) Co and Fe substitute Ni in the ' binder phase and W is obtained from the hard material during sintering and its concentration is controlled by regulating the total car¬ bon concentration of the hard metal in the grinding.opera¬ tion. Suitably the concentration of W in the binder phase should not exceed 8 vol- of the sintered hard metal. The alloying elements, which are dissolved in the binder phase, can be classified into groups with respect to their influ¬ ence on the properties of the hard metal. Co or Fe, respec¬ tively, can in certain cases be included in concentrations up to 20 or 10 vol- , respectively, in the binder phase and will substitute Ni without deteriorating the surprisingly good properties. It is necessary to add Cr in concentrations of 2 - 20 vol- and Mo in concentrations of 1 - 6 vol-# of the totally added amount of binder phase in order to obtain the favourable properties. For additions of Cr in concentrations of 10 - - 25 vol-# and concentrations of Mo of 3 - 15 vol-#, where Cr + Mo together comprise at least 20 -τo - of the binder phase or where Mo comprises more than 6 vol- of the binder phase, also Al in concentrations 0.5 - 5.0 vol- , Si in con¬ centrations 0.5 - 5.0 vol-# or Cu in concentrations 0.5 - 10 vol-# must be added to the binder phase. Surprisingly, Al, Si or Cu of these concentrations have got a stabilizing in¬ fluence on the binder phase of this type of hard metal. If Al, Si or Cu are not added for the chromium and molybdenum concentrations given above, brittle phases are formed in the hard metal during sintering. The amount of added Cr + Mo inthe binder phase should not exceed 30 vol-# of the " latter one in order to retain the favourable properties. In certain cases, principally concer¬ ning solution hardening of the binder phase, it can be ad¬ vantageous partly substituting Ni and Cr by Mn, suitably in concentrations up to 8 vol- of the added amount of binder phase. The concentration of added chromium must not be below 3 vol-JJ. of the added amount of binder phase in order to re¬ tain the favourable properties. Completely determining for obtaining the good toughness pro¬ perties is, besides the interval given above for the content of Cr + Mo, that the total concentration of carbon of the sintered hard metal is kept within a narrow interval. This condition must be fulfilled in order to obtain a single pha¬ se and tough binder phase and in order to prevent the forma¬ tion of brittle carbides. The carbon concentration is influ¬ enced as well by the concentration of carbides and the type of carbides as by the concentration of added Cr + Mo. The following interval has been optimal when the hard material comprises only WC: w/o C = A. - B i χ (l00 minus w/o hard material) for pure WC: A^ - 6.13 For Cr + Mo between 3 - 15 vol-#, B ± - 0.06l - 0.008 (w/o C = total carbon For ' Cr + Mo between 16 - 35 vol-#, concentration of sin- B. = O.058 + 0.007 tered hard metal) - f< A For pure WC-Ni hard metal a two-phase structure can be ob¬ tained in the following interval: A. = 6.13, B * ■ _- O.069 + 0.010. For the case that besides WC also other carbides are included as hard material, the value of A. must be corrected according to the example below, where A. is the stoechiometric carbon concentration of each carbide, in w/o. Hard mmaatteerriiaall A Ai C 6.13 A i - l/lOO (w/o WC in hard material x TaC 6.22 6.13 + " w/o TaC in hard material x VC 19.08 6.22 + w/o VC in hard material x 19.08) For hard material compositions according to the invention, i.e. at least 90 vol-^ WC, the B-value according to the case with solely WC as hard material can with advantage be used. The interval given above for the total carbon concentration of the sintered hard metal involves, compared with pure WC- Ni hard metal, that the available interval for obtaining a single phase binder phase has been shrunk and displaced to a higher concentration of carbon with respect to the present WC-concentration in order to obtain the favourable properties. According to experience of development of WC-Co hard metal i the toughness can be influenced only by displacing the strength in the opposite direction. An increased concentra¬ tion of binder phase, alternatively a coarser mean grain size of WC, increases the toughness but causes decreased strength. These are hitherto the only known methods to im¬ prove the toughness provided that the hard metal structure from a general point of view is without objection. It is also known that the alloying of the Co binder phase " without exceptions causes deteriorated toughness but often also de¬ creased strength. It is therefore very surprising that additives .of Cr and Mo to WC-Ni hard metal according to the present invention cause both increased toughness and increased strength. Both Cr and Mo, from a ther o-dynamical point of view, are known as around as strong carbide stabilizers