GB2364005A

GB2364005A - Surface forming of metal components

Info

Publication number: GB2364005A
Application number: GB0122535A
Authority: GB
Inventors: Stephen Robert Manley; Martin John Riley
Original assignee: Unova UK Ltd
Current assignee: Intermec Europe Ltd
Priority date: 1999-06-04
Filing date: 2000-05-12
Publication date: 2002-01-16
Anticipated expiration: 2020-05-12
Also published as: GB2364005B; GB0122535D0

Abstract

A metal machining process, in particular hard turning using a computer controlled precision lathe, comprises the step of controlling the tool to increase the depth of cut at intervals during machining, so as to create a plurality of depressions (12 to 16). As applied to a synchromesh cone (10), for example, the depressions may typically be annular and 1 micron in depth, with a base width of 0.16mm and spaced at 1.0mm along the taper. The process enables components to be produced whose surface is similar to that of ground components.

Description

2364005 Title: Surface forming of metal components.

Field of invention

This invention concerns the formation of surface finishes in machined components and applies both to internal and external surfaces.

Background to the invention

The surfaces of metal components hitherto surface-finished by a grinding process, have been specified by means of measurements which can be performed on the components as they are manufactured.

Typically these measurements have involved size tolerance at a particular position along the length of the component, an acceptable variation in the height of peaks to troughs in the surface when measured along a single line along the component, known as the Ra measure, and the bearing ratio of the peaks and troughs at one or more depths from the peaks This last measurement may be required to lie between a maximum and a minimum percentage of the length of the line.

Overall flatness has often been measured in terms of the percentage of the area of the surface which will be inked by a standard bluing gauge.

All other things being equal, provided the measurements on production components fall within the specification set down as acceptable by the designer, the components will be expected to function correctly for the purpose they are intended Thus for example surface finish specifications may be laid down for the bores in fuel injectors for diesel engines and for the cones for synchronous meshing of gears in transmission units.

Generally the surface finishing of such components has been achieved by grinding processes which, although superficially leaving a very smooth surface finish, in fact leave a pitted surface (at the micron level) since the removal of the metal is achieved by each piece of grit in the surface of the grinding wheel gouging out a tiny portion of the metal, with the relative rotation of the wheel and the component The grit contact with the metal is relatively random and arbitrary since the grit is not uniform in size and distribution and the result is a surface having a large number of tiny pockets relatively randomly distributed over the area of the surface.

It has been proposed to replace the grinding finishing step for such components with precision turning, sometimes referred to as hard turning It is an object of the present invention to provide a process and apparatus for achieving a machined surface finish which, to a first approximation, is within the specification laid down for the component when finished by grinding In this way, for example turned components can be compared alongside components produced by conventional techniques.

In addition if, as may be the case, the life and/or functionality of certain components is dependent on the type of surface produced by grinding, the method of the invention will go some way to ensuring that the life and/or functionality of such components when machined, eg by hard turning, is similar to that of the ground components.

Summary of the invention

According to the present invention there is provided a turning process in which a cutting tool engages the surface of a rotating component so as to remove a helix of metal therefrom as a result of synchronisation of the relative axial movement of the tool and the component and the rotation of the latter, at least the depth of cut achieved by the tool and component engagement is under the control of a programmed computer.

The computer may also be programmed to control the speed of rotation of the component.

The computer may also be programmed to control the relative axial movement between the tool and the component.

Typically the tool is moved axially relative to the component so as to progress the point of engagement between the tool and the surface of the component along the length of the latter as the component rotates.

Preferably the computer is programmed so as to synchronize the rotation of the component and the axial movement of the tool so that the locus of the point of engagement of the tool and the component is a helix.

Preferably the axial movement of the tool is synchironised with the rotation of the component so that the angle of the helix is such as to just advance the tool by the thickness of its cutting tip during each revolution, so that not only is a continuous helix of metal peeled away from the surface of the component as the machining progresses but a smooth surface is left behind.

If a taper is required in the component the depth of cut may be increased progressively with axial advance of the tool relative to the component, however the increasing depth of cut would still normally be controlled so as to produce a smooth surface, albeit of progressively reducing diameter.

The programming may be such as to increase the depth of cut during regularly spaced apart intervals.

The timing of the intervals may such that at least one depression is created during at least a part of each revolution of the component.

