Sintered carbonitride cutting insert with improved wear resistance

Abstract: The present invention relates to a sintered titanium based carbonitride alloy for milling and turning where the hard constituents are based on Ti, Zr, Hf, V, Nb, Ta, Cr, Mo and/or W and 3-25 % binder phase based on Co and/or Ni. The alloy is characterized in that the bottom of crater caused by the crater wear consists of grooves with a mutual distance between their peaks of 40-100 µm, preferably 50-80 µm, and where the main part, preferably >75 % of the grooves have a height of >12 µm, preferably >15 µm.

Description: The present invention relates to a sintered carbonitride alloy having titanium as main component intended for use as an insert for turning and milling with improved wear resistance without an accompanying decrease in toughness. Classic cemented carbide, i.e., based upon tungsten carbide (WC) and with cobalt (Co) as binder phase has in the last few years met with increased competition from titanium based hard materials, usually called cermets. In the beginning these titanium based alloys were based on TiC+Ni and were used only for high speed finishing because of their extraordinary wear resistance at high cutting temperatures. This property depends essentially upon the good chemical stability of these titanium based alloys. The toughness behaviour and resistance to plastic deformation were not satisfactory, however, and therefore the area of application was relatively limited. Development has proceeded and the range of application for sintered titanium based hard materials has been considerably enlarged. The toughness behaviour and the resistance to plastic deformation have been considerably improved. This has been done, however, by partly sacrificing the wear resistance. An important development of titanium based hard alloys is substitution of carbides by nitrides in the hard constituent phase. This decreases the grain size of the hard constituents in the sintered alloy. Both said decrease in grain size and the use of nitrides lead to the possibility of increasing the toughness at unchanged wear resistance. Characteristic for said alloys is that they usually are considerably more finegrained than normal cemented carbide, i.e., WC-Co-based hard alloy. Nitrides are also generally more chemically stable than carbides which results in lower tendencies to stick to work piece material or wear by solution of the tool, so called diffusion wear. In the binder phase, the metals of the iron group, i.e., Fe, Ni and/or Co, are used. In the beginning, only Ni was used, but nowadays both Co and Ni are often found in the binder phase of modern alloys. The amount of binder phase is generally 3 - 25 % by weight. Besides Ti, the other metals of the groups IVa, Va and VIa, i.e., Zr, Hf, V, Nb, Ta, Cr, Mo and/or W, are normally used as hard constituent formers as carbides, nitrides and/or carbonitrides. There are also other metals used, for example Al, which sometimes are said to harden the binder phase and sometimes improve the wetting between hard constituents and binder phase, i.e., facilitate the sintering. A very common structure in alloys of this type is hard constituent grains with a core-rim structure. An early patent in this area is US 3,971,656 which comprises Ti- and N-rich cores and rims rich in Mo, W and C. It is through Swedish patent application SE 8902306-3 known that at least two different combinations of duplex core-rim-structures in well balanced proportions give optimal properties regarding wear resistance, toughness behaviour and/or plastic deformation. When using inserts of sintered carbonitride in turning and milling the inserts are worn. On the rake face(that face against which the chips slide) so called crater wear is obtained when the chip comes in contact with the insert. In connection herewith, a crater is formed which successively increases in size and gradually leads to insert failure. On the clearance face, that face which slides against the work piece, so called flank wear is obtained which means that material is worn away and the edge changes its shape. An advantage of titanium-based carbonitride alloys compared to conventional cemented carbide is the good resistance against flank wear. Decisive for the tool life is therefore most often the crater wear and how this crater moves towards the edge whereby finally crater breakthrough takes place which leads to total failure. Fig 1 to 4 show the crater wear for inserts according to known technique and according to the invention respectively. It has now turned out that it is possible to increase the level of performance by manufacturing the material such that relatively coarse, well developed grooves are formed in the bottom of the crater which is formed during machining as a result of the wear. With this structure the wear resistance can be increased without a corresponding decrease in toughness behaviour. As a consequence, a changed wear mechanism is obtained. On one hand, the wear pattern of the rake face is changed with a decreased tendency to clad to workpiece material. On the other hand, the move of the resulting wear crater towards the cutting edge is considerably retarded. This retardation is much greater than what is to be expected from the depth of the crater. The cutting insert according to the invention has the features defined in claim 1. When the titanium based carbonitride cutting insert according to the invention is used, the bottom of the crater obtained due to crater wear consists of coarser, more well developed grooves, Fig 2 and 4, than of known material, Fig 1 and 3. The distance between the peaks of the grooves is according to the invention 40-100 µm, preferably 50-80 µm, and the main part, preferably >75%, most preferably >90% shall have a height >12 µm, preferably >15 µm. This type of wear is most pronounced when dry milling a low carbon steel with a Brinell hardness of 150-200 at a cutting speed of 200-400 m/min and a feed of 0.05-0.2 mm/tooth. A material with a wear pattern according to the invention is obtained if it is manufactured by powder metallurgical methods such that it contains a grain size fraction with coarser grains 2-8 µm, preferably 2-6 µm, mean grain size in a matrix of more normal mean grain size, <1 µm and such that the difference in mean grain size between the both fractions is > 1.5 µm, most preferably > 2 µm. A suitable volume fraction of the coarser grains is 10-50 %, preferably 20-40 %. The powdery raw materials can be added as single compound, e.g., TiN or complex compound, e.g., (Ti,Ta,V)(C,N). The desired 'coarse grain material' can also be added after a certain part of the total milling time. By doing so, the grains which shall give the extra wear resistance contribution are not milled for as long a time. If the material has good resistance against mechanical disintegration, it is even possible to use a raw material that does not have coarser grain size than the rest of the raw materials but nevertheless gives a considerable contribution to increased grain size of the desired material. The 'coarse grained material' can consist of one or more raw materials. It can even be of the same type as the fine grain part. It has turned out to be particularly favourable if a raw material such as Ti(C,N), (Ti,Ta)C, (Ti,Ta)(C,N) and/or (Ti,Ta,V)(C,N) is added as coarser grains because such grains have great resistance against disintegration and are stable during the sintering process, i.e., have low tendency to dissolution. Example 1 A powder mixture was manufactured with the following composition in % by weight: 15 W, 39.2 Ti, 5.9 Ta, 8.8 Mo, 11.5 Co, 7.7 Ni, 9.3 C, 2.6 N. The powder was mixed in a ball mill. All raw materials were milled from the beginning and the milling time was 33 h. (Variant 1). Another mixture according to the invention was manufactured with identical composition but with the difference that the milling time for the Ti(CN) raw materials was reduced to 25 h. (Variant 2). Milling inserts of type SPKN 1203EDR were pressed of both mixtures and were sintered under the same condition. Variant 2 obtained a considerable greater amount of coarse grains due to the shorter milling time than variant 1. Both variants were tested in a basic toughness test as well as in a wear resistance test. The relative toughness expressed as the feed where 50 % of the inserts had gone to fracture was the same for both variants. A wear resistance test was thereafter performed with the following data: Work piece material: SS1672 Speed: 285 m/min Table Feed: 87 mm/min Tooth Feed: 0.12 mm/insert Cutting Depth: 2 mm The wear for both variants was measured continuously. It turned out that the resistance to flank wear was the same for both variants whereas the resistance to crater wear, measured as the depth of the crater, KT, was 20 % better for variant 2. The crater resulting from the crater wear had in variant 2 coarser, more well developed grooves, figs 2 and 4, than variant 1, figs 1 and 3. Due to the changed wear mechanism for inserts according to the invention the measured KT-values do not give sufficient information about the ability to counteract the move of the crater towards the edge. It is, however, this mechanism that finally decides the total life, i.e., the time to crater breakthrough. In an extended wear test, i.e., determination of the time until the inserts have been broken performed as 'one tooth milling' with the above cutting data it turned out that there is a greater difference in tool life between the variants than indicated by the KT-values. Variant 1 had a mean life of 39 min (which corresponds to a milled length of 3.4 m) whereas the mean tool life of variant 2 was 82 min corresponding to a milled length of 7.2 m, i.e., an improvement of >2 times. Example 2 A powder mixture was manufactured with the following composition in % by weight: 14.9 W, 38.2 Ti, 5.9 Ta, 8.8 Mo, 3.2 V, 10.8 Co. 5.4 Ni, 8.4 C, 4.4 N. The powder was mixed in a ball mill. All raw materials were milled from the beginning and the milling time was 38 h. (Variant 1). Another mixture according to the invention was manufactured with identical composition but with the difference that the milling time for the Ti(CN) raw material was reduced to 28 h. (Variant 2). Turning inserts of type TNMG 160408 QF were pressed of both mixtures and were sintered at the same occasion. Even in this case a considerable difference in grain size could be observed. Technological testing with regard to basic toughness showed no difference at all between the variants. On the other hand, the same observation as in the previous example could be done, i.e., a retardation of the growth of the crater towards the edge. The following cutting data were used: Work piece material: SS2541 Speed: 315 m/min Feed: 0.15 mm/rev Cutting Depth: 0.5 mm The mean life for variant 2 was 18.3 min which is 60 % better than variant 1 which worked in the average 11.5 min. In all cases, crater breakthrough was life criterium. The flank wear resistance was the same for both variants. The depth of the crater, KT, could not be determined due to the chip breaker.