as W and therefore would be supposed to stabilize a formation of double car¬ bides. These are very brittle and should therefore cause a brittle hard metal. In the exceptional cases in which chro¬ mium and/or molybdenum additives have been previously used to hard metal with Ni binder phase, the additives must have been done with the purpose of increasing the corrosion and oxidation durabilities of the hard metal. Such alloys are reported in among others the Japanese publications (Kokai) 50-45708, 50-120410 and 50-27707. The additions have been great, however, too great for discovering the favourable influence of these alloying elements on toughness and strength. The alloying concentration has often been as great as the concentration of Ni or even greater, which has involved that a multi-phase and brittle binder phase has been obtained. The bad general properties above all bad toughness, which the hard metal has obtained in normal production and which also is due to bad wetting between the carbide phase and the multi-phase binder phase, have obviously been accepted as this was in accordance with knowledge obtained in development of WC-Co hard metal. It can be somewhat surprising that lower concentrations in alloying with chromium and molybdenum have not been previous¬ ly used. However, it is well known from the development of stainless steels that additives of for instance chromium below a threshold value which practically is around 13 w/o chromium, will increase the corrosion attacks on the steel. When also carbon is present, as in hard metal, this thres¬ hold value is further increased. As is obvious from tests with the present invented hard metal (cf. Example 2) this rule is not valid for alloying of the binder phase in the present case. It is previously known that if chromium and molybdenum are added each separately to WC-Ni hard metal, this results in a decreased toughness also for low alloying concentra¬ tions. Besides, the importance of the carbon concentration for especially favourable toughness properties has not pre¬ viously been noticed for the present type of alloy. It is known, however, that solely molybdenum, often added as Mo-carbide Mθ C, has got a certain positive influence on the toughness properties of TiC-Ni hard metal, which is very brittle and has low wear resistance compared to WC-Co hard metal. However, the Mo-concentrations which are actu¬ al for the alloy according to the invention, are only about one tenth of the optimum concentration for TiC-Ni hard metal, and also other essential differences between TiC- Ni hard metal and WC-Ni hard metal exist. The reason for the good toughness and strength properties • of the alloy according to the invention is probably an in¬ teraction of the influence of chromium and molybdenum on carbide phase and binder phase. Analysis of the constituents of the hard metal shows that Mo is alloyed in both the carbide phase and the binder phase whereas Cr principally is alloyed in the binder phase. The relatively high carbon concentration of sintered hard metal is necessary to keep the alloying amount of tungsten in the binder phase low in order to prevent the formation of brittle double carbides. Mechanical data for the invented hard metal show that the good strength principally is due to a strong alloying har¬ dening by the chromium addition. A low alloying of Mo in the carbide phase together with alloying of Mo and Cr in the binder phase result in a very good wetting between carbide phase and binder phase resulting in a very favourab¬ le toughness. The difference in hardness, which exists from a general point of view between "not alloyed" WC-Co and WC-Ni hard metal proves the weak solution hardening ability of tung¬ sten in Ni-bound hard metal. The alloying of tungsten in the binder phase is therefore kept low for the present in¬ vention by now actual carbon balance relations and additi¬ ves of aluminium, silocon or copper. Among the prepared binder phase compositions which appear extremely suitable to obtain the favourable toughness pro¬ perties and also a very good oxidation resistance and cor¬ rosion resistance the following analyses could be noticed, 1. 5 - 15 vol Cr, 1.5 - 6 vol Mo where the amount of Cr + Mo does not exceed 20 vol , Co up to 5, Fe up to 3 and W up to 8 vol and the rest Ni, where in Ni also normally occurring low concentrations of impurities are present. 2. 