The timing may be such as to produce a plurality of depressions around each revolution of the component.

The timing of the intervals may be adjusted from one revolution to the next so that depressions do not become aligned parallel to the axis of the component.

The timing of the intervals may be selected so as to produce a regular or random or pseudo random pattern of depressions in the component surface.

Each interval may be of the same duration so that each depression is of the same extent, or a variation may be introduced into the duration of each of the intervals so that the depressions are of correspondingly different size.

In a preferred method each interval is arranged to extend over a plurality of consecutive revolutions of the component so that each resulting depression comprises an annular region of reduced diameter.

The transition between the turned surface of the component and each such annular depression may be gradual and itself may be generated during more than one revolution of the component, by programming the computer to increase the depth of cut gradually over the said one or more revolutions during which the transition is to occur.

At one end of such an annular depression the computer programme may be arranged to reduce the depth of cut in a similar gradual manner over a corresponding number of revolutions of the component, back to that required to produce the turned surface of the component beyond the annular depression.

Where the component is to taper in overall diameter, the depth of cut instructions generated by the programme during the transitions and during the generation of each reduced diameter annular region must take this into account, so that diameter of the component is progressively reduced during the whole of the turning process.

Since the depressions are merely to break-up what would otherwise be a smooth surface produced by the turning process, the depth of each depression relative to the surrounding turned surface will normally need only to be very small Differences in radius as between the base of each depression and the surrounding turned surface may be of the order of 1 micron or less Where more significant surface break-up is desired the difference in radius may be of the order of 2 or 3 microns or more.

Where the final surface specification includes a bearing ratio vector requirement, the latter may be achieved by adjusting the rate of change of radius (diameter) at one or both ends of each depression so that the required percentage of component material will exist at the specified depths relative to the peak diameter of the turned surface.

Where a bluing gauge percentage figure has to be complied with, the computer may be programmed to adjust the extent of the depressions relative to the remaining area of the turned component surface, so as to provide a sufficient overall area of turned surface which will be inked by the gauge, during the bluing test, relative to the overall area of the depressions, which will not normally become inked during the test.

Where the final surface is to be capable of being tested at any point along its axial length, the programme should arrange that the depressions are evenly distributed over the overall surface of the component to ensure that measurements made on the component will tend to be the same wherever they are made.

Where the component is to be gauged as part of the control of the turning process, it is desirable that the precise positions of the depressions and any transitions between depression and main turned surface are known and to this end the programme advantageously organises the computer to store co-ordinates of the depressions and transitions or an algorithm of their generation, so that an appropriate correction can be made to the result of any gauged value of (say) diameter, or the position at which a gauge is to be applied may be determined in advance of the gauging step and the gauge or the component positioned accordingly before the measurement is made.

The invention also lies in a component when manufactured in accordance with a computer controlled hard turning method as proposed by the invention disclosed herein.

The invention also lies in a metal turning machine and computer control therefor programmed to perform a hard turning operation in accordance with the invention.

The invention also lies in a metal turning machine in combination with a computer based control system therefor, when programmed to perform a hard turning process on a component in accordance with the invention.

The invention also lies in a computer when programmed to control a metal working machine so as to perform a hard turning operation on a component such as described herein.

The invention also lies in a programme adapted to operate a computer so as to provide control signals for a metal working machine to cause the latter to perform a hard turning operation such as described herein.

The invention also lies in a computer programme for operating a computer so as to control a metal working machine to perform a hard turning operation on a component such as described herein, when stored on a data carrier.

Examples of components which may be made in accordance with the invention, .

Synchro cones for gearboxes have hitherto been formed by grinding to a particular surface and taper diameter specification In a method in accordance with the invention of hard turning such a component so as to have a surface which will fall within the previous specification for the component, using a computer controlled metal turning process as aforesaid, the computer was programmed so as to introduce into the turned surface a plurality of annular depressions having a depth relative to the turned surface of 1 micron, pitched at 1 mm spacings along the axial length of the component Each depression extended over a total axial distance of 0 2 mm with a transition involving a gradual change in radius extending over 0 02 mm at each side of the depression (within the 0 2 mm width), so that the base of the depression, which lay a full 1 micron below the turned surface at either end, extended over less than the 0 2 mm width of the depression.

