GB1593213A - Method of machining workpieces after preheating - Google Patents

Description

(54) METHOD OF MACHINING WORKPIECES AFTER PREHEATING (71) We, VSESOJUZNY NAUCHO ISSLEDOVATELSKY, PROEKTNO KONSTRUKTORSKY I TEKH NOLOGICHESKY INSTITUT ELEK TROSVAROCHNOGO OBORUDO VANIA, and PRIOZVODST VENNOE OBIEDINENIE "IZHORSKY ZAVOD" both State Enterprises organised and existing under the laws of Union of Soviet Socialist Republics (U.S.S.R.), respectively of 10 Ulitsa Litovskaya, Leningrad, U.S.S.R., and I prospekt Lenina, Kolpino Leningradskoi Oblasti U.S.S.R. do hereby declare the invention, for which we pray that a patent may be granted to us, and the method by which it is to be performed, to be particularly described in and by the following statement: The present invention relates to metal working, and more specifically to methods of machining workpieces after preheating them.The invention can be adapted for application in machining cast and forged ingots and billets, in particular those having a hard skin of casting or made of hard-tomachine alloys, especially high-manganese or nickel-based alloys, as well as in machining workpieces having their surfaces coated with various wear-resistant materials.

The present invention provides a method of machining a workpiece after heating, wherein a portion of the workpiece material to be removed by a cutting tool is subjected immediately before the removal operation to intense localized heating by a plasma jet to a temperature at which the strength of material being machined is reduced.

According to the present invention there is provided a method machining a workpiece after preheating, wherein the workpiece material being cut by a tool is subjected immediately before the removal operation to intense localized heating and notching by plasma jet to form a groove in the surface of the material being cut, for which purpose a plasma torch is set ahead of the tool so that the plasma jet axis from its point of intersection with the workpiece surface being cut extends in a transverse plane lying at an angle within the range 0 to 450 to the plane of rotation of the workpiece at said point, and extends at an angle within the range 10 to 45" to a plane tangential to the circumfer- ence of the workpiece at said point.

The advantages of the invention reside in that the work-piece surface being cut is not only heated by the plasma jet but is also notched by the latter prior to being cut by the tool. The range of setting angles of the plasma torch, as indicated hereinabove, provides for the optimum operating conditions.

If the angles are smaller than those indicated the plasma cutting process will be inefficient, and with greater angles the material melted by the plasma jet may impinge on the machined surface. The better efficiency obtained when machining workpieces in accordance with the present invention results from the following circumstances.

In the first place, the groove formed on the workpiece surface being cut or machined allows an increase in the depth of the heating of the material in the direction of feeding of the cutting tool, since the plasma jet penetrates into the groove and more heat is applied to the material due to a larger area through which the heat is introduced. In addition, the groove formed on the surface being cut tends to reduce the cross-sectional area of the layer to be removed by the tool and contributes to easy deformation of the chip, thus relieving the tool of stress. The tool is further stress-relieved owing to the groove producing stress concentration on the surface being machined, with a consequent decrease in the force of cutting.

The aforementioned advantages of the method according to the invention enable the maching process to be more extensively controlled.

The groove may be positioned on different portions of the work surface being machined, and may vary in size, depending on the properties of the material processed.

Sometimes, it is advisable, throughout the machining process, that the distance between the edge of the groove nearest the cut workpiece surface, and the cut workpiece surface itself be maintained within 0.5 to 2 mm, the width "a" of the groove be maintained within 0.1C < a < 0.8C (where "C" is the width of the workpiece surface being cut), and the depth "b" of the groove be maintained within 0.15S < b < 0.9S (where "S" is the feed rate of the cutting tool per revolution or per stroke of the tool). The groove of a smaller size will not have any noticeable effect on the heating of the material and on the cutting force values, while with a larger-sized groove, the cut surface may be damaged, or else the material impinging on the tool may be overheated, causing the cutting edge thereof to be destroyed.

Alternatively, throughout the machining process, the depth of the groove may be at least 1.2 times the feed rate of the tool per revolution or per stroke, the width of the portion of the workpiece surface being cut between the cut workpiece surface and the groove not exceeding 0.8 times the width of the portion on the workpiece surface being cut between the workpiece surface to be machined and the groove.

This can be accounted for by the fact that, for a smaller depth of the groove, the cutting edge will lie at all times within the area of the material heated up to its melting point, resulting in the damage of the edge. The relative widths of the portions of the surface being cut separated by the groove are determined by different forces exerted on the respective parts of the cutting edge engaging these portions of the surface being cut, as will be shown in the detailed description of the invention.

The groove may also cover a portion of the workpiece surface being cut from a depth in the direction of feed equal to at least twice the feed rate per revolution or per stroke of the tool.