15 - 25 vol£ Cr, 3 - 10 vol# Mo, where the amount of Cr + Mo is in the range of 20 - 30 vol£, Al in concentrations " of 0.5 - 5 vol£ or Cu in concentrations of 0.5 - 8 vol#, Co up to 10, Fe up to 5 vol , W up to 7 vol# and the rest Ni, where in Ni also normally occurring low concentra¬ tions of impurities are present. Provided that the total carbon concentration of sintered hard metal is within the range of the invention, an especially favourable toughness is obtained for binder phase no. 1, where¬ as an especially favourable strength and favourable oxidation resistance and corrosion resistance are obtained for binder phase no. 2. The hard metal according to the invention is produced by pow- der metallurgy methods. Pure elements, hard materials and master alloys of parts of or of the complete binder phase, everything as powder, are the raw materials. The powder raw materials are usually ground in a milling equipment suitable ■ to the hard metal industry. Milling liquids without oxygen, such as benzene or xylol, are advantageously used to mini¬ mize the take up of oxygen by the powder during grinding. High concentrations of oxygen make the necessary control of the total carbon concentration of sintered hard metal diffi¬ cult. In certain cases, however, alcohol or acetone can be used as milling liquid. The powder is dried by evaporating the milling liquid at elevated temperature in a suitable inert atmosphere and is cooled to room temperature in this ' inert atmosphere to avoid oxidation of the powder. Sintering of the hard metal powder to a dense material and to the right constitution of structural constituents is suitably performed by so called direct sintering of a coldpressed powder body. Presintering, in which substances added in the grinding to aid in pressing are evaporated, and final sintering, in which the powder body shrinks to a dense material, is per¬ formed in one sequence. By this sintering procedure, the to¬ tal carbon concentration of the sintered material can be controlled in a satisfactory way, as among other things re- oxidation of the powder body after separate presintering is avoided. EXAMPLE 1 A number of hard metal variants comprising alloys as well within as outside the composition range according to the in¬ vention, were prepared for comparative investigations. The alloying elements, the main component of the binder phase, graphite added if necessary, and hard materials according to Table 1 below, everything as powder, were ground in a ball mill. The grinding liquid was benzene and as grinding bodi¬ es hard metal balls were chosen. To minimize the take up of oxygen in the pulp, the grinding was carried out under over- pressure of nitrogen. A grinding time of around 200h for a size of the powder batch of 5 kg resulted in a well-mixed powder of suitable grain size. The powder was dried by evaporating the grinding liquid at an elevated temperature in an inert atmosphere, such as nitrogen. The powder was cooled to room temperature in this inert atmosphere to minimize oxidation of the powder. The sintering of the hard metal powder to a dense material and to the right constitution of the structural constituents, was performed by so called direct sintering of a cold¬ pressed powder body. The pre-sintering, in which substances added, if necessary, in the grinding to aid in pressing are evaporated, and the final sintering, in which the powder body shrinks to a dense material, were carried out in one sequence. The sintering temperature and the time were suited to the amount of binder phase in the hard metal and to de¬ sired grain size of the tungsten carbide. A holding time of one to two hours and a sintering temperature of between 1410°C and 1550°C were suitable for the alloy according to the in¬ vention. The pre-sintering (if necessary) at a temperature of up to around 500 C was advantageously performed in hydrogen whereas the final sintering was performed in vacuum. OMPI TABLE 1 Variant Hard Hard Binder phase Carbon Sinteri material material vol- Composi- concentra- data vol-# Composi- Amount tion tion Temp/ti Amount tion in hard prepa- sin- in hard metal red tered metal w/o w/o 1 92 100WC 8 82Ni, 6Cr 6.04 5-86 1550°C 2Mo 2 92 ft 8 8 Ni, 11Cr 6.04 5.85 " 4Mo II 3 92 8 70Ni, 15Co, 6.04 5.86 1550°C llCr, 4Mo 4 92 It 8 lOONi 5-97 5.84 1550°C 5 92 II • 8 lOOCo 5-97 5.84 l500°C 6 85 11 .15 92Ni, 6CΓ, 5.73 5.60 1500°C 2Mo 7 It It 15 85Ni, llCr, 5.73- 5-60 " 4Mo 8 tl rt 15 73Ni, 15Cr, 5-73 5.62 " 12Mo 9 π It 15 73Ni, 19Cr, 5-76 5.63 " 6Mo, ; ..Al 10 n tl 15 Cr, 5-76 5-63 " 11 it tl 15 85Ni, 15CΓ 5-76 5.61 " 12 It It 15 85Ni, 15Mo 5-76 5-59 " 13 tt 11 15 lOONi . 