Other examples of a similar component involved the formation therein of similar depressions having the same overall axial extent and similar transitions, but with depths of 2 microns and 3 microns respectively, for comparison purposes.

Injector bores for fuel injectors for diesel engines have to be internally finished to a high accuracy and have hitherto been ground to achieve the desired finish and diameter The invention offers an alternative manufacturing process for such injectors in which the bores are hard turned under computer control in accordance with the invention and have depressions formed in their internal surfaces to produce a surface having appropriate characteristics to conform to the original specification for the product when internally ground.

The invention will now be described, by way of example only, with reference to the accompanying drawings in which:

Figure 1 is a perspective view of a synchromesh gear for an automotive manual gear box, and having an external cone formed by a turning process in accordance with the present invention; Figure 2 is a magnified plan view of depressions formed in the surface of the cone shown in Figure 1; and Figure 3 is a diagram in section (not to scale) showing the depressions of Figure 2.

The synchromesh gear shown in Figure 1 has a short external taper 10 which is formed on a precision lathe, operating in accordance with the process of the invention The lathe may be a hard turning lathe Type DT 40 made by Landis Lund (a division of UNOVA UK Limited) of Cranfield, England For further details of such a machine tool or precision lathe, reference may be made to published International Patent specification W 097/30381.

The computer programme which controls the lathe for forming the taper 10, is arranged to introduce minute annular depressions in the otherwise relatively smooth surface of the taper 10.

Three such depressions in the surface of the taper, are shown at 12, 14 and 16 in the magnified plan view of Figure 2, which is enlarged 35 times.

For a clearer view of the depressions, reference is made to the section shown in Figure 3, in which typically each depression has a depth of 1 micron, a base width of 0 16 mm, and an overall width of 0 2 mm which merges down to the base at each side over a width of 20 microns The distance or pitch between depressions is approximately Omm.

Although the invention has been described primarily with reference to hard turning, it is applicable generally to any machining process where the surface is generated by metal cutting.

It could therefore also be applied to boring, eg jig boring, and even to CNC form milling using a round-nosed cutter.

C 647 00/W

Claims

1 A programmed computer or a computer programme for operating a computer, adapted to control the operation of a metal machining process involving the removal of metal from a rotating workpiece by the engagement therewith of the tip of a metal cutting tool, at least the position of which is controlled by the said computer, and which as a result of rotation of the workpiece and of synchronised relative axial movement between the tool and the workpiece would produce a smooth machined surface thereon, wherein the programme also serves to alter the instantaneous radial position of the tool so as to introduce into the otherwise smooth surface, during the machining process, a plurality of substantially circumferentially spaced apart depressions for the purpose of simulating a surface typical of that which would be obtained thereon if the latter had been finished by grinding.

2 A metal turning machine in combination with a computer based control system therefor, when programmed to perform a hard turning process on a rotating workpiece involving the removal of metal from the surface thereof by the engagement therewith of the tip of a metal cutting tool, at least the position of which is controlled by the said computer based control system, and which as a result of rotation of the workpiece and of synchronised relative axial movement between the tool and the workpiece would produce a smooth surface thereon, wherein the programme also serves to alter the instantaneous position of the tool during the machining process, so as to introduce into the otherwise smooth surface a plurality of substantially circumferentially spaced apart depressions, for the purpose of simulating a surface typical of that which would be obtained on the workpiece if the latter had been finished by grinding.

3 A machine tool in combination with a computer based control system therefor, when programmed to perform a machining process on a workpiece, involving the removal of material from the workpiece by the engagement therewith of a cutting tool, at least the position of which is controlled by the said computer based control system and which, as a result of rotation of the workpiece and of synchronised relative movement between the tool and the workpiece would produce a smooth surface on the machined part, wherein the programme also serves to alter the instantaneous position of the tool so as to introduce into the otherwise smooth surface of the machined part a plurality of substantially circumferentially spaced apart depressions during the machining process, for the purpose of simulating a surface typical of that which would be obtained thereon if the latter had been finished by grinding.

4 Apparatus according to claim 2 or claim 3, further comprising at least one gauging or measuring device adapted to perform measurements on the workpiece during the machining process, to generate signals indicative of one or more dimensions of the workpiece, and means for conveying the signals to the computer as feedback signals indicative of how the process is progressing, to assist in the control of the process.