A smaller depth of the groove in the workpiece of low thermal conductivity materials prevents accumulation of the required quantity of heat in the layer being removed.

The invention is further illustrated by the detailed description of the embodiments thereof with reference to the accompanying drawings, wherein: Fig. 1 is a diagram showing in perspective the relative positions of a plasma torch and a cutting tool in the process of machining a workpiece after preheating, according to the invention; Fig. 2 is a longitudinal section of a workpiece being machined according to one embodiment of the invention; Fig. 3 is a longitudinal section of workpiece being machined according to another embodiment of the invention; Fig. 4 is a longitudinal section of a workpiece being machined according to still another embodiment of the invention; Fig. 5 is a longitudinal section of a workpiece with a wider surface being machined according to the method of the invention.

A workpiece 1 (Fig. 1) is machined using a plasma torch 2 and a tool 3, for example, on a turning lathe (not shown). The plasma torch 2 is positioned ahead of the cutting tool 3 on the same sliding carriage (not shown) where the cutting tool is fixed. V indicates the direction of the cutting speed. The position of the plasma torch 2 is in such that the plasma jet axis from its point of intersection 13 with the workpiece surface 4 being cut, extends in a transverse plane lying at an angle a within the range 0 to 45" to the plane of rotation of the workpiece at said point, and extends at an angle p within the range 10 to 45" to a plane tangential to the circumference of the workpiece at said point.The angle p which lies in said transverse plane is for convenience shown in Fig. 1 in an axial plane. The angles a and ss are selected in accordance with the size and material of the workpiece 1 to be machined, the feed rate of the cutting tool 3, the depth of cut, and the operating mode of the plasma torch 2. The distance H in cm, between the tip of the tool 3 and the intersection point 13 between the axis of the plasma torch 2 and the surface 4 being cut is adjusted within 0.01 V < H < 10V, where V is the cutting speed in cm/s, selected according to the cutting speed and the output of the plasma torch 2 employed.

By means of the plasma jet of the plasma torch 2, the material of the workpiece 1 on a portion 5 of its surface 4 being cut is heated to a temperature at which the strength of the material of the workpiece 1 is reduced.

Moreover, under the action of the plasma jet, the material of the portion 5 of the surface 4 of cutting is notched, and as the workpiece 1 is rotated, fresh portions of the material are effected by the plasma jet, causing a groove 6 to be formed on the surface 4 ahead of the cutting tool 3. The layer of the material together with the groove 6 is then removed by the tool 3.

The notching of the material on the surface 4 is provided by an appropriate adjustment of the power of the plasma torch 2 and the angles a and p within the limits specified.

With the angle a above 45 deg. and/or the angle p above 45 deg., the material melted by the plasma jet gets onto a cut surface 7.

On the other hand, with the angle p below 10 deg., the plasma cutting process proves to be inefficient.

To carry the method of the invention into effect a plasma torch is used with air as a plasma-forming gas. A variety of plasma torches may be adapted to be employed, such as the hafnium electrode torch for plasma cutting disclosed in the accepted British Application No. 1,220,205. Adoption of air as a plasma-forming gas ensures the maximum possible increases in the machining efficiency due to the following unexpected fact ascertained by the inventors.

With respect to roughing conditions, in the cases where the depth of cut is at least two to three times the feed rate, the maximum speed of cutting without preliminary heating is less than the speed of air-plasma cutting of sheets with a thickness equal to the feed value.

It has been found that the speed V of airplasma cutting of a steel sheet may amount to a value expressed by the following relationship: 13.2 V - cm/s, b were b is the thickness of the sheet, in cm.

The process of forming the groove 6 on the surface 4 by means of a plasma jet may be regarded as plasma cutting, and therefore, when realizing the method of machining work-pieces after preheating according to the invention, cutting speeds can be additionally increased at will.

For example, whereas conventional machining of work-pieces made of highmanganum steel alloys is generally performed, without preheating, at a speed of V = 20m/min = 33cm/s,withafeedrateS = 1.5 m/rev, the use of the above relationship makes it possible to obtain the depth "b" of the groove 6 formed by the plasma jet, at a given cutting speed: 13.2 13.2 b = = - - = 0.39 cm = 3.9 mm V 33 Thus the depth of the groove so formed exceeds the feed rate S = 1.5 mm/rev. As a consequence, the chip removed by the cut ting tool 3 will be divided into two portions, which results in reduction of the cutting forces acting on the cutting tool 3, and hence in its longer service life for a given cutting speed.

Another embodiment of the invention allows for raising the cutting speed or the feed rate, the service life of the tool 3 being the same as in the case of machining workpieces without preheating.

The size of the groove 6 and its position on the surface 4 are governed by the heat and temperature conductivity of the material to be machined, by the optimum cutting temperature of the material in question, and by the distribution of its strength properties over the width of the surface 4.