5 5.57 " 14 Tt tt 15 100Co 5-65 5-58 l450°C 15 70 tl 30 85Ni, llCr, 5-10 5-02 l400°C 4Mo 16 tt tt 30 73Ni, 19Cr, 5-10 5.03 " 6Mo, .2A1 17 11 It 30 55Ni, 30Cr, 5.15 5.07 " 9Mo, <5A1 18 11 If 30 lOONi 5.03 4.95 " 19 It tl 30 .100Co 5.03 4.95 1350°C The oxygen concentration a ter .grinding and drying could be kept lower than 0.7 w/o in all variants except var. 17, whereas var. 17 had an oxygen concentration of 0.91 w/o. (As is previously known, nickel binder phase requires, compared with the same amount of Co-binder phase, around 50°C higher sin¬ tering temperature to obtain an objectionfree hard metal.) Metallographic and physical data and results of mechanical tests are given in table 2 below: TABLE 2 Variant WC grain Hardness Transverse E-module Tough- Fracture We size, HV3 rupture ness tough- re mean strength (Energy ness ta - to brea-K-, Re kage) ~ τc ve lu (/um) N/mm £ kN/mm* MN/n. va =1 1 1.5-1.8 1590 2600 640 ι_5 11.0 10 2 It 1620 2550 tl 1.6 11.0 12 3 It 1600 2500 tf 1.5 10.5 11 4 It 1440 1900 tl 0,7 8.0 6 5 tt 1590 2400 It 1.1 10.0 9 6 1.7-2.0 1 0 3200 600 3-2 15-0 6 7 It 1380 3200 tt 3,3 15.0 6 8 tt 1410 2100 tl 1.8 9.5 4 9 It 1450 3100 tt 3-2 14.5 7 10 tt 1460 3000 tt 3-2 13.5 8 11 tt 1350 2200 tt 1.9 9.5 4 12 11 1190 2100 It 1.8 9.5 3 13 tt ll8θ 2400 It 2.1 10.5 3 14 tl 1350 3000 It 3-1 13-5 5 15 1.7-2.0 1050 3000 500 5.2 23.0 1 16 " 1120 2900 5.1 22.5 1 17 tt 1125 2000 3-2 14,0 18 It 900 2300 3.5 17.0 9 1030 2800 4.8 22,0 1 HV3 has been carried out according to ISO 3878, transverse rupture strength according to ISO 3327, measurement of the elasticity module according to ISO 3312 and measurement of wear resistance according to CCPA (Cemented Carbide Produ¬ cers Association) P-112. As is obvious from the data of hardness above, an alloying according to the invention involves an increasing hardness compared with hard metal with not alloyed Ni-binder hase. The increase can be as high as + 25# for a high alloying in the binder phase, which indicates a strong alloying hardening of the binder phase. The 2 - 9 better hardness of the in¬ vented alloy, even compared with corresponding WC-Co grades^ can be explained by a higher alloying concentration in the binder phase. The transverse rupture strength is a good estimate of tough¬ ness but only for comparisons between hard metals with the same E-module (the same composition and amount of hard mate¬ rial), which is obvious from the data above (compare transver¬ se rupture strength with toughness (energy to breakage) and the fracture toughness parameter _ r .) The great increase of transverse rupture strength, 31 - 37# increase, of the in¬ vented alloy compared with "not alloyed" WC-Ni shows that a strong improvement of the wetting between binder phase and hard material phase has been caused by the alloying. The dif¬ ference of transverse rupture strength between hard metal with "not alloyed" Ni binder phase and hard metal with Co binder phase was of the same magnitude as is previously known. For an added concentration of 8 - 15 vol of Cr + Mo (variants 2, 3, 6, 7 and 15) even an increase of the transverse rupture strength of 6 - 8 was obtained compared with WC-Co hard metal. Variants 8, 12 and 17, in which deviating not identified pha¬ ses have been obtained, showed an unfavourable toughness and also an unfavourable resistance to abrasive wear. This in spi te of the fact that in some cases a favourable hardness was' obtained. These results confirm- the very good abrasive wear resistance of the tungsten carbide (WC) compared with other carbides. EXAMPLE 2 Test specimens, which were produced according to Example 1 and with amount of the binder phase and composition of the binder phase according to variants 6, 7 * 9 * . 13 * 1*•< ■ _• 1 * 18 and 19, Example 1 have been corrosion tested. In order to get a general testimony of the corrosion resistance of hard me¬ tal grades, the tests have been carried out in a serial of buffer solutions with pH-values between 1 and 11. The buf¬ fer solutions have compositions according to Table 3 below. TABLE 3 pH- Solution 1 0.1 M HC1 2 350ml 0.1 M HC1 + 150 ml 0.1 M di-Sodium hydrogen citr 3 300ml 0.1 M HC1 + 200 ml 0.1 M " - 4 225ml 0.1 M HC1 + 275 ml 0.1 M " 5 500 ml 0.1 M " 6 200ml 0.1 M NaOH + 300ml 0.1 M " 7 275ml 0.1 M KHgPO^ + 175ml 0.05 M Na^O-, * 10 HgO 8 200ml 0.1 M " + 250ml 0.05 M - " " 9 6θml 0.1 M " + 390ml 0.05 M " 10 340ml 0.1 M Na CO, + 110ml 0.05 " 11 440ml 0.1 M " + 12 ml 0.05 M " The corrosion tests were performed as immersion tests in the solutions above with a subsequent wear by SiC in alcohol in a porcelain mill. The subsequent wear was necessary to determine the total corrosion damage of the test specimens " SU (i.e. to wear off areas of the specimen, where the binder pha¬ se had corroded away but the WC-skeleton was intact after the immersion test). Data of the immersion test: Temperature: 26 - 1°C Time: 10 days Number of specimens: 3/ ariant Specimen: Ground specimen 09 x 15(mm) Results of the corrosion tests have been plotted in diagrams, Fig. 1. As is obvious from the results, the amount of binder phase in the hard metal, for the same composition of the bin¬ der phase, has not affected the corrosion loss (A) more than the scatter between different specimens of the same composi¬ tion variant (less than 15# of the mean value), in most cases a corrosion depth of 0.1 mm/year (D) is used as an upper li¬ mit for a material to be considered as corrosion resistant in a certain environment. A corrosion depth of 0.1 mm/year (D) corresponds to 3 - 42 mdd (= mg/24h x dm ) depending .of the density of the hard metal