Claims: Cutting insert for turning and milling consisting of sintered titanium based carbonitride alloy containing hard constituents based on Ti, Zr, Hf, V, Nb, Ta, Cr, Mo and/or W and 3 - 25 % binder phase based on Co and/or Ni, at which the structure comprises at least two different grain sizes and consists of 10 - 50 % by volume hard constituent grains including Ti(C,N), (Ti,Ta)C, (Ti,Ta)(C,N) and/or (Ti,Ta,V) (C,N) having a mean grain size of 2 - 8 µm in a more fine-grained matrix with a mean grain size of the hard constituents of <1 µm and where said mean grain size of the coarse hard constituent grains is >1.5 µm larger than the mean grain size for the grains in said matrix, wherein the bottom of the crater obtained due to crater wear consists of grooves with a mutual distance between their peaks of 40 - 100 µm, at which the main part of the grooves have a height >12 µm.

Inventors: OESTLUND AKE, OSKARSSON ROLF, WEINL GEROLD, OESTLUND, AKE, OSKARSSON, ROLF, WEINL, GEROLD, Östlund, Ake
Applicants: SANDVIK AB, SANDVIK AKTIEBOLAG
Application year: 1992
Main classification: C22C29
IPC codes: C22C29, B23B27, C22C1, B23P15