Fig. 2 shows a longitudinal section of the workpiece 1 machined in accordance with one embodiment of the method of the present invention, preferably used in case the material to be machined exhibits a sufficiently high thermal conductivity, and when the maximum permissible stress on the cutting tool 3 is restricted to the tip thereof. The distance "1" between the edge of the groove 6 nearest the machined surface 7 and this surface 7 is maintained throughout the machining process within 0.5 to 2 mm depending on the depth of cut and the desirable surface finish.The width "a" of the groove 6 is kept with 0.1C G a S 0.8C, where "C" is the width of the surface 4 being cut, and the depth "b" of the groove 6 is within 0.15S < b < 0.95S, where "S" is the feed of the cutting tool 3 per revolution (for turning operation or per stroke (for planing operation).

Fig. 3 shows a longitudinal section of the workpiece machined in accordance with another embodiment of the invention, used in machining heat-proof steels and alloys.

The depth "b" of the groove 6 is at least 1.2 times the feed "S" per revolution (for turning operation) or per stroke (for planing operation). After the passage of the tool 3, a groove 8 of a depth "bl" and a width "al" is lef behind on the surface 4 of cutting. The groove 6 divides the surface 4 into two portions 9 and 10, as that the width of the portion 9 of the surface 4 between the machined surface 7 and the groove 6 is not more than 0.8 times the width of the portion 10 of the surface 4 between the groove 6 and a surface 11 to be machined.

The depth "b" of the groove 6 exceeding the feed value "S" per revolution or stroke allows the chip removed by the tool 3 to be divided into two parts with the consequent reduction of the force acting on the cutting tool 3 due to an appreciable decrease in the cross-sectional area of the chip removed. The portion of the cutting edge of the tool 3 used in turning the portion 10 of the surface 4 will be working in the free-cutting mode. The resulting total force acting on the cutting edge is substantially reduced.The value of depth of the groove 6 exceeding the feed rate per revolution or stroke is determined by the fact that, with a smaller depth of the groove 6, the width a, of the groove 8 left on the surface 4 after the cutting tool 3 has passed, would be very small, and some stray metal drops left in the groove would stick to the cutting face of the tool 3 causing it to be melted and destroyed.

The position of the groove 6 on the surface 4 is determined, first, by the fact that the force acting on one portion of the cutting edge of the tool 3, engaging the portion 9 of the surface 4 and operating in the non-free cutting mode, is invariably more than the force acting on the other portion of the cutting edge engaging the portion 10 of the surface 4 and operating in the free cutting mode, and secondly, by the fact that it is necessary to supply heat and to heat the metal cut by the tip of the tool 3, where the heat exchange is considerably greater than in the metal adjacent the surface 11 to be machined.

After the surplus metal has been removed by the cutting tool 3 on the surface 4, the groove 6 is not completely removed together with the surplus, and the remaining portion 8 thereof is exposed to the plasma jet of the plasma torch 2 with the next revolution or stroke (Fig. 1) which deepens it up to an appropriate depth. By a proper choice of the operating mode of the plasma torch 2, the cutting speed, and the angles a and p, the machining is performed so that the depth bl of the groove 8 (Fig. 3) left on the surface 4 of cutting after the passage of the cutting tool 3 is maintained constant throughout the machining process, and the position of the groove 6 on the surface 4 with respect to the machined surface 7 remains unaltered.

When machining cast parts, particularly centrifugally cast pipes, the maximum stress on the cutting edge of the tool 3 will be produced by the upper surface layer which generally contains a great quantity of sand or other abrasive inclusions. In such cases, the groove 6 (Fig. 4) is so positioned that it covers a portion of the surface 11 to be machined for a depth, in the feeding direction of the cutting tool 3, equal to at least twice the feed S per revolution or stroke.

In case the surface 4 is sufficiently wide, for example, as wide as 25 to 40 mm, and it is impossible to effect a thorough heating of the zone adjacent the tip of the cutting tool 3 with the air of the groove 6 covering a portion of the surface 11 to be machined, another groove 12 (Fig. 5) is formed on the surface 4 of cutting, positioned similarly to, and having the same dimensions as those indicated for the groove 6 when referring to Fig. 2.

Example 1 The method of the invention was tested in roughing cylindrical ingots of low-carbon boiler steel, using the technique of vacuumarc remelting. The ingots were 1350 mm in diameter, about 5000 mm long, and had the mass of 41 to 42 tons. The skin of casting on the surface of the ingots contained up to 30 per cent manganum. The method was realized using a hafnium electrode torch for plasma cutting (as disclosed in the Accepted British Application No. 1,220,205). The plasma torch was set at an angle a = 7 deg., p = 17 deg. (Fig. 1), at a distance H = 370 mm. The arc current was 250 A, the arc voltage being 190 V. On the surface of cutting with its width varying from 15 mm to 20 mm as a result of a non-uniform machining allowance, a groove of 10 mm wide and 0.5 mm deep was formed.The feed rate of the hard-alloy tool was 2.5 mm/rev, the cutting speed was 30 m/min, and the average life of the tool was 57 min.