variant. As is obvious from the results of the tests, a WC-Co grade cannot be considered as corrosion resistant in environments of lower pH than 7 - Exchange of the binder phase for "not alloyed" Ni-binder phase involves a certain decrease of the corrosion losses. The decrease can probably not be utilized practically except in very special applications (which part¬ ly explains the limited commercial use of the WC-Ni hard metal). Additions of only 6 vol# Cr and 2 vol# Mo to the binder pha¬ se of the WC-Ni hard metal involved a drastic decrease of the corrosion losses. The hard metal was found to be corro¬ sion resistant down to pH 3« An additional addition of Cr + + Mo to the binder phase involved that a hard metal, corro¬ sion resistant also at pH 1, could be obtained. Thus, according to the invention, hard metal grades with me¬ chanical properties well comparable with WC-Co grades and corrosion resistant down to pH 1, can be produced. This com¬ pared with the WC-Co grades which are corrosion resistant down to only pH 7« EXAMPLE 3 The binder phase of sintered hard metal according to the invention has been analysed. The analyses were carried out partly with a high resolution, high sensitive microprobe analyser (Camebax from Camera, France) partly by so called phase separation and conventional chemical analysis. Hard metal manufactured according to Example 1 and with com¬ positions according to the variants 7* 8, 10, 11 and 13 in Example 1,has been analysed according to the methods mentio¬ ned above. The results are evident from Tables 4-6 below. TABLE 4 Prepared composition of the hard metal (85 vol£ WC • - 15 vol# binder * phase) • • - - Var 7 91. ,00 7.77 0.81 0.42 — 5.51- -5.65 8 91. .00 6.64 1.11 1.25 - 5.55- -5.67 10 91. .10 5.59 1.55 0.94 0.64 5.56-5.68 11 91. ,20 7.70 1.10 - - 5.52- -5.66 13 90. -90 9.10 - - - 5.4l- -5.59 x) Total carbon concentration of sintered hard metal analysed by a gravimetric method. Intervals calculated by previously given expression. TABLE 5 Prepared composition of binder • phase Var Ni Cr Mo Cu w/o w/o w/o w/o 7 86.3 9.0 4.7 — 8 73.8 12.3 13.9 - 10 64.8 17. 10.6- 7.2 11 87-5 12.5 - - 13 100 — — — TABLE 6 Results of analysis of binder phase Var Ni Cr Mό Cu W Co w/σ_-- vol w/o vol# w/o vol# w/o vol w/o ■ vbl% -W/o vόl# 7 78.3 8O.9 7.7 9-9 2.92.7 9.1 4.3 1.51.6 8 62.2 68.8 9.813.4 5.04.8 21.1 10.8 1.31.5 10 59-9 61.5 15.2 19.3 6.1 5.5 6.4 6.5 10.2 4.8 1.61.7 11 75.0 78.510.113.1 12.9 6.2 1.4 1.5 13 88.1 93.4 - 8.8 4.3 1.51.6 Var Fe /b ol# 7 0.5 0.6 8 0.6 0.7 10 0.6 0.7 11 0.6 0.7 13 0.6 0.7 0-.'PI_ The results given above are mean values of the concentra¬ tions of each element, respectively, obtained by the two different analysis methods. The Ni concentration has not been determined, so also normally occurring impurities in hard metal are included in the Ni concentration above. From the analyses above, it is evident that the added amount of Ni, Cr and Cu is almost completely dissolved in the bin¬ der phase of the sintered hard metal. The existing differen¬ ce between prepared composition, Table 5* and analysed com¬ position, Table 6, is due to a dilution of the binder phase by principally W from the hard material but also by Co and Fe from raw materials and production process. The analysis values of Cr can possibly indicate a slight dissolution in the carbide phase. However, for Mo a significant difference between the analysed and the prepared composition exists, which cannot be explai¬ ned by the dilution of the binder phase. Microprobe analysis of the carbide phase proved a dissolution of Mo in the carbi¬ de phase. For the variants 7 and 10 no new phases could be detected (detection limit: 0.1 /u ). For variant 8, however, a new phase could be detected which contained principally W and Mo but also Cr. The particle size of this phase was From the analysis values of tungsten in Table 6 it is evident, that principally Mo, but to a certain degree also Cr, in¬ creases the W-dissolution in the binder phase. The W-dissolu- tion can be decreased by increased carbon concentration of the hard metal, but for the relatively high alloying concen¬ trations such as in variant 10 (cf. var. 8) also Cu (or Al, Si, respectively) must be added to keep the W-concentration of the binder phase low and to avoid the formation of britt¬ le, undesirable phases. No brittle phases could be detected in variant 11 (the vari¬ ant in which Mo was missing). From unfavourable toughness data,according to Example l,of this variant, it is evident, that the natural reason for these values is that an alloy¬ ing amount of Mo in carbide phase and binder phase is neces¬ sary to obtain the good toughness properties. As this vari¬ ant has a good strength (HV 3 in Example 1, cf. also var. 12) it is evident that the alloying hardening of the binder phase is due to principally the alloying amount of Cr. EXAMPLE 4 Modern cutter suction dredgers which can dredge at bigger depths and with a bigger capacity have been developed. The big forces which are absorbed in pumps of these dredgers, cause great technical problems. Conventional high pressure pumps cannot be used because of the high demands, such as very abrasively wearing spoil materials, corrosion demands as the pumps often work in sea water and very high sur¬ face pressures, up to 2.5 MPa on a tightening surface of dimensions 0 i = 440, 0 - 46θ (mm) and a relative speed of 7 - 7.5 m/s. Exchange and ' repair of conventional pumps must be carried out as often as once a week. The development of a new type of shaft seal for these pumps, performed as a plane tightening with hard metal rings as tightening elements, has been described in the 8 Inter¬ national Conference on Fluid sealing, University of Durham, England 1978, Mechanical face seal for big pressure dredge pump. E. Muddle and I. Wisser, pp. H3 - 19 to 34. Laboratory tests, carried out as conventionalstick - against - " ring tests, and tests carried out in a special test rig on full scale, showed that a hard metal grade with 30 vol# Co binder phase (variant 19, Example 1) and with a hardness of around HV 1000, appears to be optimal as has been described in the reference mentioned above. The grade was optimal concerning: - Strength (hardness) by the resistance to abrasive- ear whic was suited to; - Toughness, i.e. in this case resistance to the formation of thermal fatigue cracks due to high thermal stress. In the test rig the corrosion demand together with the de¬ mand of strength and toughness could not be simulated in a satisfactory way. This resulted in a very strong wear of the hard metal rings in practical tests, a level wear of stator and rotor of around 5 mm, in all, after 3000 h testing time. Investigation of the tested rings proved relatively strong corrosion damages, as the dredging had been carried out in sea water. To meet the demand of increased corrosion resistance, at the same time paying regard to the demands of the optimal strengt and toughness of this application, hard metal according to variant 15, Example- 1, was produced. Because this variant had the same carbide phase as the hard metal previously used and furthermore cobalt and nickel have nearly the same coefficients of thermal expansion, the fastening technique described in the reference could be used also for the hard metal rings of the new grade. Function tests in test rig were carried out and showed that no changes of the construc¬ tion due to the change of grade were necessary. The seal rings of WC-NiCrMo were subsequently tested in practice in a dredger. After a testing time of 5000 h the pump was de¬ mounted for an overhaul. The level wear of the stator and rotor was less than 0.5 mm, in all. The leakage had been satisfactory for the whole testing time, i.e. less than 100 cm-γh. After the overhaul the seal has been tested for 1500 h more without any faults. EXAMPLE 5 In process industry, such as for paper pulp production, there are great demands for the corrosion resistance of construc- f __ tion parts. Acidproof constructions are extensively used. Furthermore the pulp is abrasively wearing. Thus, for shaft . seals, bearings and applications of that kind, parts of hard metal are established products. Because of high demands for abrasive wear resistance and toughness, only hard metal of the type WC-Co has been appropriate. The demand for corro¬ sion resistance has in these cases been solved with various success by placing sacrificial anodes near the hard metal part, or by constructions in which the hard metal is protected from the aggressive medium by water. Previously, plane seals of a WC-8 vol# Co grade (a grade with physical and mechanical data according to variant 5 * Example 1) have been used in a shaft seal of a pressure sieve for sieving sulphite lye..The pH of the sulphite lye varied be¬ tween 3«5 and 3-9 and the temperature of the lye was 70-90°C, and so sacrificial anodes of zinc were used to protect the plane seal. The life of the seal was unsatisfactory among other reasons due to demands for intense supervision of the con¬ struction, * as the consumption of zinc anodes was high and varied strongly. A life of one to three months was normal for the plane seal and the life criterion was a strong leakage. Principally to decrease the need of maintenance of the pres¬ sure sieve, which, except for the shaft seal, was made of " acid proof construction, a shaft seal, in which the sealing rings were made of WC-NiCrMo hard metal with 8 vol# binder phase (production, composition, physical and mechanical data correspond to variant 2, Example 1, i.e. composition of the binder phase: 85Ni, llCr, 4Mo (added vol )), was tested. No sacrificial anodes were placed in the pressure sieve. The shaft seal managed in continuous ' work for 8 months. The life criterion was leakage, which had been caused by abrasi¬ ve wear by solid particles in the lye. By exchange of the hard metal grade of the plane seal, the complete pressure sieve could successfully meet the corrosion resistance demands and . the need of maintenance was drasticly decreased. Furthermore, an increase of life of the plane seal of 3 times was ob¬ tained. EXAMPLE 6 For production of low pressure polyethylene, utilizing a high pressure process in the production, pistons, alternatively cylinder linings, made of hard metal are used in the high pressure compressors. The use of hard metal for these parts has involved an increase of life of 15 - 30 times, but the greatest gain is the strongly decreased cost of production stops and repairs. For parts for high pressure compressors, which have working pressures of up to 3500 bars (350 MPa), there are high demands for good properties of toughness and strength of the hard metal. To obtain these high pressures in the compressors and furthermore minimize time and costs of maintenance, there are high demands for surface smooth¬ ness (Ra = 0.04) and exact size tolerances of the parts, and high demands for surface smoothness and size not being chan¬ ged due to wear (in cooperation with other destruction mecha¬ nisms). A hard metal with composition, physical and mechanical data according to variant 14, Example 1, i.e. WC-15 volji Co with a mean grain size of WC of 1.7 - 2.0 /urn, has been used, with as a rule very good result, for pistons for high pressure compressors. Lives of 5000 - 15000 h between each regrinding are often obtained. The possibility of regrinding the pistons often is an irremissible demand due to the high cost of aqui¬ sition of the pistons, as they are made of hard metal. In a certain type of process for polyethylene production, how¬ ever, the WC-Co grade mentioned above has not given satis¬ factory lives when used as piston in the high pressure compres OA " V. sor. After regrinding of the piston, corrosion damages have been observed, in spite of a regrinding depth of 0.1 mm. The - reason for these strong corrosion attacks has not been possib¬ le to investigate completely, but organic acids are probably . formed already in the high pressure compressor due to paral¬ lel reactions, not possible to control. A piston of size 0 87 x 1203 mm was made of hard metal with composition, physical and metallographic data according to Example 1, variant 10, WC-15 vol (NiCrMoCu) with a mean grain size of WC of 1.7 - 2.0 um. The surface smoothness of the piston was Ra =_ 0.04 after finished polishing operation. After a testing time of 8500 h the piston was demounted for inspection. No defects could be discovered and so the piston was remounted in the high pressure compressor. The piston has now been tested for additional 1000 h without any faults. EXAMPLE 7 The use of hard metal e.g. for cutters for wood working compa¬ red with the use of cutters of conventional type of material, high speed steel, has involved a reduction of tool costs of However, in working of damp wood, degree of moisture more than 20j£ and pH max. 5, conventional WC-Co grades cannot be used because of inadequate corrosion resistance. The greatest cor¬ rosion problems arise in working of oak, cedar and chestnut , which in moist state evaporate mainly acetic acid but also formic acid, oxalic acid and citric acid to air. To get a hard metal grade for working of damp wood, techno¬ logical tests were carried out. Working tests were performed in moist oak, which had been stored in a relative humidity of 8θjt and with an analysed concentration of acetic acid of 0.90^. A working operation was performed as a milling ope- ration. The mill was mounted with plane indexable inserts of dimension 50 x 12 x 1.5 mm with 45° angle of clearance. 3 indexable inserts, 2 edges per insert, were tested per composition variant for 1000 running metres. To establish the quality of the edges, surface condition tests in dry birch were milled after 200 m and 1000 m. In each milled piece of wood a measurement of the surface smoothness was made. The hard metal inserts were weighed before and after the testing to determine the loss of weight due to wear in connection with corrosion. The results given below are mean values of six tested edges: Variant Composition of Max. value of Loss of weight binder phase surface deviation after 1000 m (prepared) R { am) (mg) vo -' & Milled running metres 200 m 1000 m 7 85Ni llCr 4 Mo 35 30 1.5 8 73Ni 15Cr l2Mo 85 95 9.0 14 100 Co 50 75 12.4 The great loss of weight which was obtained for variant 8, with a high concentration of molybdenum and a relatively bad toughness (cf. Example 1) was due to tear of the edge. This tear resulted in big surface deviations in the sur¬ face smoothness test which is evident from the table above. The corrosion of the WC-Co grade resulted in the biggest