Example 2 When machining similar ingots of lowalloy steel, a hafnium electrode torch for plasma cutting was used. It was set at an angle a = 42 deg and p = 38 deg., at a distance H = 350 mm. The arc current was 270 A, and the arc voltage, 170 V. On the surface of cutting 7 to 10 mm in width, there was formed a groove 2 mm wide and 1.8 mm deep. The feed rate of the hard-alloy tool was 2.5 mm/rev. The cutting speed was 25 m/min, and the average life of the cutting tool was 50 min.

Example 3 When machining similar ingots of stainless steel OX18H1OT, a hafnium electrode torch for plasma cutting was used. It was positioned at an angle a = 15 deg., p = 29 deg., at a distance of H = 370 mm. The arc current was 250 A, and the arc voltage, 180 V. On the surface of cutting 12 to 15 mm wide, a groove was formed, 7 mm wide and 1.2 mm deep. The feed rate of the hard-alloy cutting tool was 2.5 mm/rev. The cutting speed was 34.5 m/min, and the average life of the cutting tool was 75 min.

Example 4 The method of the invention was tested in turning ingots of nickel alloy XH67BMT/0, 300 mm in diameter and 1700 mm long. A hafnium electrode torch for plasma cutting was positioned at an angle a = 12 deg. and p = 32 deg., at a distance of H = 270 mm. The arc current was 250 A, and the arc voltage, 180 V. On the surface of cutting, 10 to 12 mm wide, a groove was formed, 2.5 deep and 6 mm wide. The feed rate of the hard-alloy cutting tool was 1.75 mm/rev. The cutting speed was 12 m/min, and the life of the tool was 60 min.

Example 5 The method of the invention was tested in machining a centrifugually cast pipe of the 40X27H4ir alloy, 700 mm in diameter and with a wall 120 mm thick. There was a layer of metal sintered with quartz sand, 3 to 5 mm deep, on the surface of the pipe. A hafnium electrode torch for plasma cutting was set at an angle a = 15 deg. and p = 27 deg., at a distance of H = 430 mm. The arc current was equal to 300 A, and the arc voltage was 180 V. Formed on the surface of cutting was a groove covering the surface to be machined, which groove was 5 mm wide and 2.5 mm deep in the feeding direction. The cutting speed was 11 m/min, with the rate of feed being 1.03 mm/rev. The life of the hard-alloy tool was 120 min.

Thus, it will be seen from the aforementioned examples that the method according to the invention provides for a more efficient machining process, aside from a considerable saving in cutting tools.

It is to be understood that the present invention is not restricted to the above described specific embodiments thereof, and other modifications and variations of the invention are possible without departing from the scope as disclosed in the

Claims (6)

claims. WHAT WE CLAIM IS:

1. A method of machining a workpiece after preheating, wherein the workpiece material being cut by a tool is subjected immediately before the removal operation to intense localized heating and notching by plasma jet to form a groove in the surface of the material being cut, for which purpose a plasma torch is set ahead of the tool so that the plasma jet axis from its point of intersection with the workpiece surface being cut extends in a transverse plane lying at an angle within the range of 0 to 45" to the plane of rotation of workpiece at said point, and extends at an angle within the range of 100 to 45" to a plane tangential to the circumference of the workpiece at said point.

2. A method of machining a workpiece after preheating as claimed in claim 1, wherein the distance between the edge of the groove nearest the cut workpiece surface and the cut workpiece surface itself is maintained throughout the machining process within 0.5 to 2 mm, the width "a" of the groove is maintained within 0.1C < a < 0 8C where "C" is the width of the workpiece surface being cut, and the depth "b" of the groove is maintained within 0.15S < b S 0.9S, where "S" is feed per revolution or per stroke of the tool.

3. A method of machining a workpiece after preheating as claimed in claim 1, wherein the depth of the groove is throughout the machining process at least 1.2 times the feed per revolution or stroke, the width of the portion of the workpiece surface being cut between the cut workpiece surface and the grodve not exceeding 0.8 times the width of the portion of the workpiece surface being cut between the workpiece surface to be machined and the groove.

4. A method of machining a workpiece after preheating, as claimed in claim 1, wherein the groove covers a portion of the workpiece surface being cut for a depth in the direction of feed equal to at least twice the feed rate per revolution or per stroke of the tool.

5. Methods of machining workpieces after preheating, substantially as hereinbefore described with reference to the various Figures of the accompanying drawings.

6. A workpiece whenever machined by the method according to any one of claims 1 to 5.