loss of weight of the tested grades and furthermore unfa¬ vourable surface deviations in the worked surface. Additional practical tests have confirmed that the variants no. 7 and no. 9 gave very good results in working of damp wood. By the very good corrosion resistance in combination 0-..P with the good properties of toughness and strength of these grades, hard metal can as a rule be used in the field of wood working with drasticly decreased costs of tools as re¬ sult. EXAMPLE 8 Conventional WC-Co hard metal cannot be used in hot rolling of copper because of a strong galvanic corrosion of the bin¬ der phase. Practical tests, e.g. in a Propertzi-work, in which rollers of high-speed steel previously have been used, have been carried out for conventional hard metal grades without obtaining an improved production result between the regrindings. The criterion of regrinding was a bad surface of the copper wire. By laboratory tests, simulating the high thermal stresses and the high demands for corrosion resistance present in hot rol¬ ling of copper wire, a new hard metal grade was made. Compo¬ sition: WC-25 ol^ binder phase, the mean grain size of the carbide phase was 3. Um, prepared composition of the binder phase: 65Ni, 20Cr, 6Mo, 5Cu, 4Mn (vol . *), carbon concentra¬ tion of sintered hard metal: .2 w/o C (in powder added con¬ centration: 5 * 35 w/o C). The transverse rupture strength was measured 3000 N/mm2 and the hardness according to HV3 was 1050. The preparation of this hard metal was carried out ana¬ logously to the variants of Example 1 with a milling time of l6θ h and a sintering temperature of l450°C, the time at l450°C was for 1 h. The developed hard metal grade was tested in rollers in the Propertzi-work mentioned above. For rolling of copper wire of a final dimension 0 6.35 mm, 19 reduction steps are used in the rolling mill. Three rollers were included in each reduc¬ tion step. For the two last reduction steps rollers of a hard metal according to the invention were used. For the other reduction steps the rollers were made of the highspeed steel grade previously used. The number of tons which were produced between regrinding of the rollers of the final pair was 300 tons for high-speed rollers in the last reduction step. This corresponds to the production of three shifts. The hard metal rollers could manage 2200 tons before the surface of the produced copper wire required a regrinding of the rollers. An investigation of the tested rollers showed that the surface of the roll groove contained thermal fati¬ gue cracks as for rollers of previously tested conventional hard metal of WC-Co type. On the contrary the surface of the roll groove contained no corrosion damages, often as pits in connection with the thermal fatigue cracks, which had been observed for WC-Co hard metal rollers previously tested. To inhibit the higher cost of aquisition of hard metal rollers compared with the high-speed steel rollers previously used, the hard metal rollers must produce between 900 and 1200 tons of wire between each regrinding which according to the facts above definitely can be obtained with rollers made of the alloy according to the present invention.

Claims: Claims 1. Sintered hard metal alloy of high wear resistance combi¬ ned with good toughness properties, good strength and excel¬ lent corrosion and oxidation resistances, said alloy contai¬ ning hard materials essentially comprising tungsten carbide and a binder phase comprising minimum 50 vol# nickel, c h a ¬ r a c t e r i z e d in said alloy comprising, in percentage by volume, 55 - 95 % hard materials which comprise minimum 90 WC and at most 10 % of one or more carbides of the me¬ tals Ti, Zr, Hf, V, Nb or Ta and 5 - 45 % binder phase, which besides Ni comprises 2 - 25j£ Cr, 1 - 15% Mo, max. 10 Mn, max. Al, max. 5 Si, max. 10 Cu, max. 30 Co, max. 20 Fe and max. 13 W, and in a total carbon concentration, in percentage by weight, when the hard material exclusively is tungsten carbide, of 6.13 - (0.0.61 - 0.008) (100 minus w/o hard material) for concentrations of Cr + Mo ' between 3 - 15 vol# and 6.13 - (0.058 ± 0.007) (100 minus w/o hard material), respectively, for concentrations of Cr + Mo between 16 - 35 ' vol . 2. Sintered hard metal alloy according to claim 1, c h a ¬ r a c t e r i z e d in said binder phase comprising, besides Ni, 2 - 20 % Cr and 1 - 6 % Mo. 3. Sintered hard metal alloy according to claim 1, c h a ¬ r a c t e r i z e d in said binder phase comprising, besides Ni, 10 - 25 % Cr and 3 - 15 % Mo and 0.5 - 5-0 % Al, 0.5 - - 5 % Si or 0.5 - 10 % Cu. 4. Sintered hard metal alloy according to any of the previous claims c h a r a c t e r i z e d in the hard material com¬ prising minimum 95 and preferably minimum 98 WC.

Inventors: LINDHOLM L
Applicants: LINDHOLM L, SANDVIK AB
Application year: 1980
Main classification: C22C29
IPC